Electronically controlled rotary actuator for an aircraft control surface

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United States of America Patent

PATENT NO 10633080
APP PUB NO 20180022441A1
SERIAL NO

15216963

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A method and apparatus for positioning a control surface. A desired position for the control surface associated with an aerodynamic aircraft structure is identified. The control surface is moved to the desired position using an electronically controlled rotary actuator system located inside of the aerodynamic aircraft structure, wherein a shape of the aerodynamic aircraft structure with the electronically controlled rotary actuator system has a desired aerodynamic performance.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY929 LONG BRIDGE DRIVE ARLINGTON VA 22202

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Huynh, Neal Van Bellevue, US 13 46
McCormick, Patrick Joseph Mukilteo, US 5 30

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