Cooled variable geometry exhaust nozzle
AssigneeUnited Technologies Corporation
InventorsJames P. Allore, Stephen A. Paul, Charles D. Stoner
Life of this patent
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AssigneeUnited Technologies Corporation
InventorsJames P. Allore, Stephen A. Paul, Charles D. Stoner
Estimating the term…
A variable geometry exhaust nozzle 10 for a turbine engine includes convergent and divergent flaps 12, 18 that circumscribe a gaspath 26 and define convergent and divergent nozzle sections 30, 32 with a throat 34 therebetween. A projection 56, which resides on the divergent flaps, extends radially inwardly from the nozzle. The nozzle also includes a coolant flowpath comprising an interior space 44 in the nozzle, an intake 58 for admitting coolant C into the interior space, and a coolant outlet 60 aft of the intake for discharging the coolant from the interior space. The intake resides forward of the throat. During operation, a coolant film flows along the radially inner surface of the nozzle. The projection encourages a portion of the coolant film to enter and flow through the the coolant flowpath to convectively cool the nozzle. The location of the intake, forward of the throat, takes advantage of the locally high gaspath pressure to ensure that an adequate quantity of the coolant enters and flows through the coolant flowpath.
A variable geometry exhaust nozzle, comprising:
The nozzle of claim wherein 4 the divergent flaps have a length and the discharge ports penetrate the divergent flaps aft of about 50% of the flap length.
A convergent divergent exhaust nozzle, comprising:
Dependencies are inferred from the claim text.