Mounting system for a gas turbine engine
US8118251B2 · kind B2 · utility
17Cited by
38References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jan 18, 2008 |
| Grant date | Feb 21, 2012 |
| Priority date | — |
| Expiry date | Dec 23, 2030 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C7/20
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A mounting system for a gas turbine engine includes a thrust ring and a linkage assembly. The linkage assembly is at least partially received by the thrust ring. The linkage assembly reacts at least a side load and a thrust load communicated from the thrust ring.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.