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Starting device of small unmanned aerial vehicle engine

A technology of small unmanned aerial vehicle and starting device, which is applied in the fields of ground equipment, aircraft parts, transportation and packaging, etc., which can solve the problems of high technical difficulty, the inability to share unmanned aerial vehicles, and the increase in the weight of unmanned aerial vehicles. Transportation and storage, high device stability, and the effect of reducing the occupied space

Active Publication Date: 2015-11-25
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, engine modification is technically difficult, and the onboard starting device will also increase the empty weight of the UAV, which will affect the efficiency of the whole machine
In addition, the price of the airborne starting device is relatively high, and a set of accessories is only useful for one engine, which cannot be shared between multiple drones, which also increases the cost of using the drone system

Method used

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  • Starting device of small unmanned aerial vehicle engine
  • Starting device of small unmanned aerial vehicle engine
  • Starting device of small unmanned aerial vehicle engine

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Embodiment Construction

[0024] In order to better understand the starting device of the small UAV engine according to the solution of the present invention, a preferred embodiment of the starting device of the small UAV engine of the present invention will be further described below in conjunction with the accompanying drawings.

[0025] Such as Figure 1-Figure 3 As shown, the starting device of the small unmanned aerial vehicle engine provided by the present invention includes an upper frame 1 and a lower frame 12, wherein the upper frame 1 is a frame with corners, and the upper frame 1 is fixed with an electric starter 3, and the upper frame 1 is fixed with an electric starter 3. The frame 1 is hinged with the lower frame 12 through the axle 6; the corner of the frame of the upper frame 1 is provided with pin shaft fixing lugs, and the same position on the frame of the lower frame 12 is provided with pin shaft fixing lugs, and one end of the upper pole 5 passes through the first A pin 4 is hinged ...

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Abstract

The invention discloses a starting device of a small unmanned aerial vehicle engine, and relates to the technical field of structural design of aircraft ground auxiliary appliances. The starting device of the small unmanned aerial vehicle engine is used for starting the engine of a small unmanned aerial vehicle on the ground. An electric starter is fixed on an upper frame which is hinged to a lower frame through a wheel axle; one end of an upper supporting rod is hinged to the upper frame through a first hinge pin, one end of a lower supporting rod is hinged to the lower frame through a second hinge pin, and the other end of the upper supporting rod is connected with the other end of the lower supporting rod through a third hinge pin; a locking sleeve is arranged on the upper supporting rod. Due to the fact that the starting device of the small unmanned aerial vehicle engine is used for starting the small unmanned aerial vehicle, the starting process of the engine is made to be safer and more reliable, the occupied space can be reduced through folding, and transportation and storage are facilitated; in addition, by means of the adjustment of the installation height of the electric starter on the frame, the starting device can be suitable for the unmanned aerial vehicle with different types, and the cost of the ground maintenance of the unmanned aerial vehicle is made to be reduced.

Description

technical field [0001] The invention relates to the technical field of structural design of aircraft ground auxiliary equipment, in particular to a starting device for a small unmanned aerial vehicle engine. Background technique [0002] The layout of double tail braces is widely used in small unmanned aerial vehicles. Small unmanned aerial vehicles with this layout are generally equipped with a single tail-propelled piston propeller engine to allow space in the front of the fuselage, which is convenient for photoelectric pods and other effective load loading. However, this caused certain difficulties to start the engine at the rear of the fuselage. [0003] In order to reduce the weight as much as possible and improve the power-to-weight ratio, the piston engines used in small UAVs generally do not include a starting device. In actual use, the following three methods are usually used to start. One is to start the propeller manually by the ground crew; the other is to star...

Claims

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Application Information

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IPC IPC(8): B64F1/34
Inventor 王立波张德虎蒋汉杰李悦立唐斌
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA