Rotor assembly for gas turbine engine
US8540482B2 · kind B2 · utility
2Cited by
49References
19Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 7, 2010 |
| Grant date | Sep 24, 2013 |
| Priority date | — |
| Expiry date | Sep 19, 2031 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF01D5/3069
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A rotor assembly for a gas turbine engine includes a rotor airfoil and a first rotor disk. The rotor airfoil extends along a radial axis. The first rotor disk includes an outer rim, a bore and a web extending between the outer rim and the bore. The first rotor disk is axially offset from the radial axis of the rotor airfoil.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.