Engine control system of YUN-5 unmanned aerial vehicle system

A control system and engine technology, which is applied to aircraft power units, aircraft parts, transportation and packaging, etc., can solve the problems of increased vacancy of Y-5 aircraft and shortage of Y-5 pilots, and achieve high safety, high reliability, and structure The effect of fewer components

Pending Publication Date: 2021-02-26
XIAN LINGKONG ELECTRONICS TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide an engine control system for the UAV system, which solves the problem that the existing Yun-5 pilots are in short supply and the Yun-5 aircraft is vacant.

Method used

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  • Engine control system of YUN-5 unmanned aerial vehicle system
  • Engine control system of YUN-5 unmanned aerial vehicle system

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Embodiment Construction

[0023] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0024] The present invention transports five changes to the engine control system of the unmanned aerial vehicle system, such as figure 1 , figure 2 As shown, it includes the central console 1, the upper surface of the central console 1 is fixed to the console panel 2, the console panel 2 is installed with the carburetor steering system, the pitch steering system, and the throttle steering system, and the central console 1 is installed on one side. Parking steering gear system, high-altitude steering gear system, dust-proof steering gear system, carburetor steering gear system, pitch steering gear system, throttle steering gear system, parking steering gear system, high-altitude steering gear system, The dust-proof steering gear system is connected to the engine.

[0025] The carburetor steering gear system includes the steering gear a3 fi...

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Abstract

The invention discloses an engine control system of a YUN-5 unmanned aerial vehicle system, which comprises a central control console, a control console panel is fixedly connected to the upper surfaceof the central control console, a vaporizer steering engine system, a pitch steering engine system and an accelerator steering engine system are arranged on the control console panel, and a parking steering engine system is arranged on one side surface of the central control console. A high-altitude steering engine system is installed on the other side face of the central control board, and the dustproof steering engine system, the vaporizer steering engine system, the propeller pitch steering engine system, the accelerator steering engine system, the parking steering engine system, the high-altitude steering engine system and the dustproof steering engine system are all connected with the engine. The engine control system of the YUN-5 unmanned aerial vehicle system has the advantages ofbeing simple in structure and high in reliability, and the problems that an existing YUN-5 pilot is in shortage, vacancy of a YUN-5 aircraft is increased, and resources are wasted are solved.

Description

technical field [0001] The invention belongs to the technical field of power control systems for large-scale unmanned aerial vehicles, and in particular relates to the engine control system of the unmanned aerial vehicle system. Background technique [0002] Yunwu Aircraft is a single-engine, biplane, semi-metallic general aviation aircraft, which has good low-altitude and ultra-low-altitude flight performance, can take off and land on a short simple runway, has mature and reliable performance, and is easy to maintain. It is widely used in short-distance transportation , Farming operations, my country and the world have a huge amount. [0003] However, due to the early design of the Yun-5 aircraft, the cockpit is small, not equipped with an air-conditioning system, the cabin facilities are simple, and the comfort of the pilot and passengers is not fully considered, resulting in a poor driving environment and poor experience for the pilots of the Yun-5 aircraft. At present, t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D31/14
CPCB64D31/14
Inventor 雷黎明郭宏选董文斌沈洋
Owner XIAN LINGKONG ELECTRONICS TECH CO LTD
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