Gas turbine engine with a means of driving the accessory...

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

Reexamination Certificate

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Details

C060S039162, C060S802000

Reexamination Certificate

active

08074455

ABSTRACT:
A twin-spool gas turbine engine including a high-pressure rotor and a low-pressure rotor, which rotors are mounted in bearings supported by an intermediate casing, at least one accessory gear box, and a drive device which drives radial and coaxial shafts for transmitting movement to the accessory gear box is disclosed. The drive device includes a high-pressure drive gear driving one of the radial shafts and connected to the high-pressure rotor and a low-pressure drive gear connected to the low-pressure rotor upstream of the high-pressure drive gear and driving the other of the radial shafts. The low-pressure drive gear is supported in the intermediate casing by an axial-positioning bearing.

REFERENCES:
patent: 5103631 (1992-04-01), Edwards et al.
patent: 5349814 (1994-09-01), Ciokajlo et al.
patent: 2006/0277920 (2006-12-01), Bart et al.
patent: 2007/0177935 (2007-08-01), Galivel et al.
patent: 2008/0072568 (2008-03-01), Moniz et al.
patent: 1 574 687 (2005-09-01), None
patent: 1 748 170 (2007-01-01), None
patent: 1 813 792 (2007-08-01), None
patent: 1 323 787 (1973-07-01), None

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