Gas turbine engine system having an electric starter motor...

Power plants – Combustion products used as motive fluid – Combined with starting feature

Reexamination Certificate

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Details

C060S786000, C060S802000, C310S07500D, C310S092000, C310S100000, C417S410100, C417S423700

Reexamination Certificate

active

07131275

ABSTRACT:
A gas turbine engine system includes an electric starter motor which utilizes a partially hollow or cupped shaped rotor. Space is provided inside the rotor to fit the required clutch, bearings, and drive shaft. A rotor shaft drives the input shaft through the clutch. The clutch is mounted within a clutch cavity formed within an annular housing portion of the housing. The annular housing portion is at least partially conical and preferably extends at least partially within a hollow rotor mounted to the rotor shaft. A short package is provided due to the telescoped architecture while retaining the maximum length for electromagnetics.

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