Split disk assembly for a gas turbine engine
US8162615B2 · kind B2 · utility
1Cited by
34References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 17, 2009 |
| Grant date | Apr 24, 2012 |
| Priority date | — |
| Expiry date | Aug 31, 2030 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF01D5/3069
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A split disk assembly for a gas turbine engine includes a forward disk section and an aft disk section, the aft disk section engageable with the forward disk section to retain a multitude of rotor blades therebetween.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.