发明名称 Aircraft propulsion unit and corresponding aircraft
摘要 A propulsion unit includes at least one exhaust pipe (62, 76) that includes an air discharge that is delimited by a trailing edge (78, 82). The end part of the exhaust pipe (62, 76) includes two scalloped shapes (84) that each correspond to a preferred acoustic radiation direction, separated by advanced parts (86) that can limit the acoustic radiation, whereby the scalloped shapes are offset upward relative to the horizontal median plane.
申请公布号 EP2029879(A1) 申请公布日期 2009.03.04
申请号 EP20070789000 申请日期 2007.06.13
申请人 AIRBUS FRANCE 发明人 DRUON, YANN;CHELIN, FREDERIC;GANTIE, FABRICE
分类号 F02K1/44;F02K1/38;F02K1/48 主分类号 F02K1/44
代理机构 代理人
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