Finned surface cooled nozzle

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle with jacketed or hollow... – With subsequent mixing in main discharge stream in or...

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Details

60265, 23926539, B64C 1506, B64D 3304, F02K 112, F02K 1102

Patent

active

040811379

ABSTRACT:
An air-cooled, variable-throat, convergent-divergent nozzle for a turbojet engine. Active cooling constituent structures of the nozzle include: passages, for flow of cooling air, integral to, and within, convergent and divergent flaps and seal members; finned sections in nozzle components which are provided air from the passages; air exit slots on the convergent flaps; a hinged connection at each convergent flap-to-divergent flap (and divergent seal member) interconnection; staggered air outlet openings in each divergent flap; and, a tubular air feed system to provide cooling air from each divergent flap to an adjacent cooperating divergent seal member. Passive cooling is accomplished: by seal members overlapping adjacent side edges of convergent and divergent flaps, preventing leaking of cooling air and hot gas through the side edges; and, by a sealing hinged connection at each convergent flap-to-divergent flap (and divergent seal member) interconnection.

REFERENCES:
patent: 2801516 (1957-08-01), Battle et al.
patent: 2972226 (1961-02-01), Geary
patent: 2984068 (1961-05-01), Eatock
patent: 2989845 (1961-06-01), Howald
patent: 2999354 (1961-09-01), Gallo et al.
patent: 3979065 (1976-09-01), Madden

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