Individually removable combustor liner panel for a gas turbine e

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

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Details

60 3932, 60752, 60754, F02C 720, F02G 300

Patent

active

053236017

ABSTRACT:
This invention relates to a combustor liner for a gas turbine engine with means for loosely mounting one of the two spaced liner walls relative to the other to support it so that it "floats". The floating wall is made up of a plurality of segments to permit relatively minimal stress during thermal expansion, and the movement of each segment is restricted by at least one washer, and removal of the washer(s) permits the segment to be individually removed without removal of adjacent segments.

REFERENCES:
patent: Re30160 (1979-11-01), Emory, Jr. et al.
patent: 3706203 (1972-12-01), Goldberg et al.
patent: 4302941 (1981-12-01), DuBell
patent: 4512159 (1985-04-01), Memmen
patent: 4567730 (1986-02-01), Scott
patent: 4773227 (1988-09-01), Chabis
patent: 4901522 (1990-02-01), Commaret et al.
patent: 5055032 (1991-10-01), Altemark et al.

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