Turbomachine with integral generator/starter
US7855483B2 · kind B2 · utility
3Cited by
14References
5Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Aug 26, 2009 |
| Grant date | Dec 21, 2010 |
| Priority date | — |
| Expiry date | Aug 26, 2029 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/85
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbomachine such as an aircraft turbojet including an electrical generator/starter that can be mounted and dismounted by axial translation in an upstream enclosure of the turbomachine between the low-pressure compressor and the high-pressure compressor, and couple to electrical cables which extend inside the structural arms of the intermediate casing of the turbomachine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.