Method for determining a state of a component in a high lift system of an aircraft
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United States of America Patent
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Jul 11, 2017
Grant Date -
Jun 23, 2016
app pub date -
Dec 21, 2015
filing date -
Dec 22, 2014
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Abstract
A method for determining a state of a component in a high lift system of an aircraft comprises the steps of extending at least one high lift surface, which is coupled with two drive struts, wherein at least one of the two drive struts is a load sensing drive strut, to a first extended position, acquiring a first load sensed by a load sensing drive strut associated with the at least one high lift surface at a first flight state having a first speed, comparing the first load with a known nominal load for the first extended position and the first flight state under consideration of a predetermined threshold, and producing an alarm signal in case the acquired load differs from the nominal load including the predetermined threshold.
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