发明名称 METHOD FOR DETERMINING STATE OF COMPONENT OF AIRCRAFT ELEVATION FORCE SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a method for determining a state of a component of an aircraft elevation force system.SOLUTION: A method comprises: a step for, expanding at least one elevation force plane to a first development position, in which the elevation force plane is coupled to two drive struts, out of the two drive struts, at least one drive strut is a load detection drive strut; a step for acquiring a first load 32 which is detected by the load detection drive strut related to the at least one elevation force plane in a first flight state having first speed; a step for comparing the first load with a known constant load 28 for the first development position and the first flight state, in consideration of a predetermined threshold 30; and a step for generating an alarm signal, when the acquired load is different from the constant load 28 including the predetermined threshold 30.SELECTED DRAWING: Figure 2a
申请公布号 JP2016135668(A) 申请公布日期 2016.07.28
申请号 JP20150247618 申请日期 2015.12.18
申请人 AIRBUS OPERATION GMBH 发明人 JAN-AREND VAN BRUGGEN;EUGEN NEB;MICHAEL BRADY;WOLFGANG HARTWIG;OLIVIER CRIOU;STEPHAN LATZEL;MARK HEINTJES
分类号 B64C13/00 主分类号 B64C13/00
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