Turbine engine nozzle

Details Turbine engine nozzle Turbine engine nozzle

2006-03-07

2006-03-07

Gartenberg, Ehud (Department: 3746)

Power plants

Reaction motor

Particular exhaust nozzle feature

Reexamination Certificate

active

07007483

ABSTRACT:
A convergent/divergent nozzle for a gas turbine engine has a throat portion of non-constant radius of curvature varying from an upstream high value to an intermediate low value and then to a downstream high value.

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