Turbomachine with integral generator/starter

Details Turbomachine with integral generator/starter Turbomachine with integral generator/starter

2007-01-24

2009-11-17

Leung, Quyen (Department: 2834)

Electrical generator or motor structure

Dynamoelectric

Rotary

C310S071000, C415S122100, C415S170100

Reexamination Certificate

active

07619331

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.

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patent: 1 659 267 (2006-05-01), None
patent: 1 662 636 (2006-05-01), None
patent: WO 2005/059316 (2005-06-01), None

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