Ground start device for turbojet engine
A turbojet engine and starting device technology, which is applied in the direction of engine starting, engine ignition, engine components, etc., can solve the problem that the turbojet engine cannot be started on the ground, the small turbojet engine cannot be realized, and the start of a special site cannot be realized, etc. problem, to achieve the effect of light weight, simple structure and small volume
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[0038] Such as 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 ...
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