基本信息:
- 专利标题： Engine Exhaust System with Directional Nozzle
- 专利标题（中）：具有方向喷嘴的发动机排气系统
- 申请号：US12303970 申请日：2007-06-11
- 公开(公告)号：US20110131948A1 公开(公告)日：2011-06-09
- 发明人： Charles Hollimon , John Barber , John Sherrer , Robert Laramee
- 申请人： Charles Hollimon , John Barber , John Sherrer , Robert Laramee
- 国际申请： PCT/US07/13675 WO 20070611
- 主分类号： F02K1/00
- IPC分类号： F02K1/00
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.
摘要（中）：
用于飞行器的排气系统具有用于将来自发动机排气出口的废气连通并且被构造成与发动机一起运动的主排气管道。 二次排气管道与主排气管道流体连通并且可移动地安装到机身。 次级管道具有相对于辅助管道的其余部分选择性地可旋转的部分，用于引导废气向量。 该系统具有用于维持主管道和次管道之间的大致一致的相对对准的装置。
公开/授权文献:
- US08132755B2 Engine exhaust system with directional nozzle 公开/授权日：2012-03-13
IPC结构图谱:
| F | 机械工程；照明；加热；武器；爆破 |
| --F02 | 燃烧发动机；热气或燃烧生成物的发动机装置 |
| ----F02K | 喷气推进装置 |
| ------F02K1/00 | 以喷管或喷嘴的结构或配置为特征的装置；特有的喷管或喷嘴 |