Dual anti surge and anti rotation feature on first vane support
US10337354B2 · kind B2 · utility
0Cited by
8References
15Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 3, 2014 |
| Grant date | Jul 2, 2019 |
| Priority date | — |
| Expiry date | Jul 7, 2036 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/36
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes a vane and a combustor housing that are supported relative to an engine static structure. A retaining assembly clamps the combustor housing and the vane to one another in an axial direction. A circumferential load transfer assembly circumferentially affixes the vane relative to the engine static structure. The retaining assembly is secured to the circumferential load transfer assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.