2-D propulsive lift nozzle

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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244 125, 244 23D, 23926519, B64C 1500

Patent

active

047141972

ABSTRACT:
A two-dimensional nozzle for directing the exhaust of a gas turbine engine includes two spaced apart vertical sidewalls (16), an upper flap assembly (18) and a lower flap assembly (20). The upper flap assembly (20) includes at least a dorsal flap (22) pivotable about a first fixed axis (24). The lower flap assembly (20) includes a ventral flap (28) centrally pivotable about a second fixed axis (30) for creating a dual throat exhaust flow path.

REFERENCES:
patent: 2951660 (1960-09-01), Gilihenty
patent: 4000854 (1977-01-01), Konarski
patent: 4052007 (1977-10-01), Willard
patent: 4175385 (1979-11-01), Nash
patent: 4375276 (1983-03-01), Konarski
patent: 4392615 (1983-07-01), Madden
patent: 4505443 (1985-03-01), Bradfield
patent: 4641782 (1987-02-01), Woodward

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