Gas turbine engine assembly and method of assembling same
US8584464B2 · kind B2 · utility
6Cited by
25References
16Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 20, 2005 |
| Grant date | Nov 19, 2013 |
| Priority date | — |
| Expiry date | Nov 24, 2028 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2270/304
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A method for assembling a gas turbine engine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a high-pressure turbine, and coupling a low-pressure compressor between the core gas turbine engine and a motor such that the low-pressure compressor is driven only by the motor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.