Generator-starter system for a multi-shaft engine

Prime-mover dynamo plants – Turbogenerators

Reexamination Certificate

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Details

C060S791000, C310S058000

Reexamination Certificate

active

07745950

ABSTRACT:
In order to provide a high electric power for an aircraft via a generator driven by the engine, an additional free turbine is included in the hot-gas flow of the engine, which—equipped with generator-starter magnets (9) and surrounded by annularly arranged generator-starter coils (12)—forms a generator-starter turbine (5) and is connected to the high-pressure shaft (1) via an overrunning clutch (15), and hence, is also used for starting the engine.

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European Search Report dated Mar. 5, 2010 from corresponding patent application.

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