Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle with jacketed or hollow... – With subsequent mixing in main discharge stream in or...
Patent
1976-11-03
1978-06-06
Stoner, Jr., Bruce H.
Fluid sprinkling, spraying, and diffusing
Reaction motor discharge nozzle with jacketed or hollow...
With subsequent mixing in main discharge stream in or...
23926529, 23926537, 244 125, 244 23D, 244110B, B64C 1506, B64D 3304
Patent
active
040931226
ABSTRACT:
A relatively simple variable area divergent exhaust nozzle and low drag afterbody integrated with a target-type thrust reverser and used in conjunction with a convergent nozzle for application to the propulsion system of a high performance jet powered aircraft. Two or more aerodynamically shaped afterbody surfaces may be pivoted with a common actuation system to form: first an efficient nozzle-afterbody suitable for subsonic operation; second, a divergent nozzle-afterbody for efficient supersonic operation and; third, a target-type thrust reverser for in-flight or ground roll deceleration.
REFERENCES:
patent: 2651172 (1953-09-01), Kennedy
patent: 3684182 (1972-08-01), Maison
Hom Felix
Linderman Duane L.
Gilliam Frank D.
Kashnikow Andres
Rohr Industries, Inc.
Schlesinger Patrick J.
Stoner Jr. Bruce H.
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