Power plants – Reaction motor – With thrust direction modifying means
Patent
1990-10-12
1992-01-21
Casaregola, Louis J.
Power plants
Reaction motor
With thrust direction modifying means
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
Casaregola Louis J.
Hayes Christopher T.
Richman Howard R.
United Technologies Corporation
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