Specially configured deflection edge thrust reverser for jet engine
US5716025A · kind A · utility
12Cited by
10References
13Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 14, 1995 |
| Grant date | Feb 10, 1998 |
| Priority date | — |
| Expiry date | Dec 14, 2015 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The reverser includes a partition (28) exhibiting openings (19) and separating the cavity (16) which exists, when the doors (2) are in the closed position, between the front part (7) of the internal panel (11) of the door and the stream of gaseous flow (15) flowing in direct jet mode through the jet pipe CA, thus overcoming the aerodynamic losses which result from the presence of this cavity.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.