CN112758313A

CN112758313A - Method, device and equipment for relay passenger carrying of gyroplane and storage medium

Info

Publication number: CN112758313A
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: 2021-05-07
Anticipated expiration: 2041-01-12
Also published as: CN112758313B

Abstract

The embodiment of the application provides a relay passenger carrying method, a relay passenger carrying device and a storage medium of a gyroplane, wherein the first gyroplane sailing from a first airport and fixed with a separable target passenger cabin on a machine body can fly according to first route information received from a dispatching center of the first airport, upon determining that the distance between the first rotorcraft and the dispatch center at the second airport is less than a preset distance, sending a cabin relay request to a dispatching center of a second airport, receiving a cabin relay response fed back by the dispatching center of the second airport, when the second gyroplane to be relayed is confirmed to be fixedly connected with the target cabin, the second gyroplane is separated from the target cabin, and landing to a second airport for supplementing electrical energy, while the second rotorcraft flies according to the second course information, therefore, the passenger cabin taken by the passengers is always in the air and flies to the destination, and the flying efficiency and the user experience are improved.

Description

Method, device and equipment for relay passenger carrying of gyroplane 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 relay passenger carrying of a gyroplane.

Background

With the progress of scientific technology and the necessity of clean energy development, the gyroplane gradually enters the visual field of people, has the characteristics of energy conservation, environmental protection, high efficiency and low energy consumption, simultaneously has low noise and vibration level and good riding comfort, realizes near zero emission, and is a real environment-friendly airplane.

Among the prior art, gyroplane mainly depends on the motor to drive the aircraft flight, and the electric power source of motor mainly is the battery, receives the influence of battery technology, and the full charge electric quantity of battery is limited, need in time charge when the battery electric quantity is not enough, therefore, it has certain effect in a plurality of fields such as short distance transportation, training pilot, experience flight.

In the process of implementing the invention, the inventor finds that at least the following problems exist in the prior art: because the range of a rotorcraft is greatly limited by the electric quantity of a battery, if the range of a passenger exceeds the maximum range of a single flight that can be supported by the battery in the rotorcraft, the rotorcraft needs to be landed midway and supplemented with electric energy, and flies to a destination after the battery is fully charged, which greatly reduces the flight efficiency and the riding experience of the passenger.

Disclosure of Invention

The embodiment of the application provides a relay passenger carrying method, device and equipment of a gyroplane and a storage medium, and aims to solve the problems that the existing gyroplane is low in flight efficiency and poor in passenger experience.

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

flying in accordance with first airline information received from a dispatch center at the first airport;

when the distance between the first gyroplane and a dispatching center of a second airport is determined to be smaller than a 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, wherein the cabin relay response comprises: an identification of a second rotorcraft to be relayed;

when it is determined that the second rotorcraft is fixedly connected with the target cabin, separating the second rotorcraft from the target cabin and landing the second rotorcraft 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 includes:

establishing a communication link with the second rotorcraft based on the identity of the second rotorcraft;

and sending 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.

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

if first gyroplane through the cabin mount fixing device of downside with target cabin fixed connection, then second gyroplane with target cabin fixed connection has included: the second rotorcraft fixes the target cabin on the upper side of the second rotorcraft through a cabin fixing device on the upper side;

the device is separated from the target passenger cabin and comprises:

releasing a cabin mount fixture on an underside of the first rotorcraft to detach the first rotorcraft from the target cabin.

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

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

the device is separated from the target passenger cabin and comprises:

releasing the cabin fixture on the upper side of the first rotorcraft to detach the first rotorcraft from the target cabin.

In a second aspect, an embodiment of the present application provides a method for relay passenger carrying of a rotorcraft, applied to a second rotorcraft parked at a second airport, the method including:

receiving relay indication information sent by a dispatching center of the second airport, wherein the relay indication information comprises: second airline information and an identification of a first rotorcraft to take over;

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;

fixedly connecting 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;

flying in accordance with the second course information upon determining that the first rotorcraft is detached from the target cabin.

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

establishing a communication link with the first rotorcraft based on the identity of the first rotorcraft;

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

In another possible design of the second aspect, the fixedly connecting the target cabin to the first rotorcraft according to the real-time position information of the first rotorcraft and the fixedly connecting manner of the target cabin to the first rotorcraft on the first rotorcraft comprises:

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

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

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

the determining a target positional relationship of the second rotorcraft with the target cabin according to the fixed connection of the target cabin with the first rotorcraft comprises:

determining that the target positional relationship is that the target cabin is loaded above the second rotorcraft when the target cabin is loaded on the underside of the first rotorcraft by a cabin loading fixture on the underside of the first rotorcraft;

according to real-time position information of first gyroplane, the target location relation, with target passenger cabin fixed connection includes:

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

the target cabin is fixed on the second rotorcraft by a cabin fixing device on the upper side of the second rotorcraft.

determining that the target positional relationship is that the target cabin is mounted below the second rotorcraft when the target cabin is carried above the first rotorcraft by a cabin fixture on an upper side of the first rotorcraft;

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

and fixing the target cabin below the second rotorcraft by a cabin mounting and fixing device on the lower side of the second rotorcraft.

In a third aspect, an embodiment of the present application provides a method for relay passenger carrying of a gyroplane, which is applied to a dispatch center at an origin airport, and the method includes:

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

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

determining at least one relay airport in the target flight route and route information of the target gyroplane needing relay at each relay airport according to the airport information through which the target flight route passes and the maximum range information of the no-load gyroplane parked in each airport;

and synchronizing the flight path information of the target gyroplanes needing to be relayed at each relay airport to a dispatching center in each relay airport.

In a fourth aspect, an embodiment of the present application provides a relay passenger carrying device for a rotorcraft, where the relay passenger carrying device is applied to a first rotorcraft that starts a flight from a first airport, and a separable target passenger cabin is fixed to the first rotorcraft, and the relay passenger carrying device includes: 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 a dispatching center of a 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;

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: an identification of a second rotorcraft to be relayed;

and the processing module is also used for separating the second gyroplane from the target 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 cabin.

In one possible design of the fourth aspect, the processing module is further configured to establish a communication link with the second rotorcraft based on the identification of the second rotorcraft;

and the sending module is also used for sending 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.

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

if first gyroplane through the passenger cabin mount fixture of downside with target passenger cabin fixed connection, then second gyroplane with target passenger cabin fixed connection has specifically been: the second rotorcraft fixes the target cabin on the upper side of the second rotorcraft through a cabin fixing device on the upper side;

the processing module is used for separating from the target passenger cabin, and specifically comprises:

the processing module is specifically configured to release a cabin mounting fixture on a lower side of the first rotorcraft to separate the first rotorcraft from the target cabin.

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

if first gyroplane will through the main cabin fixing device of upside with target main cabin is fixed the upside of first gyroplane, then second gyroplane with target main cabin fixed connection has specifically been: the second rotorcraft fixing 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 fixture on an upper side of the first rotorcraft to separate the first rotorcraft from the target cabin.

In a fifth aspect, an embodiment of the present application provides a relay passenger carrying device for a rotorcraft, which is applied to a second rotorcraft parked at a second airport, and the device includes: the device comprises a receiving module, an obtaining module and a processing module;

the receiving module is configured to receive relay indication information sent by a scheduling center of the second airport, where the relay indication information includes: second airline information and an identification of a first rotorcraft 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;

and the processing module is used for fixedly connecting 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, and flying according to the second airline 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 rotorcraft based on the identification of the first rotorcraft;

the receiving module is further used for receiving real-time position information sent by the first gyroplane and a fixed connection mode between a target cabin on the first gyroplane and the first gyroplane through the communication link;

the acquisition module is specifically used for acquiring the real-time position information that the receiving module received first gyroplane sent with the target cabin on the first gyroplane with the fixed connection mode of first gyroplane.

In another possible design of the fifth aspect, the processing module is configured to be fixedly connected to the target cabin according to the real-time position information of the first rotorcraft and a fixed connection manner between the target cabin on the first rotorcraft and the first rotorcraft, and specifically:

the processing module is specifically configured to:

the processing module is used for determining a target position relation between the second gyroplane and the target cabin according to a fixed connection mode between the target cabin and the first gyroplane, and specifically comprises the following steps:

the processing module is specifically configured to determine that the target location relationship is that the target cabin is loaded above the second rotorcraft when the target cabin is loaded on the underside of the first rotorcraft by a cabin-loading fixture on the underside of the first rotorcraft;

the processing module is used for being fixedly connected with the target cabin according to the real-time position information of the first gyroplane and the target position relation, and specifically comprises the following steps:

and the processing module is specifically used for flying to the lower part of the target cabin based on the target position relation according to the real-time position information of the first gyroplane, and fixing the target cabin on 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 location relationship is that the target cabin is mounted below the second rotorcraft when the target cabin is carried above the first rotorcraft by a cabin fixture on an upper side of the first rotorcraft;

the processing module is specifically used for flying to the upper part of the target cabin according to the real-time position information of the first gyroplane and based on the target position relation, and the target cabin is fixed below the second gyroplane through the cabin mounting and fixing device on the lower side of the second gyroplane.

In a sixth aspect, an embodiment of the present application provides a relay passenger carrying device for a rotorcraft, which is applied to a dispatch center at an airport, where the relay passenger carrying device includes:

the system comprises an acquisition module, a processing module and a processing module, wherein the acquisition module is used for acquiring an origin airport and a destination airport of passengers;

the determining module is used for determining a target flight route of a target passenger cabin taken by a passenger according to the position information of the starting airport and the position information of the target airport, and determining at least one relay airport in the target flight route and route information of the target gyroplane needing relay at each relay airport according to airport information through which the target flight route passes and the maximum route information of the no-load gyroplane parked in each airport;

and the synchronization module is used for synchronizing the flight path information of the target gyroplane needing relaying at each relay airport to a dispatching center in each relay airport.

In a seventh aspect, embodiments of the present application provide a rotorcraft 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 first aspect and possible designs when executing the program, or the processor implementing the method according to the second aspect and possible designs when executing the program.

In an eighth aspect, an embodiment of the present application provides an airport dispatch center, which includes a processor, a memory, a transceiver, and a computer program stored on the memory and executable on the processor, and when the processor executes the computer program, the processor implements the method according to the third aspect.

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

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

In an eleventh aspect, an embodiment of the present application provides a computer program product, where the computer program product includes: computer instructions for implementing the method as described in the first aspect and various possible designs as described above when executed by a processor; alternatively, the computer instructions, when executed by a processor, are for implementing a method as set forth in the second aspect and various possible designs above.

In a twelfth aspect, an embodiment of the present application provides a computer program product, where the computer program product includes: computer instructions for implementing the method according to the third aspect when executed by a processor.

According to the method, the device, the equipment and the storage medium for relay passenger carrying of the gyroplane, a dispatching center of an initial airport can determine a target flight path of a target passenger cabin where passengers are seated, at least one relay airport in the target flight path and route information of the target gyroplane needing relay at each relay airport according to the acquired position information of the initial airport and the position information of a target airport, synchronize the route information of the target gyroplane needing relay at each relay airport to the dispatching center in each relay airport, correspondingly, a first gyroplane which starts a flight from a first airport and is fixed with a separable target passenger cabin on a machine body can fly according to the first route information received from the dispatching center of the first airport, when the distance between the first gyroplane and the dispatching center of a second airport is determined to be smaller than the preset distance, and sending a cabin relay request to a dispatching center of a second airport, receiving a cabin relay response fed back by the dispatching center of the second airport, separating the second rotorcraft to be relayed from the target cabin and landing the second rotorcraft to the second airport for supplementing electric energy when the second rotorcraft is confirmed to be fixedly connected with the target cabin, and flying the second rotorcraft according to second airline information, so that the cabin taken by passengers is always in the air and flies to a destination, and the flying efficiency and the user experience are improved.

Drawings

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

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

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

FIG. 2B is another schematic illustration of the loading of the passenger compartment on the rotorcraft;

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

fig. 4 is a schematic flowchart of a first method for relay passenger carrying of a rotorcraft according to an embodiment of the present disclosure;

fig. 5 is an interaction diagram of a second method for relay passenger carrying of a rotorcraft according to an embodiment of the present application;

fig. 6 is a schematic structural view of a first relay passenger carrying device of a rotorcraft according to an embodiment of the present disclosure;

fig. 7 is a schematic structural view of a second example of a relay passenger carrying device of a rotorcraft according to the present application;

fig. 8 is a schematic structural view of a third embodiment of a relay passenger carrying device of a rotorcraft according to the present application;

fig. 9 is a schematic structural diagram of an airport dispatch center provided in an embodiment of the present application;

fig. 10 is a schematic structural diagram of a rotorcraft according to an embodiment of the present disclosure.

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

Detailed Description

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

With the continuous rising of the price of petroleum and the requirement of low-carbon economy, the trip mode of new energy is an important direction for the development of various industries due to low pollution and high efficiency. The gyroplane is a new energy travel mode gradually appearing in the visual field of people along with economic development.

Because the range of the existing rotorcraft is greatly limited by the electric quantity of the battery, if the range of a passenger exceeds the maximum range of a single pass which can be supported by the battery in the rotorcraft, the rotorcraft needs to land midway and supplement electric energy, and flies to a destination after the battery is fully charged, so that the flying efficiency and the riding experience of the passenger are greatly reduced.

Aiming at the problems, the technical idea process of the application is as follows: if the organism and the main cabin with current gyroplane set to separable structure to set up main cabin fixing device respectively at the upside and the downside of organism, and set up orientation module on the organism, make two organisms can realize the relay aloft, thereby make the main cabin that the passenger took fly aloft to the purpose airport all the time on the way flying, thereby avoided the gyroplane to need descend and carried out the problem of charging, solved the gyroplane and can not continuously fly, and the inefficiency that leads to and take the poor problem of experience.

Based on the technical concept, the embodiment of the application provides a relay passenger carrying method for gyroplanes, when a dispatching center of an origin airport acquires an origin airport and a target airport of passengers, a target flight path of a target passenger cabin where the passengers are to be seated, at least one relay airport in the target flight path and route information of the target gyroplane which needs to be relayed by each relay airport can be determined according to the position information of the origin airport and the position information of the target airport, and the route information of the target gyroplane which needs to be relayed by each relay airport is synchronized to the dispatching center in each relay airport, accordingly, for a first gyroplane which starts to sail from the first airport, the first gyroplane is fixed with a separable target passenger cabin, the first gyroplane can fly according to first route information received from the dispatching center of the first airport, when the distance between the first gyroplane and the dispatching center of a second airport is determined to be smaller than a preset distance, and sending a cabin relay request to a dispatching center of a second airport, receiving a cabin relay response fed back by the dispatching center of the second airport, separating the second rotorcraft to be relayed from the target cabin when the second rotorcraft is fixedly connected with the target cabin and landing the second rotorcraft to the second airport for supplementing electric energy, wherein the second rotorcraft flies according to second airline information, so that passengers fly to destinations in the air all the time in the passenger cabin, and the flying efficiency and the user experience are improved.

Fig. 1 is a schematic structural diagram of a rotorcraft according to an embodiment of the present disclosure. As shown in fig. 1, the rotorcraft may include: the device comprises a machine body 11, a cabin fixing device 12 arranged on the upper side of the machine body 11 and a 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 can be implemented by a steering engine, a stepping motor, a hook and the like, and are mainly used for fixing the target cabin and the body 11 together, so that the target cabin and the gyroplane are fixedly connected. It is understood that the embodiments of the present application do not limit the specific implementation of the cabin fixture 12 and the cabin-mounted fixture 13, which can be determined according to actual situations.

For example, the rotorcraft according to the embodiments of the present application may be an unmanned rotorcraft or a manned rotorcraft, and the present invention is not limited thereto. Fig. 1 is illustrated as an unmanned rotorcraft.

It is understood that the embodiments of the present application also do not limit the specific structure and implementation of the machine body, which may be designed according to practical application and will not be described herein.

Based on the above-described configuration of the rotorcraft shown in fig. 1, fig. 2A is a schematic view of the loading of the passenger compartment on the rotorcraft. Fig. 2B is another loading schematic of a passenger cabin on a rotorcraft. As is apparent from the rotorcraft shown in fig. 1, the rotorcraft may have the cabin fixed to the rotorcraft by the cabin fixing device 12 on the upper side of the body 11 to form the loading plan shown in fig. 2A, or may have the cabin fixed to the rotorcraft by the cabin mounting fixing device 13 on the lower side of the body 11 to form the loading plan shown in fig. 2B.

Based on the above schematic diagrams, fig. 3 is a schematic diagram of an architecture of a relay passenger carrying system of a gyroplane. As shown in fig. 3, the architecture diagram may include: the system comprises a plurality of airports, wherein each airport is provided with a dispatching center, and each dispatching center is used for dispatching and managing the gyroplanes parked in the airport.

In the architecture diagram shown in fig. 3, 4 airports, respectively, an airport a to an airport D are exemplarily shown, wherein the airport a is a starting airport of the target cabin, the airport D is a 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 number of airports in the relay passenger carrying system of the rotorcraft is not limited in the embodiments of the present application, and the number of the rotorcraft parked in each airport is also not limited, which may be determined according to an actual scenario, and is not described herein again. Alternatively, the rotorcraft may also be referred to as an electric aircraft, and is not limited thereto.

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

For example, assume that a gyroplane # 1 at airport a is fixed with the target passenger cabin at airport a. The specific fixing mode can be various, one mode is that the No. 1 gyroplane flies to the position of the target passenger cabin based on the indication of the dispatching center, and the passenger cabin mounting fixing device on the lower side of the No. 1 gyroplane is used for automatically and separably mounting the target passenger cabin to the lower side of the No. 1 gyroplane; another mode is that the staff utilizes the cabin handling device to carry the target cabin to the position of No. 1 gyroplane, then loads the upside of No. 1 gyroplane with the target cabin for the cabin fixing device of No. 1 gyroplane upside can be separable with the separable fixing in target cabin on No. 1 gyroplane, or, No. 1 gyroplane utilizes the cabin to carry fixing device of downside automatically can be separable with the separable carry in target cabin to No. 1 gyroplane downside. In this embodiment, the fixing manner of the No. 1 rotorcraft and the target cabin is not limited, and details thereof are not described herein.

In practical applications, passengers need to first safely ride into a target cabin before a number 1 rotor aircraft takes off in the target cabin.

For example, assuming that the passenger cabin of a passenger starting from the airport a is mounted below the gyroplane 1, and the gyroplane 1 takes off from the airport a, and flies to the upper space of the airport B, the gyroplane 2 sending out a relay from the airport B is fixedly connected with the target passenger cabin in a separable manner through the passenger cabin fixing device on the upper side, and notifies the gyroplane 1, and when the gyroplane 1 determines that the gyroplane 2 is fixedly connected with the target passenger cabin, the passenger cabin mounting fixing device on the lower side is released, the gyroplane is separated from the target passenger cabin, and the gyroplane descends to the airport B for charging. Correspondingly, the No. 2 gyroplane continues flying according to the acquired route information.

Similarly, when No. 2 gyroplanes fly to the upper space of the airport C, No. 3 gyroplanes, which send out the relay at the airport C, are detachably and fixedly connected with the target cabin through the cabin mounting and fixing device at the lower side, and notify No. 2 gyroplanes, and when No. 2 gyroplanes are determined to be fixedly connected with the target cabin, the cabin fixing device at the upper side is loosened, separated from the target cabin, and the gyroplanes land to the airport C for charging. Correspondingly, No. 3 gyroplanes continue to fly according to the received airline information, land at the D airport after flying to the D airport, and the passenger arrives purpose underground passenger cabin, and No. 3 gyroplanes charge at the D airport.

The relay passenger carrying flight of the gyroplane is completed through the process, passengers fly to the destination all the time in the air when taking the gyroplane, and the problems of low efficiency and poor riding experience caused by the fact that the gyroplane needs to be landed and charged due to insufficient electric power are avoided.

The following describes the technical solutions of the present application and how to solve the above technical problems with specific embodiments. The following several specific embodiments may be combined with each other, and details of the same or similar concepts or processes may not be repeated 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 method for relay passenger carrying of a rotorcraft according to an embodiment of the present application. The relay passenger carrying method of the gyroplane is applied to a dispatching center of an initial airport. As shown in fig. 4, the method for relay loading of a rotorcraft may include the steps of:

s401, obtaining an origin airport and a destination airport of the passenger.

In this embodiment, when a passenger at an origin airport needs to go to a destination airport, a staff at the origin airport may input both the origin airport and the destination airport of the passenger to a dispatch center at the origin airport, so that the dispatch center at the origin airport may acquire the origin airport and the destination airport of the passenger. It will be appreciated that the crew at the origin airport may enter the passenger's origin and destination locations into the dispatch center at the origin airport so that the dispatch center at the origin airport may automatically locate the origin airport based on the passenger's origin location and may also automatically locate the destination airport based on the passenger's destination location. The embodiments of the present application do not limit how the dispatch center at the origin airport acquires the origin airport and the destination airport of the passenger.

S402, determining a target flight path of a target passenger cabin where passengers take according to the position information of the starting airport and the position information of the target airport.

For example, the dispatch center at the origin airport may determine the heading of the rotorcraft departing from the origin airport and the target flight path upon arrival at the destination airport based on the location information at the origin airport and the location information at the destination airport.

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

S403, determining at least one relay airport in the target flight route and route information of the target gyroplane needing relay at each relay airport according to the airport information where the target flight route passes and the maximum flight route information of the unloaded gyroplane parked in each airport.

Optionally, the dispatch center at the starting airport may obtain airport information according to the route of the target flight route and information of the gyroplanes parked in each airport, for example, information that the target flight route passes through several airports, the space size of each airport, the number of unloaded gyroplanes parked in each airport, the maximum one-way flight when each unloaded gyroplane is fully powered, and the like, so that it may be determined that when the dispatch center at the starting airport passes through a certain airport, it is determined whether the maximum one-way flight in the airport is greater than the empty and fully powered gyroplane of the mileage required by the airport and a next adjacent airport, and if so, the airport may be used as a relay airport in the target flight route, and the route information of the target gyroplane of the relay airport that needs relay is determined.

In practical application, the dispatching center of the starting airport can determine a plurality of schemes, for example, the number of relay airports in a target flight route in a certain scheme is small, the range between some relay airports is far, the gyroplane with the largest one-way range is needed, and the number of times of relay in the air is relatively small; for another example, if the number of relay airports in the target flight path in a certain scheme is large, the range between some relay airports may be relatively short, and the maximum one-way range of the required gyroplane is relatively small but the number of relays in the air is large.

In this embodiment, the dispatch center at the origin airport may present multiple determined schemes for the staff to choose according to various factors such as cost and time effectiveness, which is not limited herein.

And S404, synchronizing the flight path information of the target gyroplanes needing to be relayed at each relay airport to a dispatching center in each relay airport.

In this embodiment, when the scheduling center of the starting airport determines all relay airports in the target flight route and route information of the target gyroplane that each relay airport needs to relay, the information may be synchronized to the scheduling center of each relay airport, so that when the gyroplane flies in the range of the corresponding relay airport and sends a cabin relay request to the scheduling center of the corresponding relay airport, the scheduling center of the corresponding relay airport may determine the gyroplane to be relayed according to the maximum one-way route information of the no-load gyroplane parked in the airport, and send the corresponding flight route to the gyroplane to be relayed, so that the gyroplane to be relayed flies based on the information.

According to the method for relay passenger carrying of the gyroplane, a dispatching center of a starting airport can determine a target flight route of a target passenger cabin where passengers take according to the obtained position information of the starting airport and the position information of a target airport of the passengers, then at least one relay airport in the target flight route and route information of the target gyroplane needing relay at each relay airport are determined according to the airport information where the target flight route passes and the maximum route information of the no-load gyroplane parked in each airport, and the route information of the target gyroplane needing relay at each relay airport is synchronized to the dispatching center in each relay airport. According to the technical scheme, at least one relay airport capable of relaying in the target flight route and route information of the target gyroplane needing relaying in each relay airport can be determined, and the route information is synchronized to the dispatching center of the corresponding relay airport, so that conditions are provided for realizing relay flight subsequently.

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

s501, the dispatching center of the first airport sends the first airline information to the first gyroplane.

The first airport may be any one of all airports except the destination airport in the target flight path, that is, the first airport may be an origin airport, and may also be any one relay airport in the target flight path. The first gyroplane may be a gyroplane parked in the first airport that meets a preset condition. The preset condition is that the first gyroplane is in an unloaded state, and the maximum flight range of the first gyroplane capable of supporting flight is larger than the flight range corresponding to the first airline information.

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

Optionally, the information of the rotorcraft may include whether the rotorcraft is unloaded, whether other flight tasks exist, maximum flight distance information that the rotorcraft has the remaining power to support flight, and the like.

As an example, if the first airport is the origin airport, the dispatch center at the first airport may send the first route information directly to the first rotorcraft after determining route information for each airport and determining the first rotorcraft 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 a first gyroplane to be relayed according to first flight information synchronized from the dispatch center of the origin airport and information of all gyroplanes parked in the first airport, when receiving a cabin relay request transmitted from gyroplanes flying from other airports, and then transmit 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 separable target cabin secured to its body prior to receiving first airline information sent by a dispatch center at the first airport, the first rotorcraft may fly based on the first airline information when receiving the first airline information. For example, if the first rotorcraft is a rotorcraft that is starting at an origin airport, it may receive the first route information after the target cabin is secured to the airframe.

As another example, if a first rotorcraft has no target cabin fixed to its body when receiving first flight path information, the first rotorcraft may first need to be fixed to the target cabin and then fly based on the first flight path information when determining that the target cabin is fixed only by the first rotorcraft. For example, when the first rotorcraft is a to-be-relayed rotorcraft dispatched from a relay airport, the first rotorcraft may first obtain the first route information and then fly to the air to fix the target 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, sending 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 to a second airport from the first airport based on the first route information, and 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 shown to have flown to the coverage area of the second airport, at this time, 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 the gyroplane meeting the preset condition to carry out cabin relay. The preset condition is similar to that in S501, and is not described herein.

Optionally, the specific value of the preset distance may be determined by the flight altitude of the rotorcraft and the transceiving capacity of the rotorcraft, which is not described herein again.

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

Optionally, when the dispatch center of the second airport receives the cabin relay request, the dispatch center of the second airport determines a target airport of the target cabin, then determines second flight path information that the gyroplane taking off from the second airport and relaying needs to fly according to the flight path information synchronized from the starting airport, and then determines a second gyroplane meeting preset conditions according to the flight path of the second flight path information and the information of the plurality of gyroplanes parked in the second airport, that is, the second gyroplane is in an idle state, and the maximum flight path where the remaining electric quantity of the second gyroplane can support flying is greater than the flight path corresponding to the second flight path information.

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

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

S506, the dispatching center of the second airport sends relay indication information to the second gyroplane, and the relay indication information comprises: the second route information and an identification of the first rotorcraft to take over.

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

S507, the second gyroplane obtains 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.

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

Specifically, the first rotorcraft sends a link establishment request to the second rotorcraft, and 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 at the second airport, the second rotorcraft may determine an identifier of the first rotorcraft to be taken over, and then establish a communication link with the first rotorcraft according to the identifier of the first rotorcraft.

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

Further, after the communication link is established between the first rotorcraft and the second rotorcraft, the first rotorcraft may send the real-time location information of the first rotorcraft and the fixed connection mode of the target cabin with the first rotorcraft to the second rotorcraft through the communication link, and correspondingly, the second rotorcraft may receive the real-time location information sent by the first rotorcraft and the fixed connection mode of the target cabin on the first rotorcraft with the first rotorcraft through the communication link.

In practical application, Global Positioning System (GPS) modules are arranged on the first rotorcraft and the second rotorcraft, so that the positions of the first rotorcraft and the second rotorcraft can be acquired in real time, and the first rotorcraft and the second rotorcraft can transmit the positions of the first rotorcraft and the second rotorcraft to the second rotorcraft in real time through position sharing or in a manner that the first rotorcraft transmits the positions of the first rotorcraft and the second rotorcraft to enable the second rotorcraft to acquire real-time position information of the first rotorcraft.

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 practice, since the location where the GPS module is located on each rotorcraft is fixed, the real-time location information for each rotorcraft is actually the real-time location information for the GPS module. Furthermore, as can be seen from the above-mentioned embodiments shown in fig. 1 to 3, there may be two types of fixing positions of each rotorcraft to the target cabin, but the fixing manner of the two rotorcraft performing relay to the target cabin cannot be the same.

For example, if the target cabin is fixed to the upper side of the first rotorcraft, the target cabin needs to be mounted and fixed to the lower side of the second rotorcraft when the second rotorcraft is in relay, or if the target cabin is mounted and fixed to the lower side of the first rotorcraft, the target cabin needs to be fixed to the upper side of the second rotorcraft when the second rotorcraft is in relay.

Based on this, the second gyroplane can firstly confirm the target position relation of second gyroplane and target main cabin according to the fixed connection mode of target main cabin and first gyroplane, then according to real-time position information, the target position relation of first gyroplane, with target main cabin fixed connection again.

Specifically, as can be seen from the above-mentioned embodiments shown in fig. 1 to 3, the upper side of each rotorcraft is provided with a cabin fixing device, and the lower side of each rotorcraft is provided with a cabin mounting fixing device; thus, determining the target positional relationship of the second rotorcraft to the target cabin, based on the fixed connection of the target cabin to the first rotorcraft, can be accomplished in two ways:

a first possible implementation: when the target cabin is mounted on the lower side of the first rotorcraft through the cabin mounting fixture on the lower side of the first rotorcraft, determining that the target position relationship between the second rotorcraft and the target cabin is to be that the target cabin is mounted on the second rotorcraft.

Correspondingly, the second gyroplane then flies to the below in target main cabin according to the real-time position information of first gyroplane based on the target position relation of confirming, and then through the main cabin fixing device of second gyroplane upside, fixes target main cabin on the second gyroplane.

A second possible implementation: when the target cabin is carried on the upper surface of the first rotorcraft by a cabin fixing device on the upper side of the first rotorcraft, the target position relation between the second rotorcraft and the target cabin is determined to be that the target cabin is mounted below the second rotorcraft.

Correspondingly, the second gyroplane then flies to the top in target main cabin according to the real-time position information of first gyroplane based on the target position relation, then through the main cabin mount fixture of second gyroplane downside, fixes the below at the second gyroplane in the target main cabin.

And S509, when the second gyroplane is fixedly connected with the target passenger cabin, sending connection notification information to the first gyroplane.

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

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

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

As another example, if the first rotorcraft fixes the target cabin on the upper side of the first rotorcraft through the cabin fixture on the upper side, the second rotorcraft is already 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 fixture, and at this time, the first rotorcraft is separated from the target cabin, specifically, the cabin fixture on the upper side of the first rotorcraft is loosened, thereby realizing the separation of the first rotorcraft from the target cabin.

S511, the first rotorcraft sends a separation notification message to the second rotorcraft.

The first rotorcraft may send a detachment notification message to the second rotorcraft so that the second rotorcraft knows that the first rotorcraft has detached from the target cabin.

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

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

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

In this embodiment, when the second gyroplane has been fixed to the target cabin and the first gyroplane has been separated from the target cabin, the second gyroplane may fly to the upper space of the next relay airport based on the acquired second route information to continue to implement cabin relay based on flight, or may directly land to the target airport and supplement electric energy at the corresponding airport when the next relay airport is the target airport.

According to the rotorcraft relay passenger carrying method provided by the embodiment of the application, for a first rotorcraft which starts a flight from a first airport and is fixed with a separable target passenger cabin on a body, the first rotorcraft can fly according to first route information received from a dispatching center of the first airport, when the fact that the distance between the first rotorcraft and the dispatching center of a second airport is smaller than a preset distance is determined, a passenger cabin relay request is sent to the dispatching center of the second airport, passenger 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 passenger cabin is confirmed, the second rotorcraft is separated from the target passenger cabin and landed to the second airport to supplement electric energy, and the second rotorcraft flies according to second route information. In the technical scheme, the second gyroplane takes over the relay process that the first gyroplane bears the target cabin, the passenger cabin taken by the passenger does not need to land on 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 flying efficiency and the user experience are improved.

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

an obtaining module 601, configured to obtain an origin airport and a destination airport of a passenger;

a determining module 602, configured to determine a target flight path of a target passenger cabin where a passenger rides according to the position information of the starting airport and the position information of the target airport, and determine at least one relay airport in the target flight path and route information of a target rotorcraft that needs to relay at each relay airport according to airport information where the target flight path passes and maximum route information of a no-load rotorcraft parked in each airport;

and a synchronization module 603, configured to synchronize flight path information of the target gyroplane that needs to be relayed at each relay airport to a dispatch center in each relay airport.

The apparatus provided in the embodiment of the present application may be configured to execute the method embodiment described in fig. 4, and the implementation principle and the technical effect are similar, which are not described herein again.

Fig. 7 is a schematic structural view of a relay passenger carrying device of a rotorcraft according to a second embodiment of the present disclosure. The relay passenger carrying device of the gyroplane is applied to a first gyroplane which is started from a first airport, and a separable target passenger cabin is fixed on the first gyroplane. As shown in fig. 7, the relay passenger carrying device for rotorcraft may include: a processing module 701, a sending module 702 and a receiving module 703.

The processing module 701 is configured to fly according to first route information received by the receiving module 703 from a 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: an identification of a second rotorcraft to be relayed;

and the processing module 701 is further configured to detach the second rotorcraft from the target cabin and land the second rotorcraft to the second airport for supplementing electric energy when it is determined that the second rotorcraft is fixedly connected with the target cabin.

In one possible design of this embodiment of the present application, processing module 701 is further configured to establish a communication link with the second rotorcraft based on the identification of the second rotorcraft;

sending module 702 is further configured to send real-time location information of the first rotorcraft and a fixed connection between the target cabin and the first rotorcraft to the second rotorcraft via the communication link.

In another possible design of the embodiment of the application, 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 processing module 701 is configured to separate from the target cabin, and specifically includes:

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

In yet another possible design of the embodiment of the present application, a cabin fixing device is provided on an upper side of each rotorcraft, and a cabin mounting fixing device is provided on a lower side of each rotorcraft;

processing module 701 is specifically configured to release the cabin fixture on the upper side of the first rotorcraft to separate the first rotorcraft from the target cabin.

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

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

The receiving module 801 is configured to receive relay indication information sent by a scheduling center of the second airport, where the relay indication information includes: second airline information and an identification of a first rotorcraft to take over;

the obtaining module 802 is configured to obtain real-time position information of the first rotorcraft and a fixed connection manner between a target cabin on the first rotorcraft and the first rotorcraft;

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

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

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

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

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

the processing module 803 is specifically configured to:

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

the processing module 803, in particular, is configured to determine that the target location relationship is that the target cabin is loaded above the second rotorcraft when the target cabin is loaded on the underside of the first rotorcraft by a cabin-loading fixture on the underside of the first rotorcraft;

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

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

the processing module 803, specifically configured to determine that the target location relationship is that the target cabin is mounted below the second rotorcraft when the target cabin is carried above the first rotorcraft by a cabin fixture above the first rotorcraft;

the processing module 803 is specifically configured to fly to the top of the target cabin based on the target position relationship according to the real-time position information of the first rotorcraft, and fix the target cabin below the second rotorcraft by the cabin mounting and fixing device on the lower side of the second rotorcraft.

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

It should be noted that the division of the modules of the above apparatus is only a logical division, and the actual implementation may be wholly or partially integrated into one physical entity, or may be physically separated. And these modules can be realized in the form of software called by processing element; or may be implemented entirely in hardware; and part of the modules can be realized in the form of calling software by the processing element, and part of the modules can be realized in the form of hardware. For example, the processing module may be a separate processing element, or may be integrated into a chip of the apparatus, or may be stored in a memory of the apparatus in the form of program code, and a processing element of the apparatus calls and executes the functions of the above determination module. Other modules are implemented similarly. In addition, all or part of the modules can be integrated together or can be independently realized. 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 the form of software.

Fig. 9 is a schematic structural diagram of an airport dispatch center provided in 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 complete mutual communication, the memory 902 is used for storing computer execution instructions, the transceiver 903 is used for communicating with other equipment, and the technical scheme of the dispatch center of each airport in the above embodiments is realized when the processor 901 executes the computer execution instructions.

Fig. 10 is a schematic structural diagram of a rotorcraft according to an embodiment of the present disclosure. As shown in fig. 10, the rotorcraft may include: the system comprises a processor 1001, a memory 1002, a transceiver 1003 and a system bus 1004, wherein the memory 1002 and the transceiver 1003 are connected with the processor 1001 through the system bus 1004 and are used for achieving mutual communication, the memory 1002 is used for storing computer execution instructions, the transceiver 1003 is used for communicating with other equipment, and the processor 1001 executes the computer execution instructions to achieve the technical scheme of the first gyroplane or the second gyroplane in the embodiment.

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

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

The transceiver, i.e. the communication interface, is used to enable communication between the database access means and other devices, such as clients, read-write libraries and read-only libraries.

The system bus may be a Peripheral Component Interconnect (PCI) bus, an Extended Industry Standard Architecture (EISA) bus, or the like. The system bus may be divided into an address bus, a data bus, a control bus, and the like. For ease of illustration, only one thick line is shown, but this does not mean that there is only one bus or one type of bus.

Optionally, an embodiment of the present application further provides a computer-readable storage medium, where computer-executable instructions are stored in the computer-readable storage medium, and when the computer-executable instructions are executed on a computer, the computer is caused to execute the scheme of the method embodiment shown in fig. 4.

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

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

The embodiment of the present application further provides a chip for executing instructions, where the chip is used to execute the scheme of the first rotorcraft or the scheme of the second rotorcraft in the method embodiment shown in fig. 5.

An embodiment of the present application further provides a computer program product, where the computer program product includes: computer instructions which, when executed by a processor, are adapted to implement aspects of the method embodiment of fig. 4 described above.

An embodiment of the present application further provides a computer program product, where the computer program product includes: computer instructions that when executed by a processor are adapted to implement aspects of the first rotorcraft or the second rotorcraft in the method embodiment of fig. 5 described above.

In the present application, "at least one" means one or more, "a plurality" means two or more. "and/or" describes the association relationship of the associated objects, meaning that there may be three relationships, e.g., a and/or B, which may mean: a exists alone, A and B exist simultaneously, and B exists alone, wherein A and B can be singular or plural. The character "/" generally indicates that the former and latter associated objects are in an "or" relationship; in the formula, the character "/" indicates that the preceding and following related objects are in a relationship of "division". "at least one of the following" or similar expressions refer to any combination of these items, including any combination of the singular or plural items.

It is to be understood that the various numerical references referred to in the embodiments of the present application are merely for descriptive convenience and are not intended to limit the scope of the embodiments of the present application. In the embodiment of the present application, the sequence numbers of the above-mentioned processes do not mean the execution sequence, and the execution sequence of each process should be determined by its function and inherent logic, and should not constitute any limitation to the implementation process of the embodiment of the present application.

Other embodiments of the present 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 variations, 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 will be understood that the present disclosure is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present disclosure is limited only by the appended claims.

Claims

1. A method of relaying a load on a rotorcraft for a first rotorcraft when starting from a first airport, the first rotorcraft having a separable target cabin secured thereto, the method comprising:

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

3. Method according to claim 1 or 2, characterized in that the upper side of each rotorcraft is provided with cabin fixtures and the lower side of each rotorcraft is provided with cabin mounting fixtures;

the device is separated from the target passenger cabin and comprises:

4. Method according to claim 1 or 2, characterized in that the upper side of each rotorcraft is provided with cabin fixtures and the lower side of each rotorcraft is provided with cabin mounting fixtures;

the device is separated from the target passenger cabin and comprises:

5. A method of relaying a load carried by a rotorcraft for use by a second rotorcraft parked at a second airport, the method comprising:

6. The method of claim 5, wherein said obtaining real-time position information of the first rotorcraft and a fixed connection of a target cabin on the first rotorcraft to the first rotorcraft comprises:

7. The method of claim 5 or 6, wherein said fixedly coupling a target cabin on the first rotorcraft to the target cabin based on real-time position information of the first rotorcraft and a manner of fixedly coupling the target cabin to the first rotorcraft comprises:

8. The method of claim 7, wherein an upper side of each rotorcraft is provided with a cabin fixture and a lower side of each rotorcraft is provided with a cabin-mounting fixture;

9. The method of claim 7, wherein an upper side of each rotorcraft is provided with a cabin fixture and a lower side of each rotorcraft is provided with a cabin-mounting fixture;

10. A relay passenger carrying method of a gyroplane is applied to a dispatching center of an initial airport, and is characterized by comprising the following steps:

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

11. A rotorcraft relay passenger carrying device for use with a first rotorcraft when starting from a first airport, wherein a separable target passenger compartment is secured to the first rotorcraft, the device comprising: the device comprises a processing module, a sending module and a receiving module;

12. A rotorcraft relay passenger carrying arrangement for a second rotorcraft parked at a second airport, the arrangement comprising: the device comprises a receiving module, an obtaining module and a processing module;

13. A rotorcraft relay passenger carrying device applied to a dispatching center of an origin airport, characterized in that the device comprises:

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

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 when executing the program implements the method of claim 10.

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

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