Seal for a gas turbine engine assembly
US10443419B2 · kind B2 · utility
17Cited by
17References
17Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Mar 25, 2016 |
| Grant date | Oct 15, 2019 |
| Priority date | — |
| Expiry date | Jan 11, 2038 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2250/75
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine assembly includes a seal formed by the interface between first and second support components. The support components are each formed to include a notch. Adjacent notches cooperate to form a space when assembled. A seal member is located in the space.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.