Heat protective lining for a passage in a turbojet engine

Details Heat protective lining for a passage in a turbojet engine Heat protective lining for a passage in a turbojet engine

1990-03-07

1992-01-14

Casaregola, Louis J.

Power plants

Reaction motor

Liquid oxidizer

60753, 60757, F02K 310, F02C 100

Patent

active

050799150

ABSTRACT:
A heat protective lining for a passage in a turbojet engine is formed of tiles arranged side by side to form rings which are themselves arranged end to end. Each tile comprises a panel provided at its upstream and downstream edges with radially outwardly directed flanges forming circumferential stiffeners, the upstream flange having on its upstream radial face male securing and sealing means cooperating with complementary female means on the downstream radial face of the downstream flange of the adjacent upstream tile.

REFERENCES:
patent: 4480436 (1984-11-01), Maclin
patent: 4567730 (1986-02-01), Scott
patent: 4614082 (1986-09-01), Sterman et al.
patent: 4655044 (1987-04-01), Dierberger
patent: 4912922 (1990-04-01), Maclin

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