Rotor assembly for a gas turbine engine and method of disassembl

Details Rotor assembly for a gas turbine engine and method of disassembl Rotor assembly for a gas turbine engine and method of disassembl

1984-05-02

1986-09-16

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

415189, F02C 106, F02C 310

Patent

active

046114645

ABSTRACT:
A rotor assembly 22 for a gas turbine engine is disclosed. The engine has a compression section 12 and a turbine section 16. Various construction details which enable the modular disassembly of the turbine section are developed. The rotor assembly includes a rotor shaft 42 extending between the compression section and the turbine section. An annular shaft 66 engages a bearing 64, is joined to a rotor blade assembly 74, and rotatably supports the rotor shaft 42.

REFERENCES:
patent: 2862356 (1958-12-01), Kent et al.
patent: 3526092 (1970-09-01), Steel
patent: 3546880 (1970-12-01), Schwaar
patent: 3620009 (1971-11-01), Wilde
patent: 3673802 (1972-04-01), Krebs et al.
patent: 3756672 (1973-09-01), Hibner
patent: 3792586 (1974-02-01), Kasmarik et al.
patent: 3823553 (1976-07-01), Smith
patent: 3915521 (1975-10-01), Young
patent: 4418528 (1983-12-01), Pellow

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