Microminiature intelligent adjustable ignition system and adjusting method
An ignition system and micro-sized technology, applied in jet propulsion devices, gas turbine devices, ramjet engines, etc., can solve problems such as not being suitable for wide-area flight conditions, unable to achieve multiple ignitions of the engine, and consuming large amounts of energy
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[0032] The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0033] The invention provides a miniature intelligent adjustable ignition system, such as figure 1 As shown, including plasma igniter, fuel tank, stop valve, booster and controller.
[0034] The plasma igniter is used to ignite the atomized fuel mixture in the combustion chamber of the ramjet engine and provide a continuous and stable combustion flame; the fuel tank is used to provide stable fuel for the plasma igniter; the shut-off valve is used to prevent the fuel from flowing back in the fuel tank; The pusher is used to adjust the oil pressure in the fuel tank as an actuator to control the fuel flow of the plasma igniter; the controller includes a plasma igniter fuel flow control algorithm and a plasma igniter current control algorithm. Flight conditions such as Mach number, angle of attack, sideslip angle, total incoming pressure, and total incoming t...
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