Thrust reversing variable area nozzle

Details Thrust reversing variable area nozzle Thrust reversing variable area nozzle

2011-08-30

2011-08-30

Casaregola, Louis J. (Department: 3741)

Power plants

Reaction motor

Interrelated reaction motors

C060S230000

Reexamination Certificate

active

08006479

ABSTRACT:
A gas turbine engine system includes a first nozzle section associated with a gas turbine engine bypass passage and a second nozzle section that includes a plurality of positions relative to the first nozzle section. In at least one of the positions, there is a gap between the first nozzle section and the second nozzle section. A movable door between the first nozzle section and the second nozzle section selectively opens or closes the gap.

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