Eccentric flap nozzle

Power plants – Reaction motor – With thrust direction modifying means

Patent

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Details

60232, F02K 100

Patent

active

050818350

ABSTRACT:
Disclosed is a two-dimensional nozzle for a gas turbine engine which, through the use of divergent flaps mounted on pivot shafts eccentric to the side disks in which they are received, provides thrust vectoring and low observability flight operation.

REFERENCES:
patent: 4819876 (1989-04-01), Thayer

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