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 |
US2011131948(A1) |
申请公布日期 |
2011.06.09 |
申请号 |
US20070303970 |
申请日期 |
2007.06.11 |
申请人 |
HOLLIMON CHARLES;BARBER JOHN;SHERRER JOHN;LARAMEE ROBERT |
发明人 |
HOLLIMON CHARLES;BARBER JOHN;SHERRER JOHN;LARAMEE ROBERT |
分类号 |
F02K1/00;F01N13/08 |
主分类号 |
F02K1/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|