发明名称 MOTORENABGASSYSTEM MIT DIREKTIONALER DÜSE
摘要 An exhaust system for an aircraft has a primary exhaust duct for communicating exhaust gas from an engine exhaust exit and is configured for movement with the engine. A secondary exhaust duct is in fluid communication with the primary exhaust duct and is movably mounted to the airframe. The secondary duct has a portion selectively rotatable relative to the remainder of the secondary duct for directing the exhaust gas vector. The system has means for maintaining a generally consistent relative alignment between the primary duct and the secondary duct.
申请公布号 DE07873413(T1) 申请公布日期 2009.07.30
申请号 DE20070873413T 申请日期 2007.06.11
申请人 BELL HELICOPTER TEXTRON INC. 发明人 HOLLIMON, CHARLES;BARBER, JOHN;SHERRER, JOHN;LARAMEE, ROBERT
分类号 F02K1/00;F01N13/08 主分类号 F02K1/00
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