Blade retainer for gas turbine engine
US11339674B2 · kind B2 · utility
0Cited by
15References
14Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Aug 14, 2018 |
| Grant date | May 24, 2022 |
| Priority date | — |
| Expiry date | Nov 28, 2040 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2300/6033
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A blade retainer adapted for use in a gas turbine engine is configured to block axial movement of a blade. The blade retainer includes a first brace, a second brace, and a web that extends between the first brace and the second brace. The blade retainer is configured to block axial movement of a root of the blade out of a blade receiver slot.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.