发明名称 SILENCER FOR JET ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a silencer of a jet engine capable of reducing exhaust gas noise generated from the turbo jet engine by using an engine exhaust pipe and a mixer ejector provided at the rear side of the engine exhaust pipe and decreasing radiant quantity of the noise emitted to the outside through an ejector intake even when the jet engine is fixed to a wing of a jet airplane. SOLUTION: The silencer 3 of the jet engine can reduce the exhaust gas noise generated from the turbo jet engine 1 by using the engine exhaust pipe 9 and the mixer ejector 13. The exterior wall of the engine exhaust pipe 9 is at least partially covered with sound absorbing material 15 to prevent the noise emitted to the outside through the ejector intake EJ1 from being reflected and radiated by the wing or the body of the jet airplane which the jet engine 1 is fixed to. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2004278414(A) 申请公布日期 2004.10.07
申请号 JP20030071236 申请日期 2003.03.17
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 OISHI TSUTOMU
分类号 B64D33/00;B64D33/04;F01D25/30;F02C7/00;F02K1/48;(IPC1-7):F02C7/00 主分类号 B64D33/00
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