Gas turbine engine support structure

Rotary kinetic fluid motors or pumps – Shaft bearing combined with or retained by arm or vane in...

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Details

4152092, 4152093, 4152094, 4152101, 416244A, F01D 2516

Patent

active

059416831

ABSTRACT:
A bearing support structure for a gas turbine engine comprises an annular array of stator vanes and a radially inner bearing support portion which are interconnected by an annular array of radially extending U-shaped cross-section parts. The U-shaped cross-section parts are interconnected at their radially outer extents and are arranged so that adjacent parts are open in generally opposite axial directions. Such a bearing support structure can carry service pipes with good accessibility and be produced by casting, thereby reducing its cost.

REFERENCES:
patent: 4979872 (1990-12-01), Myers et al.
patent: 4987736 (1991-01-01), Ciokajlo et al.

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