Gas turbine engine component with discharge slot having oval geometry
US10107107B2 · kind B2 · utility
1Cited by
11References
22Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Aug 30, 2012 |
| Grant date | Oct 23, 2018 |
| Priority date | — |
| Expiry date | Feb 4, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an body portion that extends between a leading edge and a trailing edge. At least one of the leading edge and the trailing edge includes at least one discharge slot having a first portion that includes an oval geometry.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.