Gas turbine engine arrangement

Details Gas turbine engine arrangement Gas turbine engine arrangement

1991-10-15

1993-04-13

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3931, F02C 306, F02C 706

Patent

active

052017966

ABSTRACT:
A separate low pressure shaft and a high pressure shaft are axially aligned. The low pressure shaft is at one end and carries the low pressure compressor and the low pressure turbine, and is connected to the electric generator. The high pressure shaft carries the high pressure compressor and the high pressure turbine. Only three bearing housings are required. Parts of the casing are horizontally split to simplify maintenance.

REFERENCES:
patent: 2704434 (1955-03-01), Schmitt
patent: 4147024 (1979-04-01), Moellmann
patent: 4829763 (1989-05-01), Rao
patent: 4893466 (1990-01-01), Egnell et al.
Shepherd, D. G. Introduction to the Gas Turbine Constable & Company, London, 1960, pp. 56-57.

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