Single-skin thrust reverser for aircraft jet engines
US4129269A · kind A · utility
Assignee
Inventor
Key dates
| Filing date | Apr 4, 1977 |
| Grant date | Dec 12, 1978 |
| Priority date | — |
| Expiry date | Apr 4, 1997 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Thrust reverser for a jet engine of an aircraft, comprising two symmetrical doors mounted to pivot about an axis which is transverse and substantially diametrical with respect to the jet of the engine and which is disposed downstream of the jet exhaust pipe thereof, the doors being adapted to occupy a folded or stowed position in which they form part of the fairing of the engine or fuselage of the aircraft, or an unfolded or opened out position for which they are disposed transversely with respect to the jet. According to the invention, each of the doors is formed by a single skin which is at least substantially hemi-truncated in shape.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.