发明名称 |
Air intake system of a propeller-turbine engine |
摘要 |
An air intake system of a propeller-turbine engine with a propeller gearbox 1 in inline arrangement, includes one or more intake units 3 arranged essentially below a nacelle fairing 2 of the propeller-turbine engine with each intake unit 3 being related to a elbow diffuser 19, a shock diffuser 4, and a rotationally symmetric attenuation chamber 5 into which the respective shock diffuser 4 issues and which is connected to the compressor inlet 6 of the propeller-turbine engine.
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申请公布号 |
US2003113205(A1) |
申请公布日期 |
2003.06.19 |
申请号 |
US20020321490 |
申请日期 |
2002.12.18 |
申请人 |
NEGULESCU DIMITRIE;MUNDT CHRISTIAN |
发明人 |
NEGULESCU DIMITRIE;MUNDT CHRISTIAN |
分类号 |
B64D33/02;F02C7/04;(IPC1-7):F03B1/00 |
主分类号 |
B64D33/02 |
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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