Insulated cooling liner

Power plants – Reaction motor – Means to flow film on surface

Patent

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Details

60261, B64D 3300, F02K 310

Patent

active

050604724

ABSTRACT:
This disclosure is for a liner for the exit nozzle of a gas turbine engine. The liner is double walled liner with insulation material between the walls, and with a plurality of tubes extending through the walls and the insulation. Primary cooling is accomplished by film cooling through the tubes. During periods of low coolant medium flow, the liner provides a barrier against radiation and convection. The use of the insulating material allows both walls of the liner to carry the pressure loads.

REFERENCES:
patent: 3349558 (1967-10-01), Smith
patent: 3584972 (1971-06-01), Bratkovich
patent: 4071194 (1978-01-01), Eckert et al.
patent: 4422300 (1983-12-01), Dierberger et al.
patent: 4709643 (1987-12-01), Moreno et al.
patent: 4749150 (1988-06-01), Rose et al.
patent: 4773593 (1988-09-01), Auxier et al.
patent: 4817378 (1989-04-01), Giffin, III et al.

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