Turbomachine with integral generator/starter

Electrical generator or motor structure – Dynamoelectric – Rotary

Reexamination Certificate

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Details

C310S052000, C310S053000, C310S054000, C310S064000, C310S090000, C310S091000, C310S114000, C310S059000, C415S122100

Reexamination Certificate

active

07855483

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.

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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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