Seal for gas turbine engines
US10082085B2 · kind B2 · utility
17Cited by
14References
7Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Nov 17, 2014 |
| Grant date | Sep 25, 2018 |
| Priority date | — |
| Expiry date | Dec 2, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine assembly includes a support component, an engine component, and a seal. The annular support component is formed to include a notch. The engine component is mounted in spaced-apart relation to the support component so that a gap is formed between the support component and the engine component. The seal is located in the notch and is adapted to close the gap.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.