Cooling scheme for scramjet variable geometry hardware

Details Cooling scheme for scramjet variable geometry hardware Cooling scheme for scramjet variable geometry hardware

2006-10-10

2006-10-10

Kim, Ted (Department: 3746)

Power plants

Reaction motor

Air supplied by ram effect

C060S267000

Reexamination Certificate

active

07117680

ABSTRACT:
A cooling system for use in an engine having an element to be cooled includes at least one cooling channel on a first side of the element, at least one cooling channel on a second side of the element, and the at least one cooling channel on the first side communicating with the at least one channel on the second side in a nose region of the element so as to form a cooling circuit. The cooling system has particular utility in cooling interior and exterior surfaces of a movable cowl inlet flap used in a scramjet engine.

REFERENCES:
patent: 3407603 (1968-10-01), Kelley et al.
patent: 3669811 (1972-06-01), Jarvis et al.
patent: 5116251 (1992-05-01), Bichler et al.
patent: 6109038 (2000-08-01), Sharifi et al.
patent: 7000398 (2006-02-01), Bouchez et al.

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