ELECTRONIC MOTOR ACTUATORS BRAKE INHIBIT FOR AIRCRAFT BRAKING SYSTEM

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20110226569A1
SERIAL NO

12728133

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A brake system control unit controls one of first and second portions of a wheel brakes electric brake actuators to activate one of the first and second portions of the actuators and deactivate the other during an inhibited braking mode. The control unit controls the activated portion of the brake actuators to generate a braking force greater than the commanded braking force of the brake pedal command, such as twice the commanded braking force, to compensate for the deactivated portion of the brake actuators. The inhibited braking mode is discontinued during emergency braking when the commanded braking force is greater than or equal to a predetermined braking force. The inhibited braking mode is also discontinued when failure of one or more brake actuators is detected.

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Patent Owner(s)

Patent OwnerAddress
HYDRO-AIRE INC A SUBSIDIARY OF CRANE CO3000 WINONA AVENUE BURBANK CA 91510-7722

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
DEVLIEG, GARRETT H BELLEVUE, US 24 401

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