Unmanned aerial vehicle transportation and launcher device

Abstract

The utility model relates to the technical field of aviation system unmanned aerial vehicle launching, in particular to an unmanned aerial vehicle transporting and launching rack device which comprises a transport vehicle assembly, a launching rack base is fixedly installed in the center of the top of the transport vehicle assembly, and a launching bracket is fixedly installed in the center of the top of the launching rack base through a platform supporting mechanism. An engine adjusting assembly is fixedly installed on the left side of the launching rack base, an engine supporting seat is fixedly installed on the left side of the top of the launching bracket, wing supporting seats are fixedly installed in front of and behind the top of the launching bracket, and a belly supporting seat is fixedly installed in the center of the top of the launching bracket. A machine head supporting seat is fixedly mounted on the right side of the top of the launching bracket; the unmanned aerial vehicle transporting and launching device has the advantages that the unmanned aerial vehicle transporting maneuverability is high, the launching direction can be quickly adjusted and locked when the unmanned aerial vehicle encounters severe road conditions, weather and the like, the unmanned aerial vehicle transporting and launching device is simple in mechanism, convenient to operate and rotate and wide in application, and the working efficiency is improved.

Description

Technical Field

[0001] This utility model patent relates to the technical field of drone launch in aviation systems, and more specifically, to a drone transport and launch rack device. Background Art

[0002] Unmanned aerial vehicles first appeared in the 1920s. A small aircraft that did not require a human pilot and was operated by radio was developed so that it could fly over a target area of ​​the enemy for bombing. At that time, drones were used as training targets. After continuous development, especially under the conditions of modern information warfare, drones are widely used to perform tasks such as monitoring, reconnaissance, and precision strikes.

[0003] However, UAV transportation and launching devices have become key technologies. How to improve the maneuverability of UAV transportation and how to overcome the influence of bad road conditions, weather and other factors on the launching posture of UAV are issues that urgently need to be improved. Therefore, a UAV transportation and launching device is proposed to address the above problems. Utility Model Content

[0004] The purpose of the utility model is to provide a UAV transportation and launcher device, aiming to solve the problem of how to improve the maneuverability of UAV transportation and how to overcome the influence of bad road conditions, weather and other factors on the UAV launch posture.

[0005] The utility model is implemented as follows: a UAV transport and launcher device includes a transport vehicle assembly;

[0006] A launcher base is fixedly installed at the top center of the transport vehicle assembly, and a launch bracket is fixedly installed at the top center of the launcher base via a platform support mechanism;

[0007] An engine adjustment assembly is fixedly installed on the left side of the launcher base;

[0008] An engine support seat is fixedly installed on the left side of the top of the launch bracket, a wing support seat is fixedly installed on the front and rear of the top of the launch bracket, a belly support seat is fixedly installed at the center of the top of the launch bracket, and a nose support seat is fixedly installed on the right side of the top of the launch bracket.

[0009] Furthermore, the transport vehicle assembly includes a vehicle frame, and fast motor vehicle wheel assemblies are fixedly installed on both sides of the front and rear surfaces of the vehicle frame, and fast supports are fixedly installed in front and rear of both sides of the left and right sides of the vehicle frame.

[0010] Furthermore, a traction rod is detachably connected to the center of the right side of the vehicle body frame.

[0011] Furthermore, the vehicle body frame adopts 80-mm rectangular square tubes, and the tube wall thickness of the 80-mm rectangular square tubes is 8 mm.

[0012] Furthermore, the launcher base adopts a rectangular frame structure, and the left and right sides of the launcher base are both connected to the vehicle body frame through connecting plates.

[0013] Furthermore, the left side of the launcher base is fixedly mounted with the engine adjustment assembly via an interface.

[0014] Furthermore, the launching bracket adopts a rectangular square tube structure.

[0015] Compared with the prior art, the utility model facilitates the movement of the device and the transportation of the UAV through the transport vehicle assembly, and then the launcher base and the launch bracket are installed through the platform support mechanism, and the engine support seat and the wing support seat and the belly support seat and the nose support seat on the top of the launch bracket can support the UAV and make the UAV placed firmly, and then the engine adjustment assembly installed on the left side of the launcher base can adjust to adapt to the flight attitude of the UAV, so that the UAV transportation has strong maneuverability, and the function of quickly adjusting and locking the launch direction when encountering bad road conditions, weather and other reasons is realized. The UAV transportation and launching device has a simple structure, is easy to operate, and is easy to rotate. It is widely applicable and can improve work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a three-dimensional structural schematic diagram of a UAV transport and launcher device provided by the utility model;

[0017] Figure 2 This is a schematic diagram of the structure of a transport vehicle assembly of a UAV transport and launcher device provided by the utility model;

[0018] Figure 3 The utility model discloses a launching bracket structure schematic diagram of a UAV transport and launching device.

[0019] The figure marks involved in the above drawings are: 01, transport vehicle assembly; 001, traction rod; 002, vehicle body frame; 003, fast motor vehicle wheel assembly; 004, fast support; 02, launch pad base; 03, launch bracket; 04, engine adjustment assembly; 05, engine support seat; 06, platform support mechanism; 07, wing support seat; 08, belly support seat; 09, nose support seat. DETAILED DESCRIPTION

[0020] In order to make the purpose, technical solution and advantages of the utility model more clear, the utility model is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the utility model and are not used to limit the utility model.

[0021] The implementation of the present utility model is described in detail below in conjunction with specific embodiments.

[0022] according to Figure 1-3 As shown, a UAV transport and launcher device includes a transport vehicle component 01;

[0023] A launcher base 02 is fixedly installed at the top center of the transport vehicle assembly 01, and a launch bracket 03 is fixedly installed at the top center of the launcher base 02 via a platform support mechanism 06;

[0024] An engine adjustment assembly 04 is fixedly mounted on the left side of the launcher base 02;

[0025] An engine support seat 05 is fixedly installed on the left side of the top of the launching bracket 03, a wing support seat 07 is fixedly installed on the front and rear of the top of the launching bracket 03, a belly support seat 08 is fixedly installed at the center of the top of the launching bracket 03, and a nose support seat 09 is fixedly installed on the right side of the top of the launching bracket 03; when working, the transport vehicle component 01 is used to facilitate the movement of the device and the transportation of the UAV, and then the launcher base 02 and the launching bracket 03 are installed through the platform support mechanism 06, and the engine support seat 05 and the wing support seat 07 and the belly support seat 08 and the nose support seat 09 on the top of the launching bracket 03 can support the UAV and make the UAV placed firmly, and then the engine adjustment component 04 installed on the left side of the launching bracket base 02 can be adjusted to adapt to the flight posture of the UAV, so the utility model realizes that the UAV transportation has strong mobility and can quickly adjust and lock the launch direction when encountering bad road conditions, weather and other reasons. The UAV transportation and launching device has a simple structure, is easy to operate, is easy to rotate, is widely applicable, and can improve work efficiency.

[0026] The transport vehicle assembly 01 includes a vehicle body frame 002, and fast motor vehicle wheel assemblies 003 are fixedly installed on the left and right sides of the front and rear surfaces of the vehicle body frame 002, and fast supports 004 are fixedly installed in the front and rear of the left and right sides of the vehicle body frame 002; when working, the device is mainly supported by the vehicle body frame 002, and the mobile transportation of the device is facilitated by the fast motor vehicle wheel assembly 003, and stable support can be provided by the fast support 004. The fast motor vehicle wheel assembly 003 improves the rapid maneuverability of the transport vehicle during bumpy and high-speed driving, such as rapid steering, U-turn, acceleration, etc., and standard parts of fast supports 004 are set on the left and right sides of the vehicle body frame. Once the launch direction of the drone is ensured, the fast support 004 is quickly lowered to complete the launch of the drone.

[0027] The towing rod 001 is detachably connected to the center of the right side of the vehicle body frame 002; when working, the towing rod 001 can be applied to different vehicle models and has a simple structure, and can be quickly disassembled and assembled.

[0028] The vehicle body frame 002 is made of 80 rectangular square tubes, and the tube wall thickness of the 80 rectangular square tubes is 8 mm; when working, the stability of the vehicle body itself is ensured on bumpy roads.

[0029] The launcher base 02 adopts a rectangular frame structure, and the left and right sides of the launcher base 02 are clamped with the vehicle frame 002 through connecting plates; when working, the launcher base 02 and the vehicle frame 002 are firmly clamped through the connecting plates, and the left and right sides of the launcher base 02 are provided with fast rotation mechanisms to make the rotation smoother.

[0030] The left side of the launcher base 02 is fixedly installed with the engine adjustment component 04 through an interface; when working, the engine adjustment component 04 interface is set at the end of the launcher base 02, and the interface is set with a top screw to adjust the position of the engine adjustment component 04 left and right to adapt to the flight posture of the drone.

[0031] The launching bracket 03 adopts a rectangular square tube structure; when working, the support is stable and the structural strength is high.

[0032] Working principle: When in use, the transport vehicle assembly 01 facilitates the movement of the device and the transportation of the UAV, and then the launch base 02 and the launch bracket 03 are installed through the platform support mechanism 06, and the engine support seat 05 and the wing support seat 07 and the belly support seat 08 and the nose support seat 09 on the top of the launch bracket 03 can support the UAV and make the UAV placed firmly, and then the engine adjustment assembly 04 installed on the left side of the launch base 02 can adjust to adapt to the flight attitude of the UAV, so the utility model realizes the strong mobility of UAV transportation, and the function of quickly adjusting and locking the launch direction when encountering bad road conditions, weather and other reasons. The UAV transportation and launching device has a simple structure, is easy to operate, easy to rotate, widely applicable, and can improve work efficiency.

[0033] The same or similar numbers in the drawings of this embodiment correspond to the same or similar parts; in the description of the present utility model, it should be understood that if the terms "upper", "lower", "left", "right" and the like indicate directions or positional relationships based on the directions or positional relationships shown in the drawings, it is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific direction, be constructed and operated in a specific direction. Therefore, the terms describing the positional relationship in the drawings are only used for illustrative purposes and cannot be understood as limitations on this patent. For ordinary technicians in this field, the specific meanings of the above terms can be understood according to specific circumstances.

[0034] Reference Figure 1-3 As shown, it is a preferred embodiment provided by the utility model.

[0035] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A UAV transport and launcher device, comprising a transport vehicle assembly (01); It is characterized in that A launcher base (02) is fixedly mounted at the top center of the transport vehicle assembly (01), and a launch bracket (03) is fixedly mounted at the top center of the launcher base (02) via a platform support mechanism (06); An engine adjustment assembly (04) is fixedly mounted on the left side of the launcher base (02); An engine support seat (05) is fixedly mounted on the left side of the top of the launch bracket (03), a wing support seat (07) is fixedly mounted at the front and rear of the top of the launch bracket (03), a belly support seat (08) is fixedly mounted at the center of the top of the launch bracket (03), and a nose support seat (09) is fixedly mounted on the right side of the top of the launch bracket (03).

2. The UAV transport and launcher device according to claim 1, characterized in that: The transport vehicle assembly (01) comprises a vehicle frame (002), wherein fast motor vehicle wheel assemblies (003) are fixedly mounted on both left and right sides of the front and rear surfaces of the vehicle frame (002), and fast supports (004) are fixedly mounted on both the front and rear sides of the left and right sides of the vehicle frame (002).

3. The UAV transport and launcher device according to claim 2, characterized in that: A traction rod (001) is detachably connected to the center of the right side of the vehicle body frame (002).

4. The UAV transport and launcher device according to claim 3, characterized in that: The vehicle body frame (002) is made of an 80-mm rectangular square tube, and the tube wall thickness of the 80-mm rectangular square tube is 8 mm.

5. The UAV transport and launcher device according to claim 4, characterized in that: The launcher base (02) adopts a rectangular frame structure, and the left and right sides of the launcher base (02) are both connected to the vehicle body frame (002) via connecting plates.

6. The UAV transport and launcher device according to claim 5, characterized in that: The left side of the launcher base (02) is fixedly mounted with the engine adjustment assembly (04) via an interface.

7. The UAV transport and launcher device according to claim 6, characterized in that: The launching bracket (03) adopts a rectangular square tube structure.

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