Rotor support structure for a gas turbine engine

Power plants – Reaction motor – Air passage bypasses combustion chamber

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Details

415170R, F02K 302, F01D 2516

Patent

active

041977025

ABSTRACT:
A rotor support structure for a gas turbine engine comprises a rolling element bearing adapted to carry the rotor, a structurally strong ring adapted to carry the rolling element bearing, and two pairs of supporting struts for the ring, extending substantially tangentially from the ring, each pair joining at a mounting, the two mountings being diametrically opposed with respect to the ring.

REFERENCES:
patent: 2410450 (1946-11-01), Kroon
patent: 2933893 (1960-04-01), Blyth et al.
patent: 2938336 (1960-05-01), Peterson
patent: 2941781 (1960-06-01), Boyum
patent: 3830058 (1974-08-01), Ainsworth

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