Jet engine exhaust nozzle flow effector

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8683807
APP PUB NO 20110203288A1
SERIAL NO

13096305

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A jet engine exhaust nozzle flow effector is a chevron formed with a radius of curvature with surfaces of the flow effector being defined and opposing one another. At least one shape memory alloy (SMA) member is embedded in the chevron closer to one of the chevron's opposing surfaces and substantially spanning from at least a portion of the chevron's root to the chevron's tip.

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Patent Owner(s)

  • UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Buehrle, Ralph D Williamsburg, US 2 15
Cabell, Randolph H Hampton, US 4 21
Cagle, Christopher M Yorktown, US 5 30
Cano, Roberto J Yorktown, US 22 139
Hilton, George C Hampton, US 2 15
Silox, Richard J Poquoson, US 1 2
Turner, Travis L Yorktown, US 11 72

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