CN113859093A - Integrated unmanned aerial vehicle transportation launching device - Google Patents
Integrated unmanned aerial vehicle transportation launching device Download PDFInfo
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- CN113859093A CN113859093A CN202111257073.5A CN202111257073A CN113859093A CN 113859093 A CN113859093 A CN 113859093A CN 202111257073 A CN202111257073 A CN 202111257073A CN 113859093 A CN113859093 A CN 113859093A
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- 230000007306 turnover Effects 0.000 claims abstract description 32
- 230000007246 mechanism Effects 0.000 claims abstract description 20
- 230000010354 integration Effects 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 abstract description 7
- 238000000034 method Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 230000003137 locomotive effect Effects 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
- B60S9/00—Ground-engaging vehicle fittings for supporting, lifting, or manoeuvring the vehicle, wholly or in part, e.g. built-in jacks
- B60S9/02—Ground-engaging vehicle fittings for supporting, lifting, or manoeuvring the vehicle, wholly or in part, e.g. built-in jacks for only lifting or supporting
- B60S9/10—Ground-engaging vehicle fittings for supporting, lifting, or manoeuvring the vehicle, wholly or in part, e.g. built-in jacks for only lifting or supporting by fluid pressure
- B60S9/12—Ground-engaging vehicle fittings for supporting, lifting, or manoeuvring the vehicle, wholly or in part, e.g. built-in jacks for only lifting or supporting by fluid pressure of telescopic type
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
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- Aviation & Aerospace Engineering (AREA)
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The application relates to an integrated unmanned aerial vehicle transportation launching device, which belongs to the technical field of aviation and comprises a transport vehicle and a transportation launching box; the transport vehicle comprises a walking vehicle chassis and a traction vehicle head; a hydraulic turnover mechanism is arranged between the two ends of the transportation launching box and the chassis of the walking vehicle, and a launching frame is arranged on the launching platform; the transportation launching box comprises a box body with a lateral opening and a launching platform, and the launching platform is rotatably connected with the inside of the box body through a vertically arranged rotating upright post; the box with rotate and be provided with flexible push-and-pull device between the stand, flexible push-and-pull device one end is articulated mutually with the box, flexible push-and-pull device's the other end is articulated mutually with the rotation stand, when flexible push-and-pull device is elongated, thereby it rotates to rotate the stand and drive launch platform and rotate this application to the side direction opening direction of box and have can once transport many unmanned aerial vehicles and launcher and can realize that the scene expandes fast and remove and receive, thereby satisfy the requirement of unmanned aerial vehicle quick, efficient transportation and transmission.
Description
Technical Field
The application relates to the field of aeronautical technologies, in particular to an integrated unmanned aerial vehicle transportation and launching device.
Background
A drone is broadly a military aircraft that is targeted for shooting training. The aircraft simulates the aircrafts of enemy army or incoming missiles during military exercises or weapon missions by utilizing remote control or preset flight paths and modes, provides imaginary targets and shooting opportunities for various artillery or missile systems, and belongs to one type of unmanned planes.
At present, in the unmanned flight guarantee process, two transportation and emission modes are mainly adopted: the other is that unmanned aerial vehicle and launcher transport alone, and many unmanned aerial vehicles of unmanned aerial vehicle transport vechicle and launcher transport vechicle all can once transport and the launcher. In the mode, a fixed connection relation does not exist between the launching rack and the transport vehicle in the using process, the launching rack needs to be temporarily fixed on a launching site, and after a task is executed, the launching rack cannot be quickly and accurately positioned and retracted.
The other type is that a transport vechicle loads a launching cradle and an unmanned aerial vehicle, and the transport vechicle is self-propelled or pull-type, and this kind of use mode conveying efficiency is low, only is applicable to and carries out closely flight guarantee task.
Disclosure of Invention
For satisfying the requirement of quick, the efficient transportation of unmanned aerial vehicle and transmission, the integration unmanned aerial vehicle transportation emitter that can once transport many unmanned aerial vehicles and launcher and can realize that the scene expandes fast and remove and receive is now designed.
The application provides a pair of integration unmanned aerial vehicle transportation emitter adopts following technical scheme:
an integrated unmanned aerial vehicle transportation launching device comprises a transport vehicle and a transportation launching box;
the transport vehicle comprises a walking vehicle chassis and a traction vehicle head positioned at the front end of the walking vehicle chassis;
the transport emission box is movably arranged on the chassis of the walking vehicle, a hydraulic turnover mechanism is arranged between two ends of the transport emission box and the chassis of the walking vehicle, and the transport emission box moves towards the lateral direction of the chassis of the walking vehicle and falls to the lateral outer side of the chassis of the walking vehicle through the hydraulic turnover mechanism;
the launching platform is provided with a launching frame;
the transportation launching box comprises a box body with a lateral opening and a launching platform tiled on the bottom wall in the box body, the launching platform is rotatably connected with the inside of the box body through a rotating upright post which is vertically arranged, and the launching platform can rotate along with the rotating upright post so as to rotate out of the lateral opening of the box body;
and when the telescopic push-pull device extends, the rotating stand column rotates to drive the launching platform to rotate towards the side opening direction of the box body.
Through adopting above-mentioned technical scheme, after integrated unmanned aerial vehicle transportation emitter arrived to appointed place, drive hydraulic pressure upset mechanism will transport the transmission case and unload to the subaerial of walking vehicle chassis side direction. When the transportation launching box unloads to subaerial, start flexible push-and-pull device, roll out the side direction opening of launching platform from the box, make the launcher on the launching platform be located the outside of box, can directly launch unmanned aerial vehicle directly from the launcher.
Optionally, telescopic hydraulic support legs are arranged at four corners of the chassis of the walking vehicle.
Through adopting above-mentioned technical scheme, when telescopic hydraulic support leg's length extension, telescopic hydraulic support leg's bottom and ground looks butt to increase the stability under the walking vehicle chassis parking state, guarantee that unmanned aerial vehicle is difficult for taking place to remove at the in-process transport vechicle of transmission.
Optionally, the number of the transportation launching boxes is two, and when the transportation launching boxes are all located on the chassis of the walking vehicle, the transportation launching boxes are arranged from bottom to top.
Through adopting above-mentioned technical scheme, through the quantity that increases the transportation emission case, further increase the unmanned aerial vehicle's that integrated unmanned aerial vehicle transportation emitter can load quantity.
Optionally, the openings of the two transportation launching boxes face in opposite directions, and when the two transportation launching boxes move towards the chassis of the walking vehicle laterally, the moving directions of the two transportation launching boxes are opposite.
Through adopting above-mentioned technical scheme, can the lateral space of rational utilization walking vehicle chassis, when two transportation launching boxes fall on subaerial, one of them falls on the ground of walking vehicle chassis left side, and another falls on the ground of walking vehicle chassis right side.
Optionally, a power supply device is arranged on the chassis of the walking vehicle.
Through adopting above-mentioned technical scheme, set up power supply device on the vehicle chassis of walking to corresponding power can in time be supplied, need not be in extra external power source.
Optionally, a plurality of stay cables are further arranged between the top of the rotating upright column and the launching platform.
Through adopting above-mentioned technical scheme, thereby can hold the launching platform through the suspension cable, make the launching platform when changeing out to the box outside, increase the anti bending capability of launching platform, make it difficult to take place the bending downwards.
Optionally, the hydraulic turnover mechanism includes a turnover rocker arm, one end of the turnover rocker arm is hinged to the transport launch box, the other end of the turnover rocker arm is hinged to the chassis of the traveling vehicle, a main turnover hydraulic telescopic push-pull device is arranged between the turnover rocker arm and the chassis of the traveling vehicle, one end of the main turnover hydraulic telescopic push-pull device is hinged to the turnover rocker arm, and the other end of the main turnover hydraulic telescopic push-pull device is hinged to the chassis of the traveling vehicle.
Through adopting above-mentioned technical scheme, when the flexible push-and-pull device of main upset hydraulic pressure extends, the flexible push-and-pull device of main upset hydraulic pressure promotes the upset rocking arm and rotates, thereby drives the transportation transmission case along with the rotation of upset rocking arm and removes to the side direction of walking vehicle chassis, until the transportation transmission case falls on walking vehicle chassis side direction subaerial.
Optionally, an auxiliary overturning hydraulic telescopic push-pull device is arranged between the overturning rocker arm and the transportation launching box, one end of the auxiliary overturning hydraulic telescopic push-pull device is hinged to the overturning rocker arm, and the other end of the auxiliary overturning hydraulic telescopic push-pull device is hinged to the transportation launching box.
Through adopting above-mentioned technical scheme, through setting up the flexible push-pull device of vice upset hydraulic pressure, when the transportation launching box was driven by the upset rocking arm, the flexible push-pull device of vice upset hydraulic pressure extends in step, guarantees that the transportation launching box keeps a vertical state, reduces the condition that the in-process that the transportation launching box removed appears acutely rocking.
Optionally, a storage box is further arranged on the chassis of the walking vehicle.
Through adopting above-mentioned technical scheme, required instrument when can launching unmanned aerial vehicle is put into the inside of bin.
In summary, the present application includes at least one of the following beneficial technical effects:
1. after the integrated unmanned aerial vehicle transportation launching device arrives at a specified place, the hydraulic overturning mechanism is driven to unload the transportation launching box onto the ground in the lateral direction of the chassis of the walking vehicle. When the transport launch box is unloaded onto the ground, the telescopic push-pull device is started, the launch platform is rotated out from the lateral opening of the box body, so that the launch frame on the launch platform is positioned on the outer side of the box body, and the unmanned aerial vehicle can be launched directly from the launch frame;
2. the quantity of transportation launching box is two, can the lateral space of rational utilization walking vehicle chassis, when two transportation launching boxes fall on subaerial, one of them falls on the ground of walking vehicle chassis left side, and another falls on the ground of walking vehicle chassis right side.
Drawings
Fig. 1 is a schematic structural diagram of an integrated unmanned aerial vehicle transportation launching device according to a first embodiment of the present application;
fig. 2 is a schematic structural diagram of the integrated unmanned aerial vehicle transportation launching device in a transportation launching box unloading state according to the first embodiment of the application;
FIG. 3 is a schematic view of a connection structure between a hydraulic overturning structure and a chassis and a transport launching box of a walking vehicle in the first embodiment of the application;
FIG. 4 is a schematic structural view of a transport launch box according to a first embodiment of the present application in an unfolded state;
FIG. 5 is a partial enlarged view of portion A of FIG. 4;
fig. 6 is a schematic structural diagram of a transport vehicle according to a first embodiment of the present application;
fig. 7 is a schematic structural diagram of an integrated unmanned aerial vehicle transportation launching device according to a second embodiment of the present application;
fig. 8 is a schematic structural diagram of the integrated unmanned aerial vehicle transportation launching device in a transportation launching box unloading state in the second embodiment of the present application.
Description of reference numerals: 1. a transport vehicle; 11. a chassis of a walking vehicle; 111. a telescopic hydraulic support leg; 12. towing the locomotive; 2. transporting the launch box; 21. a box body; 211. a lateral opening; 22. a launch platform; 23. rotating the upright post; 231. an extension portion; 24. a pushing hydraulic cylinder; 25. a stay cable; 26. a launcher; 3. a hydraulic turnover mechanism; 31. turning over the rocker arm; 32. a main overturning hydraulic cylinder; 33. an auxiliary overturning hydraulic cylinder; 4. a hydraulic station; 5. a power supply station; 6. a storage box.
Detailed Description
The present application is described in further detail below with reference to figures 1-8.
The first embodiment is as follows:
the embodiment of the application discloses integration unmanned aerial vehicle transportation emitter.
Referring to fig. 1 and 2, the integrated unmanned aerial vehicle transportation launching device comprises a transport vehicle 1 and a transportation launching box 2 for storing the unmanned aerial vehicle. The transport vehicle 1 comprises a walking vehicle chassis 11 and a traction vehicle head 12 positioned at the front end of the walking vehicle chassis 11, and the traction vehicle head 12 is fixedly connected with the walking vehicle chassis 11 so as to drive the walking vehicle chassis 11 to move through the traction vehicle head 12. The transport pod 2 is loaded above the chassis 11 of the walking vehicle.
The whole transportation launching box 2 is of a rectangular body structure. The longitudinal direction of the transport box 2 is set from the front end to the rear end of the chassis 11 of the walking vehicle. The one end that transportation emission case 2 orientation was pull locomotive 12 is the front end of transportation emission case 2, and the one end that transportation emission case 2 deviates from and pulls locomotive 12 is the rear end of transportation emission case 2. Hydraulic turnover mechanisms 3 are arranged between the front end and the rear end of the transportation launching box 2 and the chassis 11 of the walking vehicle, and the hydraulic turnover mechanisms 3 at the front end and the rear end of the transportation launching box 2 are oppositely arranged. The transport pod 2 can thus be unloaded from the chassis 11 of the walking vehicle onto the ground laterally of the chassis 11 of the walking vehicle by means of the hydraulic tilting mechanism 3.
Referring to fig. 2 and 3, in the embodiment of the present application, the hydraulic turnover mechanism 3 is exemplified by the hydraulic turnover mechanism 3 located at the rear end of the transportation launching box 2. The hydraulic tilting mechanism 3 comprises a tilting rocker arm 31 and a main tilting hydraulic cylinder 32 between the transport pod 2 and the chassis 11 of the travelling vehicle. The tilting rocker 31 is triangular. One corner of the turnover rocker arm 31 is hinged with the middle position of the top end of the rear end wall plate of the transportation launching box 2, and the other corner is hinged with the chassis 11 of the walking vehicle. One end of the main turning hydraulic cylinder 32 is hinged with the chassis 11 of the walking vehicle, and the other end of the main turning hydraulic cylinder 32 is hinged with the rest angle of the turning rocker arm 31. The connecting lines of the hinge point between the main turning hydraulic cylinder 32 and the walking vehicle chassis 11, the hinge point between the main turning hydraulic cylinder 32 and the turning rocker arm 31 and the hinge point between the turning rocker arm 31 and the walking vehicle chassis 11 are a triangle.
When the main roll-over hydraulic cylinder 32 is activated, the main roll-over hydraulic cylinder 32 pushes the roll-over swing arm 31, so that the roll-over swing arm 31 rolls over upward at the hinge point of the roll-over swing arm 31 and the chassis 11 of the traveling vehicle. The transport launching box 2 is driven to move towards the lateral direction of the chassis of the walking vehicle along with the upward overturning of the overturning rocker arm 31 until the transport launching box 2 is completely unloaded onto the ground at the lateral direction of the chassis 11 of the walking vehicle.
The structure of the hydraulic turnover mechanism 3 positioned at the front end of the transport launching box 2 is the same as that of the hydraulic turnover mechanism 3 positioned at the rear end of the transport launching box 2, and the difference is that the turnover rocker arm 31 is connected with the front end wall plate of the transport launching box 2.
An auxiliary overturning hydraulic cylinder 33 is further arranged between the end face wall plate of the transportation launching box 2 and the overturning rocker arm 31, one end of the auxiliary overturning hydraulic cylinder 33 is hinged with the transportation launching box 2, and the other end of the auxiliary overturning hydraulic cylinder is hinged with the overturning rocker arm 31. When the transportation launching box 2 is unloaded to the process of the lateral ground of the chassis 11 of the walking vehicle, the length of the auxiliary overturning hydraulic cylinder 33 is synchronously extended along with the movement of the transportation launching box 2, so that the transportation launching box 2 is ensured to be always in a vertical stable state, and the severe shaking of the transportation launching box 2 in the moving process is avoided.
Referring to fig. 2 and 4, the transport launch box 2 comprises a box body 21 with a lateral opening 211 on one side, the lateral opening of the box body 21 facing in the direction in which the transport launch box 2 is moved by the hydraulic tilting mechanism 3. The inside bottom that is located box 21 is provided with the launching platform 22 of tiling at the bottom wallboard of box 21, and the one end that launching platform 22 is located the box 21 rear end is provided with the rotation stand 23 of vertical setting towards side direction opening 211 one side of box 21, rotates stand 23 and rotates the inside of connecting at box 21, and welded fastening rotates between stand 23 and the launching platform 22. When the rotating column 23 rotates, the launching platform 22 rotates synchronously with the rotation of the rotating column 23 and can rotate out of the lateral opening of the box 21 to the outside of the box 21.
Referring to fig. 4 and 5, the side wall of the rotating column 23 is provided with an extending portion 231 extending outward, and the extending portion 231 is integrally formed with the rotating column 23. A pushing hydraulic cylinder 24 is arranged between the rear end wall plate of the box body 21 and the rotating upright post 23, and the pushing hydraulic cylinder 24 is arranged on one side of the rotating upright post 23 departing from the lateral opening 211 of the box body 21. One end of the pushing hydraulic cylinder 24 is hinged to the rear end wall plate of the box 21, and the other end of the pushing hydraulic cylinder 24 is hinged to one end of the extending part 231, which is far away from the rotating upright 23. When the pushing hydraulic cylinder 24 starts to extend, the pushing hydraulic cylinder 24 pushes the rotating upright 23 to rotate, and the rotating upright 23 rotates to drive the launching platform 22 to rotate towards the lateral opening 211 of the box body 21 and rotate out of the lateral opening 211 of the box body 21.
In order to ensure that the launching platform 22 can rotate out of the interior of the box 21, one end face of the launching platform 22 facing the front end wall plate of the box 21 is an arc-shaped face.
Referring to fig. 4, a stay cable 25 is disposed between the top of the rotating column 23 and the edge of the launching platform 22 facing the lateral opening 211 of the box 21 and between the top of the rotating column and the edge of the launching platform 22 facing the rear end of the box 21, one end of the stay cable 25 is fixedly connected with the launching platform 22, and the other end of the stay cable 25 is fixedly connected with the rotating column 23.
The number of the stay cables 25 on one side edge of the launch platform 22 facing the lateral opening 211 of the tank 21 is plural and is arranged at intervals along one side edge of the launch platform 22 facing the lateral opening 211 of the tank 21. The number of the stay cables 25 between the rear end edge of the launching platform 22 facing the box body 21 and the rotating post 23 is one. The connection point of the stay cable 25 and the launching platform 22 is located at the side of the rear end edge of the launching platform 22 away from the rotating upright 23.
The resistance to deformation of the launch platform 22 at locations away from the rotating post 23 can be increased by the stay cables 25, making the launch platform 22 less susceptible to complete deformation.
A plurality of launchers 26 are installed on the surface of the launching platform 22 at intervals along the length direction of the launching platform 22, and the launchers 26 are used for loading and launching the unmanned aerial vehicle. When the launching platform 22 is rotated from the inside of the casing 21, the launcher 26 on the launching platform 22 is also moved to the outside of the casing 21.
Referring to fig. 5, for the stability of walking vehicle chassis 11 when guaranteeing unmanned aerial vehicle transmission, be located walking vehicle chassis 11's four corners department and install the telescopic hydraulic support leg 111 of vertical setting, when telescopic hydraulic support leg 111 extends, telescopic hydraulic support leg 111's bottom can the butt on walking vehicle chassis 11 stop position subaerial.
The hydraulic station 4 and the power supply station 5 are arranged on the bottom end surface of the walking vehicle chassis 11, and the hydraulic station 4 and the power supply station 5 can provide required hydraulic power and electric power for the main overturning hydraulic cylinder 32, the auxiliary overturning hydraulic cylinder 33, the pushing hydraulic cylinder 24 and the telescopic hydraulic support legs 111.
The bottom surface that is located walking vehicle chassis 11 still is provided with bin 6, and bin 6 is used for storing the required instrument when unmanned aerial vehicle launches.
The implementation principle of the integrated unmanned aerial vehicle transportation transmitting device of the embodiment of the application is as follows: after the integrated unmanned aerial vehicle transportation launching device arrives at a designated place, the telescopic hydraulic support legs 111 at the four corners of the chassis 11 of the walking vehicle are started firstly, so that the telescopic hydraulic support legs 111 are abutted to the ground. The main and sub-tipping hydraulic cylinders 32 and 33 of the hydraulic tipping mechanism are driven, so that the transport pod 2 is smoothly dropped onto the ground in the lateral direction of the chassis 11 of the traveling vehicle. When the transportation launching box 2 unloads to the ground, start propelling movement pneumatic cylinder 24, roll out launching platform 22 from the side direction opening of box 21, make the launcher 26 on the launching platform 22 be located the outside of box 21, can directly launch unmanned aerial vehicle directly from launcher 26.
Example two:
the embodiment of the application discloses integration unmanned aerial vehicle transportation emitter.
Referring to fig. 7 and 8, the difference between the second embodiment and the first embodiment is: the number of the transport pods 2 is two. When the transport pods 2 are moved above the chassis 11 of the traveling vehicle, the two transport pods 2 are arranged from bottom to top.
The lateral openings 211 on the body 21 of the two transport pods 2 face opposite. When the transport pod 2 is dropped onto the traveling vehicle chassis 11 laterally on the ground, the lateral opening 211 of the case body 21 moves toward the transport pod 2 on the left side of the traveling vehicle chassis 11 in the left direction of the traveling vehicle chassis 11, and the lateral opening 211 of the case body 21 moves toward the transport pod 2 on the right side of the traveling vehicle chassis 11 in the right direction of the traveling vehicle chassis 11.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (9)
1. The utility model provides an integration unmanned aerial vehicle transportation emitter which characterized in that: comprises a transport vehicle (1) and a transport launching box (2);
the transport vehicle (1) comprises a walking vehicle chassis (11) and a traction vehicle head (12) positioned at the front end of the walking vehicle chassis (11);
the transportation launching box (2) is movably arranged on the walking vehicle chassis (11), a hydraulic turnover mechanism (3) is arranged between two ends of the transportation launching box (2) and the walking vehicle chassis (11), and the transportation launching box (2) moves towards the lateral direction of the walking vehicle chassis (11) and falls to the lateral outer side of the walking vehicle chassis (11) through the hydraulic turnover mechanism (3);
a launching rack (26) is arranged on the launching platform (22);
the transportation launching box (2) comprises a box body (21) with a lateral opening (211) and a launching platform (22) tiled on the bottom wall of the interior of the box body (21), wherein the launching platform (22) is rotatably connected with the interior of the box body (21) through a vertically arranged rotating upright post (23), and the launching platform (22) can rotate along with the rotating upright post (23) so as to rotate out of the lateral opening (211) of the box body (21);
a telescopic push-pull device is arranged between the box body (21) and the rotating upright post (23), one end of the telescopic push-pull device is hinged to the box body (21), the other end of the telescopic push-pull device is hinged to the rotating upright post (23), and when the telescopic push-pull device extends, the rotating upright post (23) rotates to drive the launching platform (22) to rotate towards the side opening (211) of the box body (21).
2. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: and telescopic hydraulic support legs (111) are arranged at the four corners of the chassis (11) of the walking vehicle.
3. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: the number of the transportation launching boxes (2) is two, and when the transportation launching boxes (2) are all positioned on the chassis (11) of the walking vehicle, the transportation launching boxes (2) are arranged from bottom to top.
4. The integrated unmanned aerial vehicle transportation launching device of claim 3, wherein: the openings of the box bodies (21) of the two transportation launching boxes (2) face opposite directions, and when the two transportation launching boxes (2) move towards the side direction of the chassis (11) of the walking vehicle, the moving directions of the two transportation launching boxes (2) are opposite.
5. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: the chassis (11) of the walking vehicle is provided with a power supply device.
6. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: a plurality of stay cables (25) are further arranged between the top of the rotating upright column (23) and the launching platform (22).
7. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: the hydraulic turnover mechanism (3) comprises a turnover rocker arm (31), one end of the turnover rocker arm (31) is hinged to the transportation launching box (2), the other end of the turnover rocker arm (31) is hinged to the running vehicle chassis (11), a main turnover hydraulic stretching push-pull device is arranged between the turnover rocker arm (31) and the running vehicle chassis (11), one end of the main turnover hydraulic stretching push-pull device is hinged to the turnover rocker arm (31), and the other end of the main turnover hydraulic stretching push-pull device is hinged to the running vehicle chassis (11).
8. The integrated unmanned aerial vehicle transportation launching device of claim 7, wherein: an auxiliary overturning hydraulic telescopic push-pull device is arranged between the overturning rocker arm (31) and the transportation launching box (2), one end of the auxiliary overturning hydraulic telescopic push-pull device is hinged with the overturning rocker arm (31), and the other end of the auxiliary overturning hydraulic telescopic push-pull device is hinged with the transportation launching box (2).
9. The integrated unmanned aerial vehicle transportation launching device of claim 1, wherein: the chassis (11) of the walking vehicle is also provided with a storage box (6).
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| CN202111257073.5A CN113859093A (en) | 2021-10-27 | 2021-10-27 | Integrated unmanned aerial vehicle transportation launching device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114889838A (en) * | 2022-03-31 | 2022-08-12 | 哈尔滨工业大学 | Unmanned aerial vehicle take-off and landing platform for electromagnetic emission |
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