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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Conversion system fault management system for tiltrotor aircraft

Invented by: Kenneth E. Builta
Euless, TX

Originally Assigned to: Bell Helicopter Textron Inc.
Hurst, TX
[Now assigned to . . .]

Issued:2012-09-18
Filed:2006-08-21
Application No:11507035
Examined by:Nguyen; Cuong H

The difference between a first position of a first pylon of a tiltrotor aircraft and a second position of a second pylon of the aircraft is prevented from becoming too large. An actuator position error for the first pylon is calculated from a difference between the first position and a commanded first position of the first pylon. An actuator position error for the second pylon is calculated from a difference between the second position and a commanded second position of the second pylon. An absolute value of the actuator position error for the first pylon is compared to the preset limit. If the absolute value of the actuator position error for the first pylon is greater than or equal to a preset limit, the actuator position error for the second pylon is calculated from the difference between the first position and the second position.

[pdf] U.S. Pat. No. 8,271,149

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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