CN214986157U - Staying unmanned aerial vehicle's receive and release cabin device - Google Patents
Staying unmanned aerial vehicle's receive and release cabin device Download PDFInfo
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- CN214986157U CN214986157U CN202122417299.9U CN202122417299U CN214986157U CN 214986157 U CN214986157 U CN 214986157U CN 202122417299 U CN202122417299 U CN 202122417299U CN 214986157 U CN214986157 U CN 214986157U
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- unmanned aerial
- aerial vehicle
- cabin
- lifting platform
- retractable
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Abstract
The utility model relates to a cabin retracting device for mooring an unmanned aerial vehicle, which comprises a cabin retracting body and a lifting platform; the lifting platform is arranged in the accommodating space of the retraction cabin body in a lifting manner; at least one locking mechanism is arranged on the lifting platform to lock the mooring unmanned aerial vehicle parked on the lifting platform. The utility model discloses a set up the kayser structure on lift platform, when mooring unmanned aerial vehicle parks on lift platform, through kayser mechanism locking mooring unmanned aerial vehicle's position, make it in the transportation on the highway section of jolting, can not take place to rock, the condition of collision.
Description
Technical Field
The utility model relates to an aircraft technical field especially relates to a staying unmanned aerial vehicle's cabin device that receive and releases.
Background
A tethered drone is a drone that is developing rapidly today. Because the flight and control of the tethered unmanned aerial vehicle require high voltage and large current to be loaded, most tethered unmanned aerial vehicles are not equipped with power supply units themselves, or the power supply of their power supply units is very small. Typically, tethered drones rely on one or more cables to connect to and provide the amount of power required for endurance to the ground power supply system. Therefore, the tethered drone always drags cables during flight, and the tethered drone is named accordingly.
And the technology of receive and release of mooring unmanned aerial vehicle is the important component part of mooring unmanned aerial vehicle technique, plays important guarantee effect to mooring unmanned aerial vehicle's take off and land and park protection etc.. And the unmanned aerial vehicle's of mooring winding and unwinding devices can't guarantee the stability of mooring unmanned aerial vehicle in the transportation among the prior art, very easily leads to mooring unmanned aerial vehicle's rocking in the highway section of jolting, collides with even, leads to mooring unmanned aerial vehicle's the condition of damage to take place.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that a staying unmanned aerial vehicle's receive and release cabin device is provided, through the kayser structure that sets up on lift platform, realize staying unmanned aerial vehicle's fixed, avoided the highway section of jolting, it takes place to rock the condition of colliding with to stay unmanned aerial vehicle and takes place.
In order to solve or improve above-mentioned technical problem to a certain extent, according to the utility model discloses an aspect provides a staying unmanned aerial vehicle's cabin device that receive and releases, include: the retractable cabin comprises a retractable cabin body and a lifting platform;
the lifting platform is arranged in the accommodating space of the retractable cabin body in a lifting manner;
at least one locking mechanism is arranged on the lifting platform to lock the mooring unmanned aerial vehicle parked on the lifting platform.
In some embodiments, the latch mechanism includes a base, a first connecting rod, a ram, and a handle;
wherein the base is fixedly connected to the lifting platform;
the first connecting rod and the handle are both hinged to the base, and the first connecting rod is hinged to the handle;
the pressure head set up in the one end of head rod is used for compressing tightly tie unmanned aerial vehicle.
In some embodiments, the latch mechanism further comprises a second connecting rod, and two ends of the second connecting rod are respectively hinged to the handle and the base so as to realize the connection between the handle and the base.
In some embodiments, the ram is provided with an arcuate recess to match the landing gear of the tethered drone.
In some embodiments, the stowage compartment arrangement of the tethered drone further comprises: and the at least two oppositely arranged lifting mechanisms are arranged in the accommodating space of the retractable cabin body and are connected to the lifting platform.
In some embodiments, the lift mechanism comprises: a guide rail, a slide block and a bracket;
one end of the guide rail is fixedly connected to the retraction cabin body;
the sliding block is connected with the guide rail and can slide along the length direction of the guide rail;
the bracket is connected with the sliding block, and the lifting platform is connected with the bracket.
In some embodiments, the stowage compartment device of the tethered drone further comprises an elastic member disposed between the lift platform and the support.
In some embodiments, the lifting mechanism further comprises a first driving device connected to the slider to drive the slider to slide along the length direction of the guide rail.
In some embodiments, the stowage compartment body is provided with a lid that slides open and closed.
In some embodiments, the hatch comprises a hatch body, a slide rail and a second driving device;
the sliding rail is fixedly connected to the retraction cabin body;
the hatch cover body is connected to the sliding rail in a sliding manner;
the second driving device is connected to the hatch cover body or the sliding rail and drives the hatch cover body to slide along the sliding rail so as to open and close the hatch cover.
Compared with the prior art, the utility model obvious advantage and beneficial effect have. Borrow by above-mentioned technical scheme, the utility model relates to a staying unmanned aerial vehicle's cabin device that receive and releases can reach considerable technical progress nature and practicality to have the wide use value in industry, it has following advantage at least:
firstly, a clamping and locking structure is arranged on a lifting platform, when the mooring unmanned aerial vehicle is parked on the lifting platform, the position of the mooring unmanned aerial vehicle is locked through the clamping and locking structure, so that the mooring unmanned aerial vehicle cannot shake or collide during transportation of a bumpy road section;
after the mooring unmanned aerial vehicle is parked at the designated position of the lifting platform, a pressure head of the locking mechanism presses the landing gear of the mooring unmanned aerial vehicle by pressing the handle, and meanwhile, two hinged points of the handle and the base are in the same straight line with the hinged point of the first connecting rod and the handle, so that the locking mechanism is in a dead point state, and the locking mechanism can be prevented from being loosened in the bumping process;
thirdly, between lift platform and elevating system's support, set up the elastic component to play the effect of buffering when mooring unmanned aerial vehicle descends, prevent that mooring unmanned aerial vehicle from landing hard, avoid mooring unmanned aerial vehicle's impact.
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical means of the present invention more clearly understood, the present invention may be implemented according to the content of the description, and in order to make the above and other objects, features, and advantages of the present invention more obvious and understandable, the following preferred embodiments are described in detail with reference to the accompanying drawings.
Drawings
Fig. 1 is a schematic structural view of a cabin retracting device of a tethered unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic structural view of a cabin retracting device of a tethered unmanned aerial vehicle according to another embodiment of the present invention;
fig. 3 is the utility model discloses a local enlarged structure schematic diagram of cabin device that receive and releases of mooring unmanned aerial vehicle.
[ notation ] to show
Mooring the unmanned aerial vehicle;
2: a cabin retracting device for mooring the unmanned aerial vehicle;
20: a retraction cabin body;
21: a lifting platform;
210: cable hole
22: a latch mechanism;
220: a base;
221: a first connecting rod;
222: a pressure head;
223: a handle;
224: a first hinge point;
225: a second hinge point;
226: a third hinge point;
227: a fourth hinge point;
23: a lifting mechanism;
230: a guide rail;
231: a slider;
232: a support;
24: an elastic member;
25: a hatch cover;
250: a hatch body;
251: a slide rail;
252: a second driving device.
Detailed Description
To further illustrate the technical means and effects of the present invention for achieving the objectives of the present invention, the following detailed description is provided with reference to the accompanying drawings and preferred embodiments for the specific embodiments and effects of the retractable cabin device for mooring an unmanned aerial vehicle according to the present invention.
The embodiment of the utility model provides a staying unmanned aerial vehicle 1's receive and release cabin device 2. As shown in fig. 1 and 2, the folding cabin comprises a folding cabin body 20 and a lifting platform 21.
Wherein, the lifting platform 21 is arranged in the accommodating space of the cabin body 20 in a lifting manner. As shown in fig. 1, when the tethered unmanned aerial vehicle 1 takes off or lands, the lifting platform 21 is lifted to the opening of the retractable cabin body 20, so as to facilitate the taking off or landing of the tethered unmanned aerial vehicle 1. After mooring unmanned aerial vehicle 1 descends at lift platform 21, as shown in fig. 2, lift platform 21 descends to the accommodation space who receive and releases cabin body 20 in to realize mooring unmanned aerial vehicle 1's recovery and deposit.
In order to guarantee the stability of mooring unmanned aerial vehicle 1 in the transportation, prevent to appear because of the condition that shaking of mooring unmanned aerial vehicle 1 that the road surface jolts and leads to colliding with. As shown in fig. 1 and 2, at least one latching mechanism 22 is provided on the lifting platform 21. After the captive unmanned aerial vehicle 1 stops at the designated position of the lifting platform 21, the captive unmanned aerial vehicle 1 is locked by the locking mechanism 22 and stably stops on the lifting platform 21.
In one embodiment, as shown in FIG. 3, the latch mechanism 22 includes a base 220, a first link 221, a ram 222, and a handle 223.
The base 220 is fixedly connected to the lifting platform 21, the first connecting rod 221 and the handle 223 are both hinged to the base 220, the first connecting rod 221 and the handle 223 are hinged to each other, and the pressure head 222 is arranged at one end of the first connecting rod 221. When the driving handle 223 moves downwards, the handle 223 drives the end of the first connecting rod 221 provided with the pressing head 222 to move downwards, so that the pressing head 222 abuts against the tethered drone 1.
In one embodiment, the latch mechanism 22 is further provided with a second connecting rod (not shown), and both ends of the second connecting rod are respectively hinged to the base 220 and the handle 223, so as to realize the hinge connection between the handle 223 and the base 220.
Specifically, as shown in fig. 3, a first connecting rod 221 is hinged to the base 220 through a first hinge point 224, a handle 223 is hinged to the first connecting rod 221 through a second hinge point 225, one end of the second connecting rod is hinged to the handle 223 through a third hinge point 226, and the other end of the second connecting rod is hinged to the base 220 through a fourth hinge point 227. When mooring unmanned aerial vehicle 1 parks behind the assigned position of lift platform 21, make pressure head 222 support on mooring unmanned aerial vehicle 1's undercarriage through pressing down handle 223, realize fixed to unmanned aerial vehicle. When handle 223 is pressed down, when second pin joint 225, third pin joint 226 and fourth pin joint 227 are located the collinear, latch mechanism 22 is in the dead point state, and at this moment, when on the road of jolting, the ascending effort that mooring unmanned aerial vehicle 1 was used in on pressure head 222 can't make latch mechanism 22 unblock, and then guarantees the stability of latch mechanism 22 locking state.
In an embodiment, as shown in fig. 3, an arc-shaped groove is provided on the pressing head 222, and the arc-shaped groove matches with the shape of the landing gear of the tethered drone 1, so as to ensure the firmness of the locking of the tethered drone 1.
Further, the ram 222 is made of rubber to prevent the ram 222 from wearing the tethered drone 1.
In an embodiment, as shown in fig. 1 and fig. 2, in order to realize the lifting of the lifting platform 21, the cabin retracting device 2 of the tethered unmanned aerial vehicle further includes at least two lifting mechanisms 23 arranged oppositely, and the lifting mechanisms 23 are arranged in the accommodating space of the cabin retracting body 20 and connected to the lifting platform 21.
Specifically, the lifting mechanism 23 includes a guide rail 230, a slider 231, and a bracket 232. Wherein, one end of the guide rail 230 is fixedly connected to the retraction cabin body 20, more specifically, the guide rail 230 is vertically arranged, and the other end is connected to the bottom of the retraction cabin body 20. The slider 231 is coupled to the guide rail 230 and can slide along the length direction of the guide rail 230. The bracket 232 is fixedly connected to the slider 231, and the lifting platform 21 is connected to the bracket 232. The elevating platform 21 is further elevated by the elevating mechanism 23.
Further, the lifting mechanism 23 is further provided with a first driving device (not shown in the figure), which is connected to the slider 231 to drive the slider 231 to slide along the length direction of the slide rail 251.
Preferably, the first drive means is a motor.
In one embodiment, the pod body 20 is further provided with a slidably openable hatch 25 to open and close the pod body 20.
Further, the hatch 25 includes a hatch body 250, a slide rail 251, and a second driving device 252. The sliding rails 251 are fixedly installed at the top end of the storage compartment body 20, and the cover body 250 is slidably connected to the sliding rails 251. The second driving device 252 is connected to the hatch body 250 or the slide rail 251 to drive the hatch body 250 to slide along the slide, so as to open and close the hatch 25.
Preferably, the second driving device 252 is a motor.
In an embodiment, in order to prevent the occurrence of a situation in which the impact is too large due to hard landing when the tethered drone 1 lands on the lifting platform 21, resulting in damage to the tethered drone 1, an elastic member 24 is further provided between the lifting platform 21 and the support 232.
Wherein, the elastic member 24 may be a shock absorber with a certain damping, or may be an elastic member such as a spring, rubber or silica gel, but the present invention is not limited thereto.
Since the cable will always follow the tethered drone 1, in order to avoid tangling of the cable and ensure that the cable has the correct outlet direction, the lifting platform 21 is further provided with a cable hole 210 and a wire guide (not shown in the figure) arranged below the cable hole 210, and the cable passes through the cable hole 210 and the wire guide and is connected to the tethered drone 1.
Preferably, the cable may be an aircraft mooring cable comprising two alloy wires and one optical fiber wire having characteristics of high tensile strength, flexibility, coilable recovery, high voltage resistance and high current resistance, and a single mode optical fiber core may be used for communication.
Further, the cabin retracting device 2 further comprises a positioning member (not shown in the figure) for positioning the tethered unmanned aerial vehicle 1 during takeoff, return voyage, hovering and following of the tethered unmanned aerial vehicle 1, and the positioning member enables the tethered unmanned aerial vehicle to be parked at the designated position of the lifting platform 21. In a preferred embodiment, the locating member is mounted within the pod body 20.
Further, the positioning means comprises a differential GPS locator (not shown in the figures) for acquiring information of the relative position of the tethered drone 1 and said lifting platform 21, including data of the lifting platform 21 in relation to the central positioning coordinates, so as to help control the tethered drone 1 to be precisely parked on the lifting platform 21.
The retractable cabin device of the mooring unmanned aerial vehicle has the advantages that the clamping lock structure is arranged on the lifting platform, so that when the mooring unmanned aerial vehicle is parked on the lifting platform, the position of the mooring unmanned aerial vehicle is locked through the clamping lock structure, and the mooring unmanned aerial vehicle cannot shake or collide during the transportation process of a bumpy road section; after the mooring unmanned aerial vehicle is parked at the designated position of the lifting platform, the pressure head of the locking mechanism is enabled to press the landing gear of the mooring unmanned aerial vehicle by pressing the handle, and meanwhile, two hinge points of the handle and the base are in the same straight line with the hinge point of the first connecting rod and the handle, so that the locking mechanism is in a dead point state, and the locking mechanism can be prevented from being loosened in the bumping process; between lift platform and elevating system's support, set up the elastic component to play the effect of buffering when mooring unmanned aerial vehicle descends, prevent that mooring unmanned aerial vehicle from landing hard, avoid the impact to mooring unmanned aerial vehicle.
The above description is only a preferred embodiment of the present invention, and the present invention is not limited to the above embodiments, and although the present invention has been disclosed with the preferred embodiments, it is not limited to the present invention, and any skilled person in the art can make some modifications or equivalent embodiments without departing from the scope of the present invention, but all the technical matters of the present invention are within the scope of the present invention.
Claims (10)
1. A cabin retracting device for mooring an unmanned aerial vehicle is characterized by comprising a cabin retracting body and a lifting platform;
the lifting platform is arranged in the accommodating space of the retractable cabin body in a lifting manner;
at least one locking mechanism is arranged on the lifting platform to lock the mooring unmanned aerial vehicle parked on the lifting platform.
2. The stowage compartment apparatus of the tethered drone of claim 1, wherein the latch mechanism comprises a base, a first connecting rod, a ram, and a handle;
wherein the base is fixedly connected to the lifting platform;
the first connecting rod and the handle are both hinged to the base, and the first connecting rod is hinged to the handle;
the pressure head set up in the one end of head rod is used for compressing tightly tie unmanned aerial vehicle.
3. The retractable cabin apparatus of a tethered drone of claim 2,
the clamping and locking mechanism further comprises a second connecting rod, and two ends of the second connecting rod are respectively hinged to the handle and the base so as to realize the connection of the handle and the base.
4. The retractable cabin apparatus of a tethered drone of claim 2 or 3, wherein said ram is provided with an arcuate groove to match the landing gear of the tethered drone.
5. The retractable cabin apparatus of a tethered drone of claim 1, further comprising: and the at least two oppositely arranged lifting mechanisms are arranged in the accommodating space of the retractable cabin body and are connected to the lifting platform.
6. The retractable cabin apparatus of a tethered drone of claim 5, wherein said lifting mechanism comprises: a guide rail, a slide block and a bracket;
one end of the guide rail is fixedly connected to the retraction cabin body;
the sliding block is connected with the guide rail and can slide along the length direction of the guide rail;
the bracket is connected with the sliding block, and the lifting platform is connected with the bracket.
7. The retractable cabin apparatus of a tethered drone of claim 6, further comprising an elastic member disposed between the lift platform and the support.
8. The retractable cabin apparatus of a tethered drone of claim 6 or 7 wherein said lift mechanism further comprises a first drive means connected to said slider to drive said slider to slide along the length of said guide rail.
9. The retractable cabin apparatus of a tethered unmanned aerial vehicle of claim 8 wherein said retractable cabin body is provided with a slidably openable and closable hatch.
10. The retractable hatch apparatus of the tethered drone of claim 9, wherein the hatch comprises a hatch body, slide rails and a second drive means;
the sliding rail is fixedly connected to the retraction cabin body;
the hatch cover body is connected to the sliding rail in a sliding manner;
the second driving device is connected to the hatch cover body or the sliding rail and drives the hatch cover body to slide along the sliding rail so as to open and close the hatch cover.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122417299.9U CN214986157U (en) | 2021-10-08 | 2021-10-08 | Staying unmanned aerial vehicle's receive and release cabin device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122417299.9U CN214986157U (en) | 2021-10-08 | 2021-10-08 | Staying unmanned aerial vehicle's receive and release cabin device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986157U true CN214986157U (en) | 2021-12-03 |
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|---|---|---|---|
| CN202122417299.9U Active CN214986157U (en) | 2021-10-08 | 2021-10-08 | Staying unmanned aerial vehicle's receive and release cabin device |
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- 2021-10-08 CN CN202122417299.9U patent/CN214986157U/en active Active
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