Fan cowl support for a turbofan engine
US8272595B2 · kind B2 · utility
2Cited by
6References
19Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 27, 2009 |
| Grant date | Sep 25, 2012 |
| Priority date | — |
| Expiry date | Aug 8, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D29/08
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A fan cowl support for an aircraft having an engine pylon, an engine fan case and an engine fan cowl. The fan cowl support includes a support having a forward end connected to the engine fan case and an aft end connected to the engine pylon. At least a portion of the engine fan cowl is connected to the support.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.