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:
Oct. 21, 2014

Filed:

Mar. 08, 2013
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Martin Recksiek, Hamburg, DE;

Mark Heintjes, Weyhe, DE;

Christoph Winkelmann, Buchholz, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); B64C 13/30 (2006.01); B64C 13/24 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/24 (2013.01); B64C 13/30 (2013.01); B64D 45/0005 (2013.01);
Abstract

A monitoring device is disclosed for an actuation system of an aircraft for monitoring a guiding device of a regulating flap with a load sensor. An actuation system with the monitoring device and a method for reconfiguring such an actuation system are disclosed. The monitoring device includes an interface to the load sensor and an interface to a driving device for adjusting the regulating flap. The monitoring device can determine or receive in-flight information actively signaling a predefined flight attitude and/or a predefined operational state of the aircraft. The monitoring device can compare a load value corresponding to a sensor value acquired by the load sensor and a limiting value corresponding to a minimum operational load for the predefined flight attitude and/or the predefined operational state of the aircraft and a monitoring function. The monitoring function can assign a fault mode to the regulating flap.


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