Gas turbine engine

Details Gas turbine engine Gas turbine engine

1977-09-22

1979-04-03

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

With lubricators

60 3936, F02C 706

Patent

active

041470265

ABSTRACT:
A gas turbine engine which includes one of a radial compressor or a combined axial-radial compressor, a reversing annular combustion chamber, a compressor drive turbine and a gas generator rotor. The gas generator rotor is rotatably mounted in the gas turbine engine by way of at least one movable bearing and a fixed bearing. A bearing spider is provided for the fixed bearing and is disposed behind the radial compressor and in front of the compressor drive turbine. The bearing spider is designed with a box construction so as to resist axial forces.

REFERENCES:
patent: 2439273 (1948-04-01), Silvester
patent: 3014694 (1961-12-01), Paul et al.
patent: 3088278 (1963-05-01), Franz
patent: 3546880 (1970-12-01), Schwaar
patent: 3623318 (1971-11-01), Shank

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