Power plants – Reaction motor – Particular exhaust nozzle feature
Reexamination Certificate
2007-02-13
2007-02-13
Rodriguez, William H. (Department: 3746)
Power plants
Reaction motor
Particular exhaust nozzle feature
C239S265190, C060S228000
Reexamination Certificate
active
10801265
ABSTRACT:
A device for controlling propulsive gas mixing at an outlet of an aircraft jet engine, wherein propulsive jets are composed of a hot primary jet exiting from a nozzle of the jet engine and a secondary flux flowing between an external wall of the nozzle and an internal wall of the jet engine including a divergent trailing edge on the wall that generates conditions of a separation of the primary jet close to an existence limit value and a primary jet controller that enables control of passage of the primary jet from a separated state to a reattached state, and vice versa.
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Bonnet Jean-Paul
Collin Erwan
Delville Joel
Moreau Eric
Tensi Jean
Centre National de la Recherche Scientifique--CNRS
DLA Piper (US) LLP
Rodriguez William H.
LandOfFree
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