Aeronautics and astronautics – Aircraft – heavier-than-air – Fluid sustained
Patent
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.
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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.
Farbridge Joseph E.
Garland Douglas
Schexnayder Albert F.
Boeing Canada Ltd.
Ellis Christopher P.
General Electric Company
Peters Jr. Joseph F.
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