Augmentor liner construction

Power plants – Reaction motor – Liquid oxidizer

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Details

2391273, 60264, F02K 310

Patent

active

047182300

ABSTRACT:
The cooling air for the nozzle of an augmentor of a gas turbine engine is maintained uniformly around the circumference to assure the prevention of hot streaks that would be occasioned by the liner "sagging". A separate end piece having judiciously located gaps for directing air over the nozzles, flaps and seals attached to the end of the augmentor duct maintains concentricity during augmentor operation, and affords support to the liner of the duct.

REFERENCES:
patent: 2735262 (1956-02-01), Geary
patent: 2794319 (1957-06-01), Stockdale
patent: 2846842 (1958-08-01), Brown
patent: 2974486 (1961-03-01), Edwards
patent: 3825365 (1974-07-01), Peng
patent: 3826088 (1974-07-01), Nash et al.
patent: 3866417 (1975-02-01), Velegol
patent: 3966354 (1976-06-01), Patterson
patent: 3972475 (1976-08-01), Nelson et al.

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