A dual combustion chamber scramjet engine and its control method
A scramjet, dual-combustion chamber technology, used in ramjet engines, combined engines, machines/engines, etc., can solve the problems of combination and relay difficulties, reduce the adjustment of additional mass, facilitate combustion organization, and improve engine performance. Effect
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[0045] This embodiment provides a dual combustion chamber scramjet, figure 1 Its structure is shown, the engine is made up of intake port 1', subsonic combustion chamber 2', supersonic combustion chamber 3' and tail nozzle 4', and said subsonic combustion chamber 2' and supersonic combustion chamber 3' Use rectangular parallel layout;
[0046] see figure 2 and image 3 , figure 2 Schematic diagram of the layout of the double inlet runners provided by the embodiment of the present invention; image 3 It is a schematic diagram of the air inlet channel adjustment scheme in the embodiment of the present invention. The inlet channel 1' adopts a binary inlet channel configuration, and is divided into a sub-combustion channel B and a super-combustion channel A and C by a support plate along the flow direction. The B channel is an intermediate channel, which connects In the subsonic combustion chamber 2', the A and C flow channels are distributed on both sides of the B flow cha...
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