| 摘要 |
air-breathing gas-turbine engines primarily of ejector type; engine manufacture. SUBSTANCE: turbo- ejector engine has high-pressure channel of its gas ejector communicating on one end with compressor through main combustion chamber and on other end, with turbine through mixing chamber; low-pressure channel of gas ejector communicates on one end directly with atmosphere through inlet device and on other end, with turbine through mixing chamber. EFFECT: enhanced thrust and efficiency at supersonic flying speeds. 2 cl, 14 dwg
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