CN112758313B

CN112758313B - Rotorcraft relay passenger carrying method, device, equipment and storage medium

Info

Publication number: CN112758313B
Application number: CN202110035263.6A
Authority: CN
Inventors: 郄新越
Original assignee: Beijing Jingdong Qianshi Technology Co Ltd
Current assignee: Beijing Jingdong Qianshi Technology Co Ltd
Priority date: 2021-01-12
Filing date: 2021-01-12
Publication date: 2024-01-12
Anticipated expiration: 2041-01-12
Also published as: CN112758313A

Abstract

The embodiment of the application provides a method, a device, equipment and a storage medium for carrying passengers in relay of a rotorcraft, wherein the first rotorcraft takes off from a first airport and is fixedly provided with a separable target cabin, the first rotorcraft can fly according to first route information received from a dispatching center of the first airport, when the distance between the first rotorcraft and the dispatching center of a second airport is determined to be smaller than a preset distance, a cabin relay request is sent to the dispatching center of the second airport, a cabin relay response fed back by the dispatching center of the second airport is received, the second rotorcraft to be relayed is separated from the target cabin when the second rotorcraft is confirmed to be fixedly connected with the target cabin, and falls to the second airport to supplement electric energy, and the second rotorcraft flies according to the second route information, so that the passenger cabin taken by a passenger always flies in the air and to a destination, and the flight efficiency and the user experience are improved.

Description

Rotorcraft relay passenger carrying method, device, equipment and storage medium

Technical Field

The embodiment of the application relates to the technical field of gyroplanes, in particular to a method, a device, equipment and a storage medium for carrying passengers in relay of a gyroplane.

Background

Along with the progress of scientific technology and the necessity of clean energy development, the gyroplane gradually enters the field of view of people, has the characteristics of energy conservation, environmental protection, high efficiency and low energy consumption, has low noise and vibration level, good riding comfort, realizes near zero emission, and is an environment-friendly airplane which is truly rare.

In the prior art, the gyroplane mainly drives the plane to fly by the motor, the electric power source of the motor is mainly a battery, the electric power of the battery is limited due to the influence of battery technology, and the battery needs to be charged in time when the electric power of the battery is insufficient, so that the gyroplane has certain effects in a plurality of fields such as short-distance transportation, pilot training, flight experience and the like.

In the process of implementing the present invention, the inventor finds that at least the following problems exist in the prior art: because the range of the rotorcraft is limited to the electric quantity of the battery to a great extent, if the range of the passenger exceeds the one-way maximum range which can be supported by the battery in the rotorcraft, the rotorcraft needs to drop midway and supplement electric energy, and fly to a destination after the battery is full of electricity, so that the flight efficiency and the riding experience of the passenger are reduced to a great extent.

Disclosure of Invention

The embodiment of the application provides a rotorcraft relay passenger carrying method, device, equipment and storage medium, which are used for solving the problems of low flight efficiency and poor passenger experience of the existing rotorcraft.

In a first aspect, an embodiment of the present application provides a method for relay passenger carrying of a gyroplane, applied to a first gyroplane sailing from a first airport, on which a separable target cabin is fixed, the method comprising:

flying according to first route information received from a dispatch center of the first airport;

when the distance between the first gyroplane and the dispatching center of the second airport is smaller than the preset distance, sending a cabin relay request to the dispatching center of the second airport;

receiving a cabin relay response fed back by a dispatch center of the second airport, the cabin relay response comprising: identification of the second gyroplane to be relayed;

and when the second gyroplane is determined to be fixedly connected with the target passenger cabin, separating the second gyroplane from the target passenger cabin, and landing the second gyroplane to the second airport for supplementing electric energy.

In one possible design of the first aspect, after the receiving the cabin relay response fed back by the dispatch center of the second airport, the method further comprises:

establishing a communication link with the second gyroplane according to the identification of the second gyroplane;

and sending real-time position information of the first rotorcraft and a fixed connection mode of the target cabin and the first rotorcraft to the second rotorcraft through the communication link.

In another possible design of the first aspect, the upper side of each gyroplane is provided with a cabin attachment fixture, and the lower side of each gyroplane is provided with a cabin mounting fixture;

if the first gyroplane is fixedly connected with the target cabin through the cabin mounting fixing device at the lower side, the second gyroplane is fixedly connected with the target cabin, and the method comprises the following steps: the second gyroplane fixes the target cabin on the upper side of the second gyroplane through a cabin fixing device on the upper side;

said separating from said target passenger compartment comprising:

and loosening the cabin mounting fixing device on the lower side of the first gyroplane so as to separate the first gyroplane from the target cabin.

In a further possible design of the first aspect, the upper side of each gyroplane is provided with a cabin attachment fixture, and the lower side of each gyroplane is provided with a cabin mounting fixture;

if the first gyroplane secures the target cabin to an upper side of the first gyroplane via an upper side cabin securing device, then the second gyroplane is fixedly connected to the target cabin, comprising: the second rotorcraft fixes the target cabin on the lower side of the second rotorcraft through the downloaded cabin mounting fixing device;

Said separating from said target passenger compartment comprising:

and releasing the cabin fixing device on the upper side of the first gyroplane to separate the first gyroplane from the target cabin.

In a second aspect, embodiments of the present application provide a method for relay passenger carrying of a gyroplane, applied to a second gyroplane parked at a second airport, the method comprising:

receiving relay indication information sent by a dispatching center of the second airport, wherein the relay indication information comprises: the second route information and the identity of the first gyroplane to take over;

acquiring real-time position information of the first gyroplane, and fixedly connecting a target cabin on the first gyroplane with the first gyroplane;

according to the real-time position information of the first gyroplane and the fixed connection mode of the target cabin on the first gyroplane and the first gyroplane, the first gyroplane is fixedly connected with the target cabin;

and when the first gyroplane is separated from the target passenger cabin, flying according to the second route information.

In one possible design of the second aspect, the acquiring real-time position information of the first gyroplane and a fixed connection manner between the target cabin on the first gyroplane and the first gyroplane includes:

Establishing a communication link with the first gyroplane according to the identification of the first gyroplane;

and receiving real-time position information sent by the first rotorcraft through the communication link and a fixed connection mode of a target cabin on the first rotorcraft and the first rotorcraft.

In another possible design of the second aspect, the method for fixedly connecting the target cabin on the first gyroplane with the first gyroplane according to the real-time position information of the first gyroplane and the fixed connection mode of the target cabin on the first gyroplane includes:

determining a target position relationship between the second gyroplane and the target cabin according to a fixed connection mode of the target cabin and the first gyroplane;

and according to the real-time position information of the first gyroplane and the target position relation, the first gyroplane is fixedly connected with the target passenger cabin.

Optionally, a cabin fixing device is arranged on the upper side of each gyroplane, and a cabin mounting fixing device is arranged on the lower side of each gyroplane;

the determining, according to the fixed connection manner of the target cabin and the first gyroplane, the target positional relationship between the second gyroplane and the target cabin includes:

When the target cabin is mounted on the lower side of the first gyroplane through a cabin mounting fixing device on the lower side of the first gyroplane, determining the target position relationship as that the target cabin is loaded on the second gyroplane;

the method for fixedly connecting the first gyroplane with the target cabin according to the real-time position information of the first gyroplane and the target position relationship comprises the following steps:

according to the real-time position information of the first gyroplane, flying to the lower part of the target cabin based on the target position relation;

and fixing the target cabin on the second gyroplane through a cabin fixing device on the upper side of the second gyroplane.

when the target cabin is borne on the first gyroplane through a cabin fixing device on the upper side of the first gyroplane, determining the target position relationship as that the target cabin is mounted below the second gyroplane;

according to the real-time position information of the first gyroplane, flying to the position above the target cabin based on the target position relation;

and fixing the target cabin below the second gyroplane through a cabin mounting and fixing device at the lower side of the second gyroplane.

In a third aspect, an embodiment of the present application provides a method for relay passenger carrying of a gyroplane, applied to a dispatch center of an initial airport, the method including:

acquiring an initial airport and a destination airport of a passenger;

determining a target flight route of a target passenger cabin where the passenger takes according to the position information of the starting airport and the position information of the destination airport;

determining at least one relay airport in the target flight route and the route information of the target rotorcraft needing relay in each relay airport according to the airport information of the target flight route and the maximum route information of the idle rotorcraft parked in each airport;

synchronizing route information of the target gyroplanes requiring relay for each relay airport to a dispatch center in each relay airport.

In a fourth aspect, embodiments of the present application provide a gyroplane relay passenger carrier device for use with a first gyroplane sailing from a first airport, the first gyroplane having a detachable target cabin secured thereto, the device comprising: the device comprises a processing module, a sending module and a receiving module;

the processing module is used for flying according to the first route information received by the receiving module from the dispatching center of the first airport;

the sending module is used for sending a cabin relay request to the dispatching center of the second airport when the distance between the first rotorcraft and the dispatching center of the second airport is determined to be smaller than a preset distance;

the receiving module is configured to receive a cabin relay response fed back by a dispatch center of the second airport, where the cabin relay response includes: identification of the second gyroplane to be relayed;

the processing module is further configured to, when it is determined that the second gyroplane is fixedly connected to the target cabin, separate from the target cabin and drop to the second airport for supplementing electrical energy.

In one possible design of the fourth aspect, the processing module is further configured to establish a communication link with the second gyroplane according to an identification of the second gyroplane;

The sending module is further configured to send, to the second gyroplane through the communication link, real-time location information of the first gyroplane and a fixed connection manner between the target cabin and the first gyroplane.

In another possible design of the fourth aspect, the upper side of each gyroplane is provided with a cabin attachment fixture, and the lower side of each gyroplane is provided with a cabin mounting fixture;

if the first gyroplane is fixedly connected with the target cabin through the cabin mounting fixing device at the lower side, the second gyroplane is fixedly connected with the target cabin, specifically: the second gyroplane fixes the target cabin on the upper side of the second gyroplane through a cabin fixing device on the upper side;

the processing module is configured to be separated from the target cabin, specifically:

the processing module is specifically configured to release the cabin mounting fixture on the lower side of the first gyroplane, so as to separate the first gyroplane from the target cabin.

In a further possible design of the fourth aspect, the upper side of each gyroplane is provided with a cabin attachment fixture, and the lower side of each gyroplane is provided with a cabin mounting fixture;

If the first gyroplane fixes the target cabin on the upper side of the first gyroplane through the cabin fixing device on the upper side, the second gyroplane is fixedly connected with the target cabin, specifically: the second rotorcraft fixes the target cabin on the lower side of the second rotorcraft through the downloaded cabin mounting fixing device;

the processing module is specifically configured to release a cabin fixing device on an upper side of the first gyroplane so as to separate the first gyroplane from the target cabin.

In a fifth aspect, embodiments of the present application provide a gyroplane relay passenger carrier for use with a second gyroplane parked at a second airport, the device comprising: the device comprises a receiving module, an acquisition module and a processing module;

the receiving module is configured to receive relay indication information sent by a dispatch center of the second airport, where the relay indication information includes: the second route information and the identity of the first gyroplane to take over;

the acquisition module is used for acquiring real-time position information of the first gyroplane and a fixed connection mode of a target cabin on the first gyroplane and the first gyroplane;

The processing module is used for carrying out flight according to the real-time position information of the first gyroplane, the fixed connection mode of the target cabin on the first gyroplane and the first gyroplane, the processing module is fixedly connected with the target cabin, and the processing module is used for carrying out flight according to the second route information when determining that the first gyroplane is separated from the target cabin.

In one possible design of the fifth aspect, the processing module is further configured to establish a communication link with the first gyroplane according to an identification of the first gyroplane;

the receiving module is further configured to receive, through the communication link, real-time position information sent by the first gyroplane and a fixed connection manner between a target cabin on the first gyroplane and the first gyroplane;

the acquisition module is specifically configured to acquire the real-time position information sent by the first gyroplane and received by the receiving module, and a fixed connection mode between a target cabin on the first gyroplane and the first gyroplane.

In another possible design of the fifth aspect, the processing module is configured to fixedly connect the target cabin on the first gyroplane with the target cabin according to the real-time position information of the first gyroplane and a fixed connection mode of the target cabin on the first gyroplane, specifically:

The processing module is specifically configured to:

the processing module is configured to determine, according to a fixed connection manner between the target cabin and the first gyroplane, a target positional relationship between the second gyroplane and the target cabin, specifically:

the processing module is specifically configured to determine that the target cabin is loaded on the second gyroplane when the target cabin is mounted on the lower side of the first gyroplane through the cabin mounting fixing device on the lower side of the first gyroplane;

the processing module is configured to be fixedly connected with the target cabin according to the real-time position information of the first gyroplane and the target position relationship, and specifically includes:

the processing module is specifically configured to fly to a position below the target cabin based on the target positional relationship according to the real-time positional information of the first gyroplane, and fix the target cabin above the second gyroplane through a cabin fixing device on the upper side of the second gyroplane.

the processing module is specifically configured to determine that the target cabin is mounted below the second gyroplane when the target cabin is carried on the first gyroplane by a cabin fixing device on the upper side of the first gyroplane;

the processing module is specifically configured to fly to above the target cabin based on the target positional relationship according to the real-time positional information of the first gyroplane, and fix the target cabin below the second gyroplane through the cabin mounting and fixing device at the lower side of the second gyroplane.

In a sixth aspect, an embodiment of the present application provides a rotorcraft relay passenger device, applied to a dispatch center of an origin airport, the device comprising:

The acquisition module is used for acquiring an initial airport and a destination airport of a passenger;

the determining module is used for determining a target flight route of a target passenger cabin taken by the passenger according to the position information of the starting airport and the position information of the destination airport, and determining at least one relay airport in the target flight route and route information of the target rotorcraft needing relay in each relay airport according to the airport information passed by the target flight route and the maximum route information of the idle rotorcraft parked in each airport;

and the synchronization module is used for synchronizing the route information of the target gyroplane which needs to be relayed by each relay airport to a dispatching center in each relay airport.

In a seventh aspect, embodiments of the present application provide a gyroplane, including a processor, a memory, a transceiver, and a computer program stored on the memory and executable on the processor, the processor implementing the method according to the first aspect and possibly designed as described above when executing the program, or the processor implementing the method according to the second aspect and possibly designed as described above when executing the program.

In an eighth aspect, embodiments of the present application provide an airport dispatch center comprising a processor, a memory, a transceiver, and a computer program stored on the memory and executable on the processor, the processor implementing the method according to the third aspect when executing the program.

In a ninth aspect, embodiments of the present application provide a computer-readable storage medium having stored therein computer-executable instructions for implementing the method according to the first aspect and the various possible designs described above when executed by a processor, or for implementing the method according to the first aspect and the various possible designs described above when executed by a processor.

In a tenth aspect, embodiments of the present application provide a computer-readable storage medium having stored therein computer-executable instructions, which when executed by a processor, are configured to implement a method as described in the third aspect above.

In an eleventh aspect, embodiments of the present application provide a computer program product comprising: computer instructions for implementing the method as described in the above first aspect and various possible designs when executed by a processor; alternatively, the computer instructions, when executed by a processor, are adapted to carry out the method as described in the second aspect and the various possible designs described above.

In a twelfth aspect, embodiments of the present application provide a computer program product comprising: computer instructions for implementing the method according to the third aspect described above when executed by a processor.

According to the method, the device, the equipment and the storage medium for carrying passengers in relay of the gyroplane, the dispatching center of the initial airport can determine the target flight route of a target cabin taken by a passenger according to the acquired position information of the initial airport and the position information of the destination airport, at least one relay airport in the target flight route and the route information of the target gyroplane, which needs to be relayed, of each relay airport, and synchronize the route information of the target gyroplane, which needs to be relayed, of each relay airport to the dispatching center in each relay airport, accordingly, the first gyroplane, which takes off from the first airport and is provided with a separable target cabin, flies according to the first route information received from the dispatching center of the first airport, sends a cabin relay request to the dispatching center of the second airport when the distance between the first gyroplane and the dispatching center of the second airport is determined to be smaller than a preset distance, receives a cabin relay response fed back by the dispatching center of the second airport, separates from the target when the second gyroplane, which needs to be relayed is confirmed to be fixedly connected with the target, and accordingly, the first gyroplane, takes off from the target and lands to the second gyroplane, and the passenger can always fly in the second aircraft according to the second aircraft, and the electric energy is always received by the second aircraft, and the passenger cabin information, and the passenger cabin is always takes on the second aircraft.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the disclosure and together with the description, serve to explain the principles of the disclosure.

Fig. 1 is a schematic structural diagram of a gyroplane according to an embodiment of the present disclosure;

FIG. 2A is a loading schematic of a passenger cabin on a rotorcraft;

FIG. 2B is another loading schematic of a passenger cabin on a rotorcraft;

FIG. 3 is a schematic diagram of an architecture of a rotorcraft relay passenger system;

fig. 4 is a schematic flow chart of a first embodiment of a method for carrying passengers on a rotorcraft according to an embodiment of the present application;

fig. 5 is an interactive schematic diagram of a second embodiment of a rotorcraft relay passenger carrying method provided in an embodiment of the present application;

fig. 6 is a schematic structural view of a first embodiment of a rotorcraft relay passenger carrier provided by the present application;

fig. 7 is a schematic structural diagram of a second embodiment of a rotorcraft relay passenger carrier provided by the present application;

fig. 8 is a schematic structural view of a third embodiment of a rotorcraft relay passenger carrier provided by the present application;

fig. 9 is a schematic structural diagram of an airport dispatching center according to an embodiment of the present application;

fig. 10 is a schematic structural view of a gyroplane according to an embodiment of the present application.

Specific embodiments of the present disclosure have been shown by way of the above drawings and will be described in more detail below. These drawings and the written description are not intended to limit the scope of the disclosed concepts in any way, but rather to illustrate the disclosed concepts to those skilled in the art by reference to specific embodiments.

Detailed Description

Reference will now be made in detail to exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numbers in different drawings refer to the same or similar elements, unless otherwise indicated. The implementations described in the following exemplary examples are not representative of all implementations consistent with the present disclosure. Rather, they are merely examples of apparatus and methods consistent with some aspects of the present disclosure as detailed in the accompanying claims.

With the continuous rising of petroleum price and the requirement of low carbon economy, the traveling mode of new energy becomes an important direction of development of various industries due to low pollution and high efficiency. The gyroplane is a new energy traveling mode which gradually appears in the field of vision of people along with the economic development.

Because the voyage of the existing rotorcraft is limited by the electric quantity of the battery to a great extent, if the voyage of a passenger exceeds the single-trip maximum voyage which can be supported by the battery in the rotorcraft, the rotorcraft needs to drop midway and supplement electric energy, and fly to a destination after the battery is full of electricity, so that the flight efficiency and the riding experience of the passenger are reduced to a great extent.

Aiming at the problems, the technical conception process of the application is as follows: if the engine body and the cabin of the existing rotorcraft are arranged into a separable structure, and the upper side and the lower side of the engine body are respectively provided with a cabin fixing device, and a positioning module is arranged on the engine body, so that the two engine bodies can realize relay in the air, the passenger cabin taken by the passenger always flies to a destination airport in the air in the middle of the flight, the problem that the rotorcraft needs to land for charging is avoided, and the problems of inefficiency and poor riding experience caused by the fact that the rotorcraft cannot continuously fly are solved.

Based on the technical conception, the embodiment of the application provides a rotorcraft relay passenger carrying method, when a dispatch center of a starting airport obtains the starting airport and the target airport of a passenger, a target flight route of a target cabin taken by the passenger, at least one relay airport in the target flight route and route information of the target rotorcraft required to be relayed by each relay airport can be determined according to the position information of the starting airport and the position information of the target airport, and the route information of the target rotorcraft required to be relayed by each relay airport is synchronized to the dispatch center in each relay airport.

Exemplary, fig. 1 is a schematic structural diagram of a gyroplane according to an embodiment of the present application. As shown in fig. 1, the gyroplane may include: the passenger cabin fixing device comprises a machine body 11, a passenger cabin fixing device 12 arranged on the upper side of the machine body 11 and a passenger cabin mounting fixing device 13 arranged on the lower side of the machine body 11.

Optionally, in practical application, the cabin fixing device 12 and the cabin mounting fixing device 13 may be implemented by a steering engine, a stepper motor, a hook, and the like, and are mainly used for fixing the target cabin with the body 11, so as to implement the fixed connection between the target cabin and the gyroplane. It will be appreciated that the embodiments of the present application are not limited to specific implementations of the cabin fixing device 12 and the cabin mounting fixing device 13, and may be determined according to actual situations.

By way of example, the gyroplane of the embodiments of the present application may be either an unmanned gyroplane or a manned gyroplane, which is not limited herein. Fig. 1 is an exemplary illustration of an unmanned gyroplane.

It will be appreciated that the embodiments of the present application are not limited to the specific structure and implementation of the machine body, and may be designed according to actual design, which is not described herein.

Based on the structure of the gyroplane shown in fig. 1, fig. 2A is a schematic loading diagram of the passenger cabin on the gyroplane. Fig. 2B is another loading schematic of a passenger cabin on a rotorcraft. As can be seen from the gyroplane shown in fig. 1, the gyroplane can fix the cabin on the gyroplane by using the cabin fixing device 12 on the upper side of the body 11 to form the loading diagram shown in fig. 2A, and can fix the cabin on the gyroplane by using the cabin mounting fixing device 13 on the lower side of the body 11 to form the loading diagram shown in fig. 2B.

Based on the above schematic diagrams, fig. 3 is a schematic structural diagram of a relay passenger carrying system of a gyroplane. As shown in fig. 3, the architecture diagram may include: a plurality of airports, each having a dispatch center disposed therein, each dispatch center for dispatching and managing gyroplanes parked within the airport at which they are located.

In the architecture diagram shown in fig. 3, 4 airports are exemplarily shown, namely an airport a to an airport D, wherein the airport a is the initial airport of the target cabin, the airport D is the destination airport of the target cabin, and the airports B and C are relay airports of the target cabin.

It can be understood that the embodiments of the present application do not limit the number of airports in the rotorcraft relay passenger carrying system, and also do not limit the number of rotorcraft parked in each airport, which may be determined according to actual situations, and will not be described herein. Alternatively, the rotorcraft may also be referred to as an electric aircraft, which is not limited herein.

In practical application, when the target cabin needs to start from the airport a and needs to arrive at the airport D, the dispatching center of the airport a can determine the target flight route of the target cabin according to the position information of the airport a and the airport D, further can determine at least one relay airport in the target flight route and the route information of the target rotorcraft needing relay in each relay airport according to the information of the airport passed by the target flight route and the maximum route information of the idle rotorcraft parked in each airport, and finally synchronizes the route information of the target rotorcraft needing relay in each relay airport to the dispatching center of the corresponding relay airport.

Illustratively, assume that rotorcraft number 1 in airport A is stationary with the target passenger cabin at airport A. The specific fixing modes can be various, and one mode is that the No. 1 gyroplane flies to the position of a target cabin based on the indication of the affiliated dispatching center, and the cabin mounting fixing device at the lower side of the No. 1 gyroplane is utilized to automatically mount the target cabin to the lower side of the No. 1 gyroplane in a separable manner; the other mode is that a worker uses the cabin moving device to carry the target cabin to the position of the No. 1 gyroplane, and then loads the target cabin to the upper side of the No. 1 gyroplane, so that the cabin fixing device on the upper side of the No. 1 gyroplane can detachably fix the target cabin on the No. 1 gyroplane, or the No. 1 gyroplane uses the cabin mounting fixing device on the lower side to automatically detachably mount the target cabin on the lower side of the No. 1 gyroplane. The fixing manner of the number 1 gyroplane and the target cabin is not limited in this embodiment, and will not be described here again.

In practice, passengers need to first safely ride into the target cabin before the number 1 rotor takes off with the target cabin.

For example, assuming that the passenger cabin of the passenger from airport a is mounted below the rotorcraft No. 1, and that the rotorcraft No. 1 takes off from airport a and flies to the upper space of airport B, the rotorcraft No. 2, which is served by airport B, realizes detachable fixed connection with the target cabin through the cabin fixing device on the upper side, and notifies the rotorcraft No. 1, and when it is determined that the rotorcraft No. 2 is fixedly connected with the target cabin, the cabin mounting fixing device on the lower side is released, separated from the target cabin, and falls to airport B for charging. Correspondingly, the No. 2 gyroplane continues to fly according to the acquired route information.

Similarly, when the No. 2 gyroplane flies to the upper air of the C airport, the C airport sends out the relay No. 3 gyroplane to realize detachable fixed connection with the target passenger cabin through the passenger cabin mounting fixing device on the lower side, and the No. 2 gyroplane is informed, and when the No. 3 gyroplane is determined to be fixedly connected with the target passenger cabin, the passenger cabin fixing device on the upper side is loosened, and the C airport is separated from the target passenger cabin and falls to the C airport to charge. Correspondingly, the No. 3 gyroplane continuously flies according to the received route information, the aircraft lands on the D airport after flying to the D airport, passengers arrive at the destination underground cabin, and the No. 3 gyroplane is charged on the D airport.

The relay passenger carrying flying of the rotorcraft is completed through the process, so that passengers always fly to the destination in the air when taking the rotorcraft, and the problems of low efficiency and poor riding experience caused by the fact that the rotorcraft needs to fall and charge due to insufficient power are avoided.

The following describes the technical solutions of the present application and how the technical solutions of the present application solve the above technical problems in detail with specific embodiments. The following embodiments may be combined with each other, and the same or similar concepts or processes may not be described in detail in some embodiments. Embodiments of the present application will be described below with reference to the accompanying drawings.

Fig. 4 is a schematic flow chart of a first embodiment of a method for carrying passengers on a rotorcraft according to an embodiment of the present application. The rotorcraft relay passenger carrying method is applied to a dispatching center of an initial airport. As shown in fig. 4, the rotorcraft relay passenger carrying method may include the following steps:

s401, acquiring an initial airport and a destination airport of a passenger.

In this embodiment, when a passenger at the starting airport needs to go to the destination airport, the staff at the starting airport can input both the starting airport and the destination airport of the passenger to the dispatch center of the starting airport, so that the dispatch center of the starting airport can obtain the starting airport and the destination airport of the passenger. It will be appreciated that the staff at the starting airport may input the starting position and destination position of the passenger to the dispatch center at the starting airport, so that the dispatch center at the starting airport may automatically locate the starting airport based on the starting position of the passenger and may also automatically locate the destination airport based on the destination position of the passenger. The embodiments of the present application do not limit how the dispatch center at the origin airport can obtain the origin airport and destination airport of the passenger.

S402, determining a target flight route of a target passenger cabin where the passenger takes according to the position information of the starting airport and the position information of the destination airport.

For example, the dispatch center of the starting airport may determine the heading of the rotorcraft from the starting airport and the target flight path when the rotorcraft arrives at the destination airport based on the location information of the starting airport and the location information of the destination airport.

In this embodiment, the target flight path of the target passenger cabin on which the passenger is seated is actually the theoretical path of the gyroplane flying from the starting airport to the destination airport. The target flight path may include multiple segments, each of which may only fly one of which, based on the maximum unidirectional range of the gyroplanes.

S403, determining at least one relay airport in the target flight route and the route information of the target rotorcraft requiring relay in each relay airport according to the airport information of the target flight route and the maximum route information of the idle rotorcraft parked in each airport.

Optionally, the dispatch center of the starting airport may acquire information of the air-carrier according to the air-carrier information of the target flight route and information of the gyroplanes parked in each air-carrier, for example, information such as the route of the target flight route through several air-carriers, the space size of each air-carrier, the number of idle gyroplanes parked in each air-carrier, the maximum unidirectional course when each idle gyroplane is full, etc., so as to determine whether the maximum unidirectional course existing in the air-carrier is greater than the idle full-electric gyroplanes of the air-carrier and the required mileage of the next adjacent air-carrier when the dispatch center of the starting airport passes through a certain air-carrier, and if the maximum unidirectional course exists, the air-carrier can be used as a relay air-carrier in the target flight route, and determine the air-carrier information of the target gyroplanes requiring relay of the relay air-carrier.

In practical application, the dispatching center of the initial airport can determine various schemes, for example, the number of relay airports in a target flight route in a certain scheme is small, the range among certain relay airports is far, and a gyroplane with a large maximum unidirectional range is needed, but the number of relay in the air is relatively small; for another example, if the number of relay airports in the target flight route in a certain scheme is large, the range between certain relay airports may be smaller, and the maximum unidirectional range of the required gyroplane is relatively smaller, but the number of relay in the air is large.

In this embodiment, the dispatch center at the starting airport may present a plurality of determined schemes for the staff to choose according to a plurality of factors such as cost, time-of-day, etc., which is not limited herein.

S404, synchronizing the route information of the target gyroplanes requiring relay in each relay airport to a dispatching center in each relay airport.

In this embodiment, when determining all relay airports in the target flight route and route information of the target rotorcraft requiring relay for each relay airport, the dispatch center of the starting airport may synchronize the above information to the dispatch center of each relay airport, so that when the rotorcraft flies within the range of the corresponding relay airport and sends a cabin relay request to the dispatch center of the corresponding relay airport, the dispatch center of the corresponding relay airport may determine the rotorcraft to be relayed according to the maximum unidirectional route information of the idle rotorcraft parked in the affiliated airport, and send the corresponding flight route to the rotorcraft to be relayed, so that the rotorcraft to be relayed flies based on the information.

According to the rotorcraft relay passenger carrying method, the scheduling center of the starting airport can determine the target flight route of the target passenger cabin where passengers take according to the acquired position information of the starting airport and the position information of the destination airport of the passengers, and then determine at least one relay airport in the target flight route and the route information of the target rotorcraft needing relay in each relay airport according to the airport information of the target flight route and the maximum route information of the idle rotorcraft parked in each airport, and synchronize the route information of the target rotorcraft needing relay in each relay airport to the scheduling center in each relay airport. According to the technical scheme, at least one relay airport capable of relaying in a target flight route and route information of a target rotorcraft needing relaying in each relay airport can be determined and synchronized to a dispatching center of the corresponding relay airport, so that conditions are provided for realizing relay flight subsequently.

Fig. 5 is an interactive schematic diagram of a second embodiment of a rotorcraft relay passenger carrying method according to an embodiment of the present application. The rotorcraft relay passenger carrying method is explained by information interaction among a dispatching center of a first airport, the dispatching center of a first rotorcraft, a second airport and a second rotorcraft. As shown in fig. 5, the rotorcraft relay passenger carrying method may include the following steps:

S501, a dispatching center of the first airport sends first route information to the first gyroplane.

The first airport can be any one of all airports except the destination airport in the target flight route, namely the first airport can be an initial airport or any relay airport in the target flight route. The first gyroplane may be a gyroplane that meets a preset condition, which is parked in the first airport. The preset condition is that the first gyroplane is in an idle state, and the maximum range of the residual electric quantity of the first gyroplane capable of supporting flying is larger than the range corresponding to the first route information.

In this embodiment, the dispatch center of the first airport may determine, according to the acquired first route information and information of all gyroplanes parked in the first airport, a first gyroplane meeting a preset condition from all gyroplanes, and send the first route information to the first gyroplane.

Optionally, the information of the gyroplane may include whether the gyroplane is idle, whether there is other flight tasks, whether the gyroplane has the maximum range information of the remaining power that can support the flight, etc., which is not limited in this embodiment, and may be determined according to the actual scene.

As an example, if the first airport is the starting airport, the dispatch center of the first airport may send the first route information directly to the first gyroplane after determining the route information of each airport and determining the first gyroplane to be flown.

As another example, if the first airport is a relay airport in the target flight route, the dispatch center of the first airport may first determine, when receiving a cabin relay request sent from gyroplanes in other airports, a first gyroplane to be relayed according to first flight information synchronized from the dispatch center of the starting airport and information of all gyroplanes parked in the first airport, and then send the first route information to the first gyroplane.

S502, the first gyroplane flies according to the received first route information.

As an example, if a first rotorcraft has a detachable target cabin secured to its body before receiving first airline information sent by a dispatch center of the first airport, the first rotorcraft may fly based on the first airline information when it receives the first airline information. For example, if the first rotorcraft is a rotorcraft that is sailing from a starting airport, it may not receive the first airline information until the target passenger cabin is secured on the body.

As another example, if the first rotorcraft does not fix the target cabin on its body when it receives the first route information, the first rotorcraft first needs to fix with the target cabin, then fly based on the first route information when it is determined that the target cabin is fixed only by the first rotorcraft. For example, when the first gyroplane is a to-be-relayed gyroplane dispatched at a relay airport, the first gyroplane may first acquire the first route information and then fly into the air to fix the target passenger cabin.

S503, when the first gyroplane determines that the distance between the first gyroplane and the dispatching center of the second airport is smaller than the preset distance, the first gyroplane sends a cabin relay request to the dispatching center of the second airport.

Wherein the second airport is a relay airport adjacent to the first airport in the target flight path.

The first gyroplane flies from the first airport to the second airport based on the first route information, when the distance between the first gyroplane and the dispatching center of the second airport is determined to be smaller than the preset distance, the first gyroplane is indicated to fly into the coverage range of the second airport, and at the moment, a cabin relay request can be sent to the dispatching center of the second airport, so that the dispatching center of the second airport sends out gyroplanes meeting preset conditions to carry out cabin relay. The preset condition is similar to that in S501, and will not be described here.

Optionally, the specific value of the preset distance may be determined by the flying height of the gyroplane and the transceiving capability of the gyroplane, which is not described herein.

S504, determining a second gyroplane to be relayed from a plurality of gyroplanes parked in the second airport by the dispatching center of the second airport according to the received cabin relay request.

Optionally, when receiving the cabin relay request, the dispatch center of the second airport determines the destination airport of the target cabin, then determines the second route information that the gyroplane taking off from the second airport and relaying needs to fly according to the route information synchronized from the initial airport, and then determines the second gyroplane meeting the preset condition according to the route of the second route information and the information of a plurality of gyroplanes parked in the second airport, i.e. the second gyroplane is in an idle state, and the remaining electric quantity of the second gyroplane can support the maximum route of flying to be greater than the route corresponding to the second route information.

S505, the dispatch center of the second airport sends a cabin relay response to the first gyroplane, the cabin relay response comprising: identification of the second gyroplane to be relayed.

In this step, after determining the second gyroplane to be relayed, the dispatch center of the second airport may feed back a cabin relay response to the first gyroplane, specifically, send the identifier of the second gyroplane to be relayed to the first gyroplane, so that the first gyroplane performs certain operations, for example, actively establishes a connection with the second gyroplane, or waits for connection information sent by the second gyroplane after receiving the cabin relay response.

S506, the dispatch center of the second airport transmits relay indication information to the second gyroplane, where the relay indication information includes: the second route information and the identity of the first gyroplane to take over.

Optionally, after determining the second gyroplane to be relayed, the dispatch center of the second airport may send relay indication information carrying the second route information and the identifier of the first gyroplane to be successed to the second gyroplane, so that the second gyroplane actively establishes a connection with the first gyroplane, or waits for a connection establishment request initiated by the first gyroplane.

S507, the second gyroplane obtains real-time position information of the first gyroplane, and a target cabin on the first gyroplane is fixedly connected with the first gyroplane.

In one possible design of the present application, after receiving the cabin relay response sent by the dispatch center of the second airport, the first gyroplane may determine an identification of the second gyroplane to be relayed, and then establish a communication link with the second gyroplane according to the identification of the second gyroplane.

Specifically, the first rotorcraft sends a link establishment request to the second rotorcraft, the second rotorcraft receives the link establishment request, establishes a communication link between the first rotorcraft and the second rotorcraft, and sends a link establishment response to the first rotorcraft that the link establishment was successful.

In another possible design of the present application, after receiving the relay indication information sent by the dispatch center of the second airport, the second gyroplane may determine the identity of the first gyroplane to take over, and then establish a communication link with the first gyroplane according to the identity of the first gyroplane.

Specifically, the second gyroplane sends a link establishment request to the first gyroplane, the first gyroplane receives the link establishment request, establishes a communication link between the second gyroplane and the first gyroplane, and sends a link establishment response to the second gyroplane that the link establishment is successful.

Further, after the first gyroplane and the second gyroplane establish a communication link, the first gyroplane may send the real-time position information of the first gyroplane and the fixed connection mode of the target cabin and the first gyroplane to the second gyroplane through the communication link, and correspondingly, the second gyroplane may receive the real-time position information sent by the first gyroplane and the fixed connection mode of the target cabin and the first gyroplane on the first gyroplane through the communication link.

In practical application, all be provided with global positioning system (global positioning system, GPS) module on first gyroplane and the second gyroplane, first gyroplane and second gyroplane can acquire self position in real time like this, and both pass through the mode that the position sharing or first gyroplane sent self position to the second gyroplane in real time for the second gyroplane can acquire the real-time position information of first gyroplane.

S508, the second gyroplane is fixedly connected with the target cabin according to the real-time position information of the first gyroplane and the fixed connection mode of the target cabin on the first gyroplane and the first gyroplane.

In practical applications, since the position of the GPS module provided on each gyroplane is fixed, the real-time position information of each gyroplane is actually the real-time position information of the GPS module. In addition, according to the embodiments shown in fig. 1 to 3, there may be two fixed positions between each gyroplane and the target cabin, but the fixed connection manner between the two gyroplanes that perform the relay and the target cabin may not be the same.

For example, if the target cabin is fixed to the upper side of the first gyroplane, the second gyroplane needs to be fixed to the lower side of the second gyroplane when relaying, or if the target cabin is fixed to the lower side of the first gyroplane, the second gyroplane needs to be fixed to the upper side of the second gyroplane when relaying.

Based on the above, the second gyroplane can firstly determine the target position relationship between the second gyroplane and the target cabin according to the fixed connection mode between the target cabin and the first gyroplane, and then is fixedly connected with the target cabin according to the real-time position information and the target position relationship of the first gyroplane.

Specifically, as can be seen from the embodiments shown in fig. 1 to 3, the upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device; therefore, according to the fixed connection mode of the target cabin and the first rotorcraft, the second rotorcraft determines the target position relationship between the second rotorcraft and the target cabin in two ways:

a first possible implementation: when a target cabin is mounted on the lower side of a first gyroplane through a cabin mounting fixing device on the lower side of the first gyroplane, determining that the target position relationship between a second gyroplane and the target cabin is that the target cabin is loaded on the second gyroplane.

Correspondingly, the second gyroplane flies to the lower part of the target cabin based on the determined target position relation according to the real-time position information of the first gyroplane, and then the target cabin is fixed on the second gyroplane through the cabin fixing device on the upper side of the second gyroplane.

A second possible implementation: when a target cabin is borne on the first gyroplane through a cabin fixing device on the upper side of the first gyroplane, determining that the target position relationship between the second gyroplane and the target cabin is that the target cabin is mounted below the second gyroplane.

Correspondingly, the second gyroplane flies to the upper part of the target cabin based on the target position relation according to the real-time position information of the first gyroplane, and then the target cabin is fixed below the second gyroplane through the cabin mounting fixing device at the lower side of the second gyroplane.

And S509, when the second rotorcraft determines that the second rotorcraft is fixedly connected with the target cabin, sending connection notification information to the first rotorcraft.

For example, when the second gyroplane detachably fixes the target cabin on the upper side of the second gyroplane, or the target cabin detachably mounts on the lower side of the second gyroplane, the second gyroplane may send connection notification information to the first gyroplane to inform the first gyroplane that the second gyroplane is fixedly connected with the target cabin.

And S510, separating the first gyroplane from the target cabin when the second gyroplane is determined to be fixedly connected with the target cabin.

As an example, if the first gyroplane is fixedly connected to the target cabin through the cabin hanging device on the lower side, the second gyroplane is fixedly connected to the target cabin, specifically, the second gyroplane fixes the target cabin on the upper side of the second gyroplane through the cabin fixing device on the upper side, at this time, the first gyroplane is separated from the target cabin, that is, the cabin hanging fixing device on the lower side of the first gyroplane is released, and the first gyroplane is separated from the target cabin.

As another example, if the first gyroplane secures the target cabin to the upper side of the first gyroplane through the cabin securing device on the upper side, the second gyroplane and the target cabin are fixedly connected, specifically, the second gyroplane secures the target cabin to the lower side of the second gyroplane through the downloaded cabin mounting securing device, at this time, the first gyroplane is separated from the target cabin, specifically, the cabin securing device on the upper side of the first gyroplane is released, thereby achieving the separation of the first gyroplane from the target cabin.

S511, the first gyroplane transmits the separation notification information to the second gyroplane.

The first gyroplane may send a separation notification message to the second gyroplane to make the second gyroplane aware of the first gyroplane having been separated from the target cabin.

And S512, the first gyroplane falls to a second airport to supplement electric energy.

After the first rotorcraft has been separated from the target cabin, at which point it has completed the present flight mission, it may be dropped to a nearby airport, for example, to a dispatch center at a second airport for recharging, in preparation for the next flight mission.

S513, the second gyroplane flies according to the second route information when the first gyroplane is determined to be separated from the target cabin.

In this embodiment, when the second gyroplane is already fixed to the target cabin and the first gyroplane is already separated from the target cabin, the second gyroplane can continue to achieve cabin relay based on the acquired second route information and based on the flight, or, when the latter relay airport is the destination airport, directly land to the target airport and supplement electric energy at the corresponding airport.

According to the rotorcraft relay passenger carrying method, for the first rotorcraft which takes off from the first airport and is fixed with the separable target cabin, the first rotorcraft can fly according to the first route information received from the dispatching center of the first airport, when the distance between the first rotorcraft and the dispatching center of the second airport is smaller than the preset distance, a cabin relay request is sent to the dispatching center of the second airport, and a cabin relay response fed back by the dispatching center of the second airport is received, when the fact that the second rotorcraft to be relayed is fixedly connected with the target cabin is confirmed, the second rotorcraft is separated from the target cabin and falls to the second airport to supplement electric energy, and the second rotorcraft flies according to the second route information. In the technical scheme, the second gyroplane takes over the relay process of the first gyroplane bearing target cabin, the passenger cabin taken by the passenger does not need to fall to the ground, the purpose that the passenger always flies to the destination in the air in the passenger cabin taken by the passenger is achieved, and the flight efficiency and the user experience are improved.

Fig. 6 is a schematic structural diagram of a first embodiment of a rotorcraft relay passenger carrier provided by the present application. The rotorcraft relay passenger carrying device is applied to a dispatching center of an initial airport. Referring to fig. 6, the gyroplane relay passenger carrier may include:

an acquisition module 601 for acquiring a start airport and a destination airport of a passenger;

a determining module 602, configured to determine, according to the location information of the starting airport and the location information of the destination airport, a target flight route of a target passenger cabin where the passenger takes, and determine, according to airport information passed by the target flight route and maximum range information of the idle gyroplanes parked in each airport, route information of at least one relay airport among the target flight routes and target gyroplanes that need to be relayed by each relay airport;

a synchronizing module 603, configured to synchronize route information of the target gyroplane that needs to be relayed by each relay airport to a dispatch center in each relay airport.

The device provided in the embodiment of the present application may be used to perform the method embodiment described in fig. 4, and its implementation principle and technical effects are similar, and are not described herein again.

Fig. 7 is a schematic structural diagram of a second embodiment of a rotorcraft relay passenger carrier provided by the present application. The rotorcraft relay passenger carrying device is applied to a first rotorcraft sailing from a first airport, and a separable target cabin is fixed on the first rotorcraft. As shown in fig. 7, the gyroplane relay passenger carrier may include: a processing module 701, a transmitting module 702 and a receiving module 703.

Wherein, the processing module 701 is configured to fly according to the first route information received by the receiving module 703 from the dispatch center of the first airport;

a sending module 702, configured to send a cabin relay request to a dispatch center of a second airport when it is determined that a distance between the first gyroplane and the dispatch center of the second airport is less than a preset distance;

a receiving module 703, configured to receive a cabin relay response fed back by a dispatch center of the second airport, where the cabin relay response includes: identification of the second gyroplane to be relayed;

the processing module 701 is further configured to, when it is determined that the second gyroplane is fixedly connected to the target cabin, separate from the target cabin and drop to the second airport for supplementing electric energy.

In one possible design of the embodiment of the present application, the processing module 701 is further configured to establish a communication link with the second gyroplane according to the identifier of the second gyroplane;

the sending module 702 is further configured to send, to the second gyroplane through the communication link, real-time location information of the first gyroplane and a fixed connection manner of the target cabin and the first gyroplane.

In another possible design of the embodiment of the present application, the upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device;

the processing module 701 is configured to be separated from the target cabin, specifically:

the processing module 701 is specifically configured to release the cabin mounting fixture on the underside of the first gyroplane to separate the first gyroplane from the target cabin.

In yet another possible design of an embodiment of the present application, the upper side of each gyroplane is provided with a cabin attachment fixture, and the lower side of each gyroplane is provided with a cabin mounting fixture;

The processing module 701 is specifically configured to release the cabin fastening device on the upper side of the first gyroplane, so as to separate the first gyroplane from the target cabin.

The device provided in the embodiment of the present application may be used to implement the technical scheme of the first gyroplane in the embodiment of the method described in fig. 5, and its implementation principle and technical effect are similar, and are not described herein again.

Fig. 8 is a schematic structural view of a third embodiment of a rotorcraft relay passenger carrier provided by the present application. The rotorcraft relay passenger carrying device is applied to a second rotorcraft of a second airport. As shown in fig. 8, the gyroplane relay passenger carrier may include: a receiving module 801, an acquiring module 802 and a processing module 803.

The receiving module 801 is configured to receive relay indication information sent by a dispatch center of the second airport, where the relay indication information includes: the second route information and the identity of the first gyroplane to take over;

the acquiring module 802 is configured to acquire real-time position information of the first gyroplane and a fixed connection manner between a target cabin on the first gyroplane and the first gyroplane;

the processing module 803 is configured to fixedly connect to the target cabin according to the real-time position information of the first gyroplane and a fixed connection mode of the target cabin on the first gyroplane and the first gyroplane, and fly according to the second route information when it is determined that the first gyroplane is separated from the target cabin.

In one possible design of the embodiment of the present application, the processing module 803 is further configured to establish a communication link with the first gyroplane according to the identification of the first gyroplane;

the receiving module 801 is further configured to receive, through the communication link, real-time location information sent by the first gyroplane and a fixed connection manner between a target cabin on the first gyroplane and the first gyroplane;

the obtaining module 802 is specifically configured to obtain the real-time position information sent by the first gyroplane and received by the receiving module 801, and a fixed connection manner between a target cabin on the first gyroplane and the first gyroplane.

In another possible design of the embodiment of the present application, the processing module 803 is configured to, according to the real-time position information of the first gyroplane and a fixed connection manner between a target cabin on the first gyroplane and the first gyroplane, fixedly connect with the target cabin, specifically:

the processing module 803 is specifically configured to:

the processing module 803 is configured to determine, according to a fixed connection manner between the target cabin and the first gyroplane, a target positional relationship between the second gyroplane and the target cabin, specifically:

the processing module 803 is specifically configured to determine that the target cabin is loaded on the second gyroplane when the target cabin is mounted on the lower side of the first gyroplane through the cabin mounting fixing device on the lower side of the first gyroplane;

the processing module 803 is configured to be fixedly connected to the target cabin according to the real-time position information of the first gyroplane and the target position relationship, specifically:

the processing module 803 is specifically configured to fly to a position below the target cabin based on the target positional relationship according to the real-time positional information of the first gyroplane, and fix the target cabin above the second gyroplane through a cabin fixing device on the upper side of the second gyroplane.

the processing module 803 is specifically configured to determine that the target cabin is mounted below the second gyroplane when the target cabin is carried on the first gyroplane by a cabin fixing device on the upper side of the first gyroplane;

the processing module 803 is specifically configured to fly to above the target cabin based on the target positional relationship according to the real-time positional information of the first gyroplane, and fix the target cabin below the second gyroplane through the cabin mounting and fixing device at the lower side of the second gyroplane.

The device provided in the embodiment of the present application may be used to implement the technical scheme of the second gyroplane in the embodiment of the method shown in fig. 5, and its implementation principle and technical effect are similar, and are not described herein again.

It should be noted that, it should be understood that the division of the modules of the above apparatus is merely a division of a logic function, and may be fully or partially integrated into a physical entity or may be physically separated. And these modules may all be implemented in software in the form of calls by the processing element; or can be realized in hardware; the method can also be realized in a form of calling software by a processing element, and the method can be realized in a form of hardware by a part of modules. For example, the processing module may be a processing element that is set up separately, may be implemented in a chip of the above apparatus, or may be stored in a memory of the above apparatus in the form of program code, and may be called by a processing element of the above apparatus to execute the functions of the above determination module. The implementation of the other modules is similar. In addition, all or part of the modules can be integrated together or can be independently implemented. The processing element described herein may be an integrated circuit having signal processing capabilities. In implementation, each step of the above method or each module above may be implemented by an integrated logic circuit of hardware in a processor element or an instruction in a software form.

Fig. 9 is a schematic structural diagram of an airport dispatching center according to an embodiment of the present application. As shown in fig. 9, the airport dispatch center may include: the system comprises a processor 901, a memory 902, a transceiver 903 and a system bus 904, wherein the memory 902 and the transceiver 903 are connected with the processor 901 through the system bus 904 and are in communication with each other, the memory 902 is used for storing computer execution instructions, the transceiver 903 is used for communicating with other devices, and the technical scheme of the dispatching center of each airport in each embodiment is realized when the processor 901 executes the computer execution instructions.

Fig. 10 is a schematic structural view of a gyroplane according to an embodiment of the present application. As shown in fig. 10, the gyroplane may include: the technical solution of the first gyroplane or the second gyroplane in the above embodiment is implemented when the processor 1001 executes the computer execution instruction.

In fig. 9 and 10, the processor may be a general-purpose processor including a central processing unit CPU, a network processor (network processor, NP), and the like; but may also be a digital signal processor DSP, an application specific integrated circuit ASIC, a field programmable gate array FPGA or other programmable logic device, a discrete gate or transistor logic device, a discrete hardware component.

The memory may comprise random access memory (random access memory, RAM), read-only memory (RAM), and non-volatile memory (non-volatile memory), such as at least one disk memory.

Transceivers, i.e. communication interfaces, are used to enable communication between the database access arrangement and other devices, such as clients, read-write libraries and read-only libraries.

The system bus may be a peripheral component interconnect standard (peripheral component interconnect, PCI) bus or an extended industry standard architecture (extended industry standard architecture, EISA) bus, among others. The system bus may be classified into an address bus, a data bus, a control bus, and the like. For ease of illustration, the figures are shown with only one bold line, but not with only one bus or one type of bus.

Optionally, the embodiment of the present application further provides a computer readable storage medium, where computer executable instructions are stored, where the computer executable instructions when executed on a computer cause the computer to perform the solution of the method embodiment shown in fig. 4.

Embodiments of the present application also provide a computer-readable storage medium having stored therein computer-executable instructions that, when executed on a computer, cause the computer to perform the method of the first gyroplane or the second gyroplane as in the method embodiment of fig. 5 described above.

Optionally, the embodiment of the present application further provides a chip for executing the instruction, where the chip is configured to execute the scheme of the method embodiment shown in fig. 4.

The embodiment of the application also provides a chip for running the instruction, and the chip is used for executing the scheme of the first gyroplane or the second gyroplane in the embodiment of the method shown in the figure 5.

Embodiments of the present application also provide a computer program product comprising: computer instructions for implementing the solution of the method embodiment shown in fig. 4 described above when executed by a processor.

Embodiments of the present application also provide a computer program product comprising: computer instructions which, when executed by a processor, are configured to implement the solution of the first rotorcraft or the second rotorcraft in the embodiment of the method shown in fig. 5 described above.

In the present application, "at least one" means one or more, and "a plurality" means two or more. "and/or", describes an association relationship of an association object, and indicates that there may be three relationships, for example, a and/or B, and may indicate: a alone, a and B together, and B alone, wherein a, B may be singular or plural. The character "/" generally indicates that the front and rear associated objects are an "or" relationship; in the formula, the character "/" indicates that the front and rear associated objects are a "division" relationship. "at least one of" or the like means any combination of these items, including any combination of single item(s) or plural items(s).

It will be appreciated that the various numerical numbers referred to in the embodiments of the present application are merely for ease of description and are not intended to limit the scope of the embodiments of the present application. In the embodiments of the present application, the sequence number of each process does not mean the sequence of execution sequence, and the execution sequence of each process should be determined by its function and internal logic, and should not constitute any limitation on the implementation process of the embodiments of the present application.

Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the application disclosed herein. This application is intended to cover any adaptations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.

It is to be understood that the present disclosure is not limited to the precise arrangements and instrumentalities shown in the drawings, and that various modifications and changes may be effected without departing from the scope thereof. The scope of the present disclosure is limited only by the appended claims.

Claims

1. A method of rotorcraft relay passenger carrying for a first rotorcraft sailing from a first airport, the first rotorcraft having a detachable target cabin secured thereto, the method comprising:

when the second gyroplane is determined to be fixedly connected with the target cabin, the second gyroplane is separated from the target cabin and falls to the second airport to supplement electric energy;

the upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device;

if the first gyroplane is fixedly connected with the target cabin through the cabin mounting fixing device at the lower side, the second gyroplane is fixedly connected with the target cabin, and the method comprises the following steps: the second gyroplane secures the target cabin to an upper side of the second gyroplane by an upper side cabin securing device.

2. The method of claim 1, wherein after the receiving the cabin relay response fed back by the dispatch center of the second airport, the method further comprises:

3. The method of claim 1 or 2, wherein the separating from the target passenger compartment comprises:

4. The method according to claim 1 or 2, wherein if the first gyroplane secures the target cabin to the upper side of the first gyroplane by an upper side cabin securing device, the second gyroplane is fixedly connected to the target cabin, comprising: the second gyroplane fixes the target cabin on the lower side of the second gyroplane through a cabin mounting fixing device on the lower side;

said separating from said target passenger compartment comprising:

5. A method of relay passenger carrying for a gyroplane, for use with a second gyroplane parked at a second airport, the method comprising:

acquiring real-time position information of the first gyroplane, and fixedly connecting a target cabin on the first gyroplane with the first gyroplane; the upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device;

the fixed connection mode of the target cabin on the first rotorcraft and the first rotorcraft comprises the following steps: the target cabin is mounted on the lower side of the first gyroplane through a cabin mounting and fixing device on the lower side of the first gyroplane;

according to the real-time position information of the first gyroplane and the fixed connection mode of the target cabin on the first gyroplane and the first gyroplane, the first gyroplane is fixedly connected with the target cabin; fixedly connected with the target passenger cabin comprises: securing the target cabin to an upper side of the second gyroplane;

6. The method of claim 5, wherein the obtaining real-time location information of the first gyroplane and the manner of fixedly connecting the target cabin on the first gyroplane to the first gyroplane comprises:

7. The method according to claim 5 or 6, wherein the fixedly connecting the target cabin on the first gyroplane to the first gyroplane according to the real-time position information of the first gyroplane and the fixed connection mode of the target cabin and the first gyroplane comprises:

8. The method of claim 7, wherein the determining the target positional relationship of the second gyroplane and the target cabin according to the manner of the fixed connection of the target cabin and the first gyroplane comprises:

when the target cabin is mounted on the lower side of the first gyroplane through a cabin mounting fixing device on the lower side of the first gyroplane, determining that the target cabin is mounted on the upper side of the second gyroplane;

and fixing the target cabin on the upper side of the second gyroplane through a cabin fixing device on the upper side of the second gyroplane.

9. The method of claim 7, wherein the determining the target positional relationship of the second gyroplane and the target cabin according to the manner of the fixed connection of the target cabin and the first gyroplane comprises:

When the target cabin is borne on the upper side of the first gyroplane through a cabin fixing device on the upper side of the first gyroplane, determining that the target cabin is mounted below the second gyroplane;

and fixing the target cabin on the lower side of the second gyroplane through a cabin mounting and fixing device on the lower side of the second gyroplane.

10. A rotorcraft relay passenger method, applied to a dispatch center of an initial airport, comprising:

acquiring an initial airport and a destination airport of a passenger;

Synchronizing route information of target gyroplanes requiring relay for each relay airport to a dispatch center in each relay airport to cause a first gyroplane, which is flown from a first airport, to perform the method of claim 1 above, or to cause a second gyroplane, which is parked at a second airport, to perform the method of claim 5 above.

11. A gyroplane relay passenger carrier for use with a first gyroplane sailing from a first airport, the first gyroplane having a detachable target passenger compartment secured thereto, the device comprising: the device comprises a processing module, a sending module and a receiving module;

the processing module is further used for separating the second gyroplane from the target passenger cabin and landing the second gyroplane to the second airport for supplementing electric energy when the second gyroplane is determined to be fixedly connected with the target passenger cabin;

The upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device; if the first gyroplane is fixedly connected with the target cabin through the cabin mounting fixing device at the lower side, the second gyroplane is fixedly connected with the target cabin, specifically: the second gyroplane secures the target cabin to an upper side of the second gyroplane by an upper side cabin securing device.

12. A gyroplane relay passenger carrier for use with a second gyroplane parked at a second airport, the device comprising: the device comprises a receiving module, an acquisition module and a processing module;

the acquisition module is used for acquiring real-time position information of the first gyroplane and a fixed connection mode of a target cabin on the first gyroplane and the first gyroplane; the upper side of each gyroplane is provided with a cabin fixing device, and the lower side of each gyroplane is provided with a cabin mounting fixing device; the fixed connection mode of the target cabin on the first rotorcraft and the first rotorcraft is specifically as follows: the target cabin is mounted on the lower side of the first gyroplane through a cabin mounting and fixing device on the lower side of the first gyroplane;

The processing module is configured to, according to the real-time position information of the first gyroplane and a fixed connection mode of a target cabin on the first gyroplane with the first gyroplane, fixedly connect with the target cabin, and when determining that the first gyroplane is separated from the target cabin, fly according to the second route information, and fixedly connect with the target cabin, specifically: the target cabin is secured to an upper side of the second gyroplane.

13. A gyroplane relay passenger carrier device for use in a dispatch center at an origin airport, the device comprising:

A synchronizing module for synchronizing route information of target gyroplanes requiring relay for each relay airport to a dispatch center in each relay airport to cause a first gyroplane, which is flown from a first airport, to perform the method of claim 1 above, or to cause a second gyroplane, which is parked at a second airport, to perform the method of claim 5 above.

14. A gyroplane comprising a processor, a memory, a transceiver and a computer program stored on the memory and executable on the processor, wherein the processor implements the method of any of the preceding claims 1-4 when executing the program or the processor implements the method of any of the preceding claims 5-9 when executing the program.

15. An airport dispatch center comprising a processor, a memory, a transceiver and a computer program stored on the memory and executable on the processor, wherein the processor implements the method of claim 10 when executing the program.

16. A computer readable storage medium having stored therein computer executable instructions for implementing the method of any of the preceding claims 1-4 when executed by a processor, or for implementing the method of any of the preceding claims 5-9 when executed by a processor, or for implementing the method of claim 10 when executed by a processor.

17. A computer program product comprising computer instructions for implementing the method of any of the preceding claims 1-4 when executed by a processor, or for implementing the method of any of the preceding claims 5-9 when executed by a processor, or for implementing the method of claim 10 when executed by a processor.