The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 23, 2009

Filed:

Jul. 29, 2005
Applicants:

Casey Hanlon, Queen Creek, AZ (US);

Paul T. Wingett, Mesa, AZ (US);

Calvin C. Potter, Mesa, AZ (US);

Inventors:

Casey Hanlon, Queen Creek, AZ (US);

Paul T. Wingett, Mesa, AZ (US);

Calvin C. Potter, Mesa, AZ (US);

Assignee:

Honeywell International Inc., Morristown, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/50 (2006.01);
U.S. Cl.
CPC ...
Abstract

An aircraft flight control surface actuation system includes a plurality of electric motors-driven flap actuators, and a plurality of electric motor-driven slat actuators. The motor-driven actuators receive activation signals from flap and slat actuator controllers and is, in response to the activation signals, move the flaps and slats between stowed and a deployed positions. The flap and slat actuator controllers each include a plurality of independent actuator control channels that independently supply the activation signals to the motor-driven actuators.


Find Patent Forward Citations

Quick Actions:

Hanlon, Casey. (2009). Electric flight control surface actuation system for aircraft flaps and slats (U.S. Patent No. 7549605). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/7549605

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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