基本信息:
- 专利标题： AIRCRAFT PROPULSION ASSEMBLY COMPRISING A THRUST REVERSER
- 申请号：US15745682 申请日：2016-07-21
- 公开(公告)号：US20180209378A1 公开(公告)日：2018-07-26
- 发明人： Nicolas Jérôme Jean Tantot , Antoine Jean-Philippe Beaujard , Pascal Coat , Didier Jean-Louis Yvon
- 申请人： SAFRAN AIRCRAFT ENGINES
- 申请人地址： FR Paris
- 专利权人： SAFRAN AIRCRAFT ENGINES
- 当前专利权人： SAFRAN AIRCRAFT ENGINES
- 当前专利权人地址： FR Paris
- 优先权： FR1556958 20150722
- 国际申请： PCT/FR2016/051884 WO 20160721
- 主分类号： F02K1/76
- IPC分类号： F02K1/76 ; F02C6/02 ; F02K1/60 ; F02K1/70 ; F02K3/06 ; F02K3/072 ; F01D13/02
摘要：
An aircraft propulsion assembly, including a turbine engine comprising at least one gas generator configured to generate a main flow, which is supplied by a central jet to at least one power turbine, the central jet being surrounded by an outer fairing, and the power turbine driving, on the periphery thereof, at least one fan rotor. The aircraft propulsion assembly comprises first movable means which are arranged so as to divert at least some of the main flow from the central jet to the outside of the outer fairing and preferably upstream of the turbine engine so as to generate thrust reversal. An aircraft which uses the propulsion assembly, particularly on the rear tip of the fuselage of the aircraft.
公开/授权文献:
- US11136937B2 Aircraft propulsion assembly comprising a thrust reverser 公开/授权日：2021-10-05
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 |
| --------F02K1/54 | .带有喷气推力反向装置的喷管 |
| ----------F02K1/76 | ..推力反向器的控制或调节 |