Heat protective lining for an afterburner or transition duct of

Details Heat protective lining for an afterburner or transition duct of Heat protective lining for an afterburner or transition duct of

1990-05-08

1991-12-03

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60752, 60757, 60 3931, F02R 310, F02C 720

Patent

active

050690345

ABSTRACT:
A heat protective lining for the afterburner or transition duct of a turbojet engine comprises an assembly of tiles overlapping laterally and longitudinally to form overlapping rings of tiles in which the tiles of each ring are offset laterally from those of each adjacent ring by half a tile width. The tiles are held together by eyelets projecting from the overlapped downstream portions of the tiles through apertures in the overlapping upstream portions, and locking members engaging through the eyelets. Fastening yokes for fixing the assembly to the duct casing are secured to the outside of the tiles.

REFERENCES:
patent: 2651912 (1953-09-01), Abbott
patent: 3422620 (1967-05-01), Fantozzi
patent: 4614082 (1986-09-01), Sterman
patent: 4628694 (1986-12-01), Kelm
patent: 4773227 (1988-09-01), Chabis

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