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Unmanned aerial vehicle with detachable flight test structure

A technology of flight testing and unmanned aerial vehicles, which is applied in the direction of aircraft component testing, aircraft, and unmanned aircraft, etc. Detection device, no way to provide detection data and other problems, to achieve the effect of various and comprehensive detection items, convenient and simple structure assembly, simple and beautiful appearance structure

Pending Publication Date: 2022-02-01
阜阳安知科技信息咨询有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Most of the traditional UAV testing work is the quality inspection of the airframe body, the lifting force inspection of the propeller, and the flight control ability inspection before leaving the factory. Th

Method used

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  • Unmanned aerial vehicle with detachable flight test structure
  • Unmanned aerial vehicle with detachable flight test structure
  • Unmanned aerial vehicle with detachable flight test structure

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0035] Example 1:

[0036] like Figure 1-4 As shown, a UAV with a detachable flight test structure includes a UAV body 1, and the UAV body 1 also includes a frame 102, and the outer walls on both sides of the frame 102 are fixedly equipped with hidden hangers 2, The bottom end of the frame 102 is movably assembled with a load-bearing detection component 3 through the hidden hanger 2, and the surface of the load-bearing detection component 3 is located at the bottom of the frame 102. A stable detection component 4 is movably assembled, and the outer surface of the load-bearing detection component 3 is located The lower movable assembly is equipped with a wind resistance assembly 5;

[0037] Refer to attached figure 2 , the inner top of the frame 102 is fixedly installed with an organic case 101, the outer wall of one side of the frame 102 is provided with a camera 103, the outer wall of the top of the frame 102 is fixedly installed with a brushless motor 104 through equidis...

Example Embodiment

[0044] Example 2:

[0045] like Figure 5-6 Shown, a kind of unmanned aerial vehicle with detachable flight test structure, comprises unmanned aerial vehicle body 1;

[0046] Refer to attached Figure 5 , the stable detection assembly 4 also includes a main liquid pipe 401, the two ends of the outer wall of the main liquid pipe 401 are fixedly connected with a conduit 402, and the ends of the conduit 402 are fixedly connected with a detection tube 403, and the main liquid pipe 401, the conduit 402 and the detection tube 403 The interiors are all connected, and the combination of the four main liquid pipes 401 and the conduit 402 is fixedly connected through the provided connecting frame 404. The bottom surface of the connecting frame 404 is fixed in the middle with a bottom swivel seat 405, and the bottom surface of the connecting frame 404 passes through the bottom swivel seat 405. An L-shaped coil 406 is rotatably connected, and the threaded end of the L-shaped coil 406 pa...

Example Embodiment

[0050] Example 3:

[0051] like Figure 7 Shown, a kind of unmanned aerial vehicle with detachable flight test structure, comprises unmanned aerial vehicle body 1;

[0052] Refer to attached Figure 7 , the air resistance assembly 5 also includes a double pipe frame 501, four double pipe frames 501 are respectively slidably assembled with four bottom guide rods 305, and the double pipe frame 501 is fixedly assembled with the bottom guide rods 305 through a threaded set screw 502, the double pipe The ends of the frame 501 are fixedly equipped with windshields 503. When detecting the flight capability of the UAV body 1 in a windy environment, the double-pipe frame 501 and the bottom guide rod 305 are first fixed and assembled by positioning screws 502, and then Place several electric fans in the test environment, and then control the drone body 1 to fly in a windy environment, and the windshield 503 in different directions will be blocked by the corresponding wind force, there...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle detection, and particularly relates to an unmanned aerial vehicle with a detachable flight test structure. The unmanned aerial vehicle comprises an unmanned aerial vehicle body, hidden hangers are fixedly arranged on the outer walls of the two sides of a rack, and a bearing detection assembly is movably assembled at the bottom end of the rack through the hidden hangers; a stable detection assembly is movably assembled on the surface of the bearing detection assembly and located at the bottom end of the rack, a wind resistance assembly is movably assembled on the outer surface of the bearing detection assembly and located below the rack, assembling holes are fixedly formed in the four corners of the assembling plate, and weight pans are movably stacked on the upper surface of the bearing plate; and the two ends of the outer wall of the main liquid pipe are fixedly connected with guide pipes, and the tail ends of the guide pipes are fixedly connected with detection pipes. According to the invention, the bearing capacity of the unmanned aerial vehicle during flight, the stability during flight and the flight capacity in strong wind can be detected, the detection items are more diversified and comprehensive, various structural components are flexible and detachable, and the structure is simple.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle detection, and in particular relates to an unmanned aerial vehicle with a detachable flight test structure. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", is an unmanned aircraft controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by the on-board computer; compared with manned aircraft, UAVs are often more suitable for tasks that are too "dumb, dirty or dangerous"; UAVs can be divided into military and civilian uses according to the application field; in aerial photography, agriculture, plant protection, micro selfie, express transportation, disaster relief, observation Applications in fields such as wild animals, monitoring infectious diseases, surveying and mapping, news reports, power inspections, disaster relief, film and television shooting, creatin...

Claims

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Application Information

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IPC IPC(8): B64F5/60B64C27/08B64C39/02
CPCB64F5/60B64C27/08B64C39/02B64U10/10B64U2101/00
Inventor 李晓露李正强
Owner 阜阳安知科技信息咨询有限公司
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