Turbomachine with integral generator/starter
US7619331B2 · kind B2 · utility
10Cited by
8References
10Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Jan 24, 2007 |
| Grant date | Nov 17, 2009 |
| Priority date | — |
| Expiry date | Dec 12, 2027 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/85
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Turbomachine such as an aircraft turbojet comprising an electrical generator/starter (26) that can be mounted and dismounted by axial translation in an upstream enclosure (18) of the turbomachine between the low-pressure compressor and the high-pressure compressor, and couple to electrical cables (34) which extend inside the structural arms (12) of the intermediate casing (10) of the turbomachine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.