Thrust reverser for a dual-flow turbine engine nacelle
US8793973B2 · kind B2 · utility
18Cited by
1References
15Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | May 18, 2010 |
| Grant date | Aug 5, 2014 |
| Priority date | — |
| Expiry date | Sep 4, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The invention relates to a thrust reverser (1) for the nacelle of a dual-flow turbine engine, in which the bypass means (4) and the actuation jacks (22) of the sliding cowling (2) and of the reverse flaps (20) are arranged in two substantially parallel planes arranged above one another in the radial direction of the nacelle. The invention also relates to a nacelle for a dual-flow turbine engine that comprises such a thrust reverser.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.