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Quick-release opposite-opened-type power cabin cover for unmanned aerial vehicle

A power cabin and split-type technology, which is applied in the direction of aircraft power devices, aircraft power device components, aircraft parts, etc., can solve the problems of long maintenance time and cumbersome ground maintenance, so as to achieve fast inspection and reduce the difficulty and intensity of maintenance work , Improve the effect of maintenance

Pending Publication Date: 2019-07-30
XIAN AISHENG TECH GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In order to avoid the shortcomings of the existing technology and overcome the problems of cumbersome ground maintenance and time-consuming maintenance of the power plant system of the UAV, the present invention proposes a quick-release split power cabin cover for the UAV, through simple operation, The power cabin cover can be easily opened to realize a quick and comprehensive inspection of the UAV's power plant system on the ground, thus meeting the needs of UAV's rapid and comprehensive support on the ground

Method used

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  • Quick-release opposite-opened-type power cabin cover for unmanned aerial vehicle
  • Quick-release opposite-opened-type power cabin cover for unmanned aerial vehicle

Examples

Experimental program
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Effect test

Embodiment Construction

[0018] This embodiment is a quick-release split-type power cabin cover for an unmanned aerial vehicle.

[0019] refer to figure 1 , figure 2 , the present embodiment is used for unmanned aerial vehicle quick-release folio type power cabin cover, by power cabin cover 101, canopy lower strut plate 102, quick-release lock 103, canopy closed and fixed quick-release lock 104, connecting hinge 105, bearing The power frame 106 and the mooring rope 201 are composed; the power cabin cover 101 is two parts with the same structure, and the power cabin cover 101 adopts the overall aerodynamic shape design, with a streamlined finish and a split structure. The power cabin cover 101 is respectively A quick card hole 206 is provided; the power cabin firewall is provided with a reinforced edge, and the two ends of the mooring rope 201 are respectively connected with the power cabin cover 101 and the reinforced edge of the power cabin firewall. The canopy lower brace 102 is fixedly connected...

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PUM

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Abstract

The invention discloses a quick-release opposite-opened-type power cabin cover for an unmanned aerial vehicle. The quick-release opposite-opened-type power cabin cover is composed of power cabin covers, cabin cover lower supporting plates, quick-release locks, a load bearing frame, and a mooring rope, wherein the power cabin covers are two components with the same structure and adopt overall pneumatic profile design, an ending structure is in a streamline shape, and the power cabin covers are respectively provided with quick inserting clamping holes; the two ends of the mooring rope are respectively connected with the power cabin covers and the strengthening edge of a power cabin firewall; the cabin cover lower supporting plates are fixedly connected with the load bearing frame, the two sides of the cabin cover lower supporting plates are connected with the power cabin covers through connection hinges respectively, the power cabin covers and the load bearing frame are connected to an airframe and fixed through the quick-release locks along the fuselage cross section, and the two power cabin covers are buttoned in a butt joint mode and fastened by the quick release locks; and when states of power cabin equipment and an engine are needed to be checked, the quick release locks are pressed, thus the opposite-opened power cabin covers separate from the top and pulled by the mooringrope to gravity whereabouts, a power device system is quickly maintained and checked, and reliable flying of the unmanned aerial vehicle is ensued.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a quick-release split power cabin cover for unmanned aerial vehicles. Background technique [0002] Most of the power plant systems of UAVs are installed centrally in their power cabins, and the ground inspection of the power plant systems on UAVs is an important part of the ground maintenance work of UAVs. It is to ensure reliable operation of engines and reliable flight of UAVs important means. [0003] As the main equipment compartment of the power plant system, the engine and its measurement and control, power supply, lubrication, ventilation and cooling, oil supply and other related subsystems are arranged in the power compartment. Before driving and flying the UAV engine on the ground, it is necessary to ensure that the engine and other equipment in the power plant system are installed and fixed reliably, the pipeline connection is firm, there is no aging ...

Claims

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Application Information

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IPC IPC(8): B64D29/00B64D29/06
CPCB64D29/00B64D29/06
Inventor 车海威
Owner XIAN AISHENG TECH GRP
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