发明名称 |
TANGENTIALLY EXHAUSTING REVOLVING COMBUSTION CHAMBER IN A REVOLVING RAMJET, TURBOJET, TURBOFAN, GAS TURBINE OR OTHER JET ENGINE |
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. |
申请公布号 |
WO2005008043(A2) |
申请公布日期 |
2005.01.27 |
申请号 |
WO2004ZA00083 |
申请日期 |
2004.07.23 |
申请人 |
ARCHERY, EUGENE, THOMAS, DAVID |
发明人 |
ARCHERY, EUGENE, THOMAS, DAVID |
分类号 |
F02C3/16;F02K7/10;F02K7/16;F23R3/56 |
主分类号 |
F02C3/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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