发明名称 METHOD OF ATTENUATING BY MASK EFFECT THE NOISE EMITTED BY THE JET NOZZLES OF JET ENGINES
摘要 1457789 Silencing jet propulsion plant SOC NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION 2 Aug 1974 [31 Aug 1973] 34200/74 Heading FIJ The noise of an aircraft jet nozzle I perceived by an observer at A is reduced by mounting a further quieter jet nozzle 2 between the jet nozzle 1 and the observer. Several quieter jet nozzles 2 may be provided, each arranged in a direction in which it is desired to attenuate the noise of jet nozzle 1. Each jet nozzle 2 may have a silencing notch 4, as disclosed in Specification 1453990 disposed in the desired direction of attenuation, or may be silenced in other ways, e.g by hinged panels as disclosed in Specifications 1457790 and 1364007. Each jet nozzle 2 may have a noise level about 15 PNdB less than that of jet nozzle 1.
申请公布号 GB1457789(A) 申请公布日期 1976.12.08
申请号 GB19740034200 申请日期 1974.08.02
申请人 SNECMA 发明人
分类号 F02K1/44;(IPC1-7):F02K1/26 主分类号 F02K1/44
代理机构 代理人
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