Stator vane shroud having an offset
US9840917B2 · kind B2 · utility
0Cited by
20References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 13, 2011 |
| Grant date | Dec 12, 2017 |
| Priority date | — |
| Expiry date | Aug 14, 2035 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/37
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An example stator vane assembly of a turbomachine includes a shroud having a leading edge, a trailing edge, and at least one circumferential edge. The leading edge is circumferentially offset relative to the trailing edge when installed within the turbomachine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.