Orientable axisymmetric nozzle of variable geometry of gas turbi

Details Orientable axisymmetric nozzle of variable geometry of gas turbi Orientable axisymmetric nozzle of variable geometry of gas turbi

1994-04-25

1995-03-21

Thorpe, Timothy S.

Power plants

Reaction motor

With thrust direction modifying means

60271, 23926535, 23926539, F02K 112

Patent

active

053984994

ABSTRACT:
Orientable axisymmetric nozzle of variable geometry for gas turbine engines which comprises convergent (2) and divergent (3) sections formed by master petals (4, 5) and slave petals (33, 34) duly connected together, each divergent master petal (5) being connected to an outer annular control part (6) by a biarticulated bar (15). This bar is connected by one end to the part (6) by a cylindrical articulation (16) while by its opposite end it is connected to the divergent master petal (5) via intermediate bars (26, 27).

REFERENCES:
patent: 4420932 (1983-12-01), Mendez et al.
patent: 4662566 (1987-05-01), Honeycutt, Jr.
patent: 4690330 (1987-09-01), Robinson et al.
patent: 4994660 (1991-02-01), Hauer
patent: 5039014 (1991-08-01), Lippmeier
patent: 5076496 (1991-12-01), Lippmeier
patent: 5082182 (1992-01-01), Bruchez, Jr. et al.
patent: 5285637 (1994-02-01), Barcza
patent: 5328098 (1994-07-01), Barcza et al.
patent: 5335489 (1994-08-01), Thayer

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