Arrangement and method for installing a component in an aircraft
US7992821B2 · kind B2 · utility
1Cited by
3References
14Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Nov 28, 2007 |
| Grant date | Aug 9, 2011 |
| Priority date | — |
| Expiry date | Mar 18, 2029 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C1/06
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An arrangement (10) for installing a component (12) in an aircraft comprises a guide device (14) which is connectable to an aircraft structure or is formed integrally with the aircraft structure, as well as an elastically deformable damping element (16; 16a, 16b, 16c) which is adapted to enable the component (12) to be mounted in the guide device (14) in a self-supporting manner. A locking mechanism (26) is adapted to fasten the component (12) in a desired position in the guide device (14) in a releasable manner.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.