Uniform cooling film replenishment thermal liner assembly

Details Uniform cooling film replenishment thermal liner assembly Uniform cooling film replenishment thermal liner assembly

1992-12-18

1993-11-30

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

60 393, 60752, F02C 700

Patent

active

052654095

ABSTRACT:
A gas turbine engine liner assembly is disclosed having uniformly spaced rows of cooling orifices oriented perpendicular to the combustion gas flow of the engine. The orifices within each row are spaced equidistant from adjacent orifices within the same row, thereby providing a uniform, uninterrupted pattern of cooling orifices over the hot side of the liner. The liner is secured to a component of the gas turbine engine by a plurality of fasteners which are secured to the liner without affecting the uniform pattern of the cooling orifices.

REFERENCES:
patent: 3199294 (1965-08-01), Hagen
patent: 3500639 (1970-03-01), Stamm
patent: 3854285 (1974-12-01), Stenger et al.
patent: 4422300 (1983-12-01), Dierberger et al.
patent: 4512159 (1985-04-01), Memmen
patent: 4848089 (1989-07-01), Crmaer
patent: 5055032 (1991-10-01), Altemark et al.
patent: 5083424 (1992-01-01), Becker
patent: 5103638 (1992-04-01), Roberts et al.
patent: 5129447 (1992-07-01), Hammer

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