Turbine frame stiffening rails

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60 3975, F02C 720

Patent

active

054837928

ABSTRACT:
A turbine frame includes outer and inner coaxially disposed annular casings having a plurality of circumferentially spaced apart struts extending therebetween is provided with at least one and preferably two axially spaced apart polygonal stiffening rails, a forward rail and an aft rail, circumferentially disposed on the outer annular casing. The rails have at least a first section with a constant cross-sectional area normal to the casing in a circumferential direction around the outer casing, a linear centroid distribution of the cross-sections in the circumferential direction, and the centroids lie in a first plane P1 which is parallel to and spaced apart from a second plane P2 that is tangential to the outer casing mid-way between adjacent struts.

REFERENCES:
patent: 2616662 (1952-11-01), Mierley
patent: 2724544 (1955-11-01), Hardigg
patent: 3024969 (1962-03-01), Russell
patent: 3166903 (1965-01-01), White
patent: 3303998 (1967-02-01), Koff et al.
patent: 3313105 (1967-04-01), Johnson
patent: 3403889 (1968-10-01), Ciokajlo
patent: 3708242 (1973-01-01), Bruneau et al.
patent: 4492078 (1985-02-01), Williamson
patent: 4987736 (1991-01-01), Ciokajlo et al.
patent: 5076049 (1991-12-01), Von Benken et al.
patent: 5180282 (1993-01-01), Lenhart et al.
GEK 9894, Page from GE Parts Manual for LM6000 Engine pp. 2-178, published Dec. 1, 1992.

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