Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft
US5181675A · kind A · utility
18Cited by
11References
6Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 22, 1992 |
| Grant date | Jan 26, 1993 |
| Priority date | — |
| Expiry date | May 22, 2012 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/18
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A pod for suspending a turbojet engine unit below the wing of an aircraft includes a suspension assembly with two laterally spaced front beams connecting the turbojet fan casing to the wing, and two rear links disposed in a common vertical plane and pivotally connected at one end to the wing and at the other end to a connection link which is connected at least to the exhaust casing of the engine, the front beams being interconnected by cross-bracing and being connected at the level of the downstream edge of the cross-bracing to at least one fixed part of the engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.