Ventral segmented nozzles for promoting rapid temperature and pr

Details Ventral segmented nozzles for promoting rapid temperature and pr Ventral segmented nozzles for promoting rapid temperature and pr

1989-02-08

1991-12-31

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft, heavier-than-air

Fluid sustained

244 124, 244 125, B64C 2900

Patent

active

050765124

ABSTRACT:
A thrust deflector system for VSTOL aircraft. The thrust directing system consists of a number of spaced-apart, downwardly facing openings along the bottom of the fuselage. The openings are fluidly connected with the outlet of the aircraft engine so that pressurized gas from the aircraft engine is discharged through the openings and away from the fuselage in discrete spaced-apart jets.

REFERENCES:
patent: Re31591 (1984-05-01), Drakeley
patent: 3099423 (1963-07-01), Wild et al.
patent: 3159362 (1964-12-01), Laing
patent: 3174707 (1965-03-01), Ricard
patent: 3212731 (1961-10-01), Koppus
patent: 3258206 (1966-06-01), Simonson
patent: 3310260 (1967-03-01), Chichester-Miles
patent: 3310948 (1961-03-01), Culp
patent: 3348380 (1967-10-01), Rees
patent: 3380661 (1968-04-01), Markowski
patent: 3380661 (1968-04-01), Markowski
patent: 3491970 (1970-01-01), MaGuire
patent: 3545210 (1970-12-01), Cresswell
patent: 3545701 (1970-12-01), Bertin
patent: 3611725 (1971-10-01), Short
patent: 3664611 (1972-05-01), Harris
patent: 3770227 (1973-11-01), Van Ohain et al.
patent: 3819134 (1974-06-01), Throndson
patent: 3830451 (1974-08-01), Fosness
patent: 3831887 (1974-08-01), Fosness
patent: 3860200 (1975-01-01), Petrushka
patent: 3893638 (1975-07-01), Kelley
patent: 3941335 (1976-03-01), Viets
patent: 4171112 (1979-10-01), Harvey
patent: 4205813 (1980-06-01), Evans et al.
patent: 4235397 (1980-11-01), Compton
patent: 4248041 (1981-02-01), Wilde et al.
patent: 4301980 (1981-11-01), Bradfield
patent: 4343446 (1982-08-01), Langley
patent: 4391424 (1973-07-01), Bartoe, Jr.
patent: 4392621 (1983-07-01), Viets
National Aeronautics and Space Administration Exhaust Jet Wake and Thrust Characteristics of Several Nozzles Designed for VTOL Downwash Suppression Tests In and Out of Ground Effect with 70.degree. F. and 1200.degree. F. Nozzle Discharge Temperatures by: C. C. Higgins, D. P. Kelly and T. W. Wainwright.

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