Ground starting device for turbojet engine

A technology of turbojet engine and starting device, which is applied in the direction of engine starting, engine components, engine ignition, etc., can solve the problem that the turbojet engine cannot meet the ground starting form, the small turbojet engine cannot be realized, and the special site starting cannot be realized. problem, to achieve the effect of light weight, simple structure and small volume

Active Publication Date: 2021-08-10
中科航星科技股份有限公司
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The present invention aims at the above-mentioned deficiency that existing turbojet engine ground starting device exists, provides a kind of turbojet engine ground starting device, and this turbojet engine ground starting device solves the low starting efficiency of the existing starting device, cumbersome equipment, and Affected by the landform, it is impossible to start on a special site. At the same time, it is impossible to realize the rapid start and multi-machine start on the test site after the small turbojet engine is mated.

Method used

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  • Ground starting device for turbojet engine
  • Ground starting device for turbojet engine
  • Ground starting device for turbojet engine

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Embodiment 1

[0038] like figure 1 As shown, the present embodiment provides a ground starting device for a turbojet engine, comprising:

[0039] A chassis, the chassis comprising a box body and a customizable panel;

[0040] An electrical system, the electrical system includes a driver, an adjustable power supply, a regulated power supply, and a relay,

[0041] Fuel system, the fuel system includes ignition oil pump, priority oil pump and fuel filter. After the ignition oil pump and priority oil pump work, the fuel flows from the external fuel tank in two ways through the ignition oil input and priority oil input interfaces on the panel of the ground starter, and enters To the internal two-way fuel filter, then to the ignition oil pump and priority oil pump, and then output from the ignition oil output interface and priority oil output interface on the panel to the two-way oil inlet interface of the engine.

[0042] The ignition oil pump and the priority oil pump are controlled by an eng...

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Abstract

The invention relates to the technical field of auxiliary power devices, in particular to a turbojet engine ground starting device, comprising: an electrical system, the electrical system includes: a driver, an adjustable power supply, a voltage stabilized power supply, a relay, a fuel system, and the fuel system includes an ignition After the fuel pump, priority fuel pump and fuel filter, the ignition fuel pump and the priority fuel pump work, the fuel flows from the external fuel tank in two ways through the ignition oil input and priority fuel input interfaces on the ground starter panel, enters the internal two-way fuel filter, and then to the ignition oil pump and the priority oil pump, and then output from the panel ignition oil output interface and the priority oil output interface to the two-way oil inlet interface of the engine. The ground starting device of the turbojet engine has high starting efficiency and can be started in a special place without being affected by the terrain. , the device structure is simple, after the small-sized turbojet engine is put into flight, multiple sets of the ground starting device can be used on the test flight site so as to realize the tasks of simultaneous starting of multiple machines and simultaneous flight of multiple machines.

Description

technical field [0001] The invention relates to the technical field of auxiliary power devices, in particular to a ground starting device for a turbojet engine. Background technique [0002] For turbojet engines, in order to start the engine reliably and meet a certain starting acceleration, it is generally used to start with a ground air source vehicle or a windmill to achieve a suitable speed. This type of operation is complicated and the starting equipment is inconvenient to move, which has great limitations. The traditional starting method of starting the engine is easily restricted in outdoor operation, and the cost is high. Therefore, it is necessary to develop suitable starting equipment to realize the starting problem of the turbojet engine in the outdoor environment. [0003] At present, the starting device of small turbojet engines mainly adopts large equipment vehicles with built-in starting equipment, pipelines and cables. After the engine is matched to the flig...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C7/266F02C7/26F02C7/00
CPCF02C7/00F02C7/26F02C7/266
Inventor 潘武义张彬刘迪张伟宁伟洁于成龙王姗姗李建云从炳雨侯海玉郭海龙冯文亮丁金龙
Owner 中科航星科技股份有限公司
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