发明名称 |
Engine exhaust system with directional nozzle |
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 |
AU2007351593(A1) |
申请公布日期 |
2008.10.23 |
申请号 |
AU20070351593 |
申请日期 |
2007.06.11 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
ROBERT LARAMEE;JOHN SHERRER;CHARLES HOLLIMON;JOHN BARBER |
分类号 |
F02K1/00;F01N13/08 |
主分类号 |
F02K1/00 |
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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