Fuel injection system and method applicable to regenerative cooling detonation combustor
A technology of fuel injection system and regenerative cooling, which is applied in the direction of intermittent injection devices, jet propulsion devices, rocket engine devices, etc., can solve problems such as pressure pulsation, achieve the effect of avoiding pressure pulsation and improving regenerative cooling capacity
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[0024] The present invention will be further described in detail below in conjunction with the accompanying drawings.
[0025] The present invention is a kind of fuel injection system and method suitable for regenerative cooling detonation combustor, such as figure 1 As shown, it includes: fuel tank 1, bypass regulating valve 2, regenerator gaseous fuel flow pipeline 3, regenerator 4, regenerator mixed fuel flow chamber 5, low pressure ratio turbine 6, excitation generator 7. Gas-liquid separation chamber 8. Detonation combustion chamber second-stage heat exchanger inlet 9. Detonation combustion chamber second-stage heat exchanger 10. Detonation combustion chamber first-stage heat exchanger outlet 11. Detonation combustion chamber Second stage heat exchanger outlet 12, detonation combustion chamber wall 13, detonation combustion chamber first stage heat exchanger 14, detonation combustion chamber first stage heat exchanger inlet 15, spark plug 16, atomizing nozzle 17, oxidant ...
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