Thrust reverser for a turbofan gas turbine engine
US8127530B2 · kind B2 · utility
7Cited by
151References
25Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 19, 2008 |
| Grant date | Mar 6, 2012 |
| Priority date | — |
| Expiry date | Sep 21, 2030 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T29/494
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The thrust reverser comprises sections, such as arms and skins, which may be connected along joints to provide a thrust reverser body. A plurality of fittings may be integrally formed on a surface of each arm.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.