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TANGENTIALLY EXHAUSTING REVOLVING COMBUSTION CHAMBER IN A REVOLVING RAMJET, TURBOJET, TURBOFAN, GAS TURBINE OR OTHER JET ENGINE
TANGENTIALLY EXHAUSTING REVOLVING COMBUSTION CHAMBER IN A REVOLVING RAMJET, TURBOJET, TURBOFAN, GAS TURBINE OR OTHER JET ENGINE
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机译:在旋转的公升机,涡轮喷气机,涡轮喷气机,燃气轮机或其他喷气机发动机中切向消灭燃烧室
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摘要
This invention consists of a combustion chamber or chambers (1), which around an axis (4) and exhaust/s tangentially (3) to its/their circle of rotation within a jet engine (2). The combustion chamber/s may be fitted in an otherwise conventional turbojet, turbofan or gas turbine engine and linked to drive the air compressors and/or other devices. The combustion chamber/s (1) may be integrated with supersonic speed ram charging air scoops, which feed inlet air into the combustion chamber/s, forming (a) revolving ramjet(s). In this form, there may or may not be prior air compressor stages.
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