Annular combustor having ceramic liner

Details Annular combustor having ceramic liner Annular combustor having ceramic liner

1980-09-22

1983-04-26

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60753, F02C 720

Patent

active

043808964

ABSTRACT:
An annular combustor for a jet turbine engine of generally rectangular cr-section having an axially-projecting aft exhaust outlet is lined by a plurality of circumferentially-extending heat-insulating liner segments, preferably ceramic, spaced from the metal shell of the combustor by spring-like spacers. The liner segments have offset tabs at their edges to slidably mate with each other and with retaining clips adjacent to the exhaust outlet, thereby being slidably secured to accept expansion of the metal shell without placing appreciable stress on the liner segments. Arcuate, generally planer liner segments along the forward and aft walls of the combustor are keyed in place by a radially-inward flanged liner segment along the outer perimetrical wall of the shell.

REFERENCES:
patent: 3088279 (1963-05-01), Diedrich
patent: 3186168 (1965-06-01), Ormerod et al.
patent: 3594109 (1971-07-01), Penny
patent: 3918255 (1975-11-01), Holden
patent: 3990231 (1976-11-01), Irwin
patent: 4030875 (1977-06-01), Grondahl et al.

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