Circumferentially retained fairing
US9297312B2 · kind B2 · utility
9Cited by
64References
13Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 29, 2012 |
| Grant date | Mar 29, 2016 |
| Priority date | — |
| Expiry date | May 22, 2034 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2250/42
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An assembly for a gas turbine engine includes a frame, a mount, and a fairing. The mount is attached to the frame and the fairing is connected to the mount. The fairing and mount have mating anti-deflection features that engage to prevent circumferential movement of the fairing relative to the frame.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.