Arched combustor

Power plants – Combustion products used as motive fluid – Combustion products generator

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F02C 314

Patent

active

053355024

ABSTRACT:
A gas turbine engine combustor includes radially spaced outer and inner liners disposed coaxially about an engine longitudinal centerline axis with each liner having forward and aft ends. An annular dome is fixedly joined to the forward ends of the outer and inner liners. The outer liner has a substantially uniform thickness and is arcuate in a longitudinal plane from the forward to aft ends for providing buckling resistance of the outer liner.

REFERENCES:
patent: 2576046 (1951-11-01), Scarth
patent: 3657882 (1972-04-01), Hugoson
patent: 4109459 (1978-08-01), Ekstedt et al.
patent: 4177637 (1979-12-01), Pask
Lefebvre, Arthur H. Gas Turbine Combustion, New York, N.Y.; McGraw-Hill, 1983, pp. 13, 22, 23, 25.

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