发明名称 Method and device for detecting an uncontrolled movement of an aircraft control surface
摘要 A detection device determines whether an uncontrolled movement of a control surface of an aircraft is occurring. The device includes means for calculating the difference between a theoretical command and an actual command in order to form a residual value, and means for detecting an uncontrolled movement of the control surface, if a comparison value depending on this residual value is greater than a threshold value If the comparison value is greater than the threshold value during a confirmation time, then the uncontrolled movement of the control surface of the aircraft is confirmed.
申请公布号 US8818573(B2) 申请公布日期 2014.08.26
申请号 US201213552104 申请日期 2012.07.18
申请人 Airbus Operations (SAS);Universite Bordeaux I;Centre National de la Recherche Scientifique 发明人 Goupil Philippe;Dayre Rémy;Le Berre Hervé;Gheorghe Anca;Zolghadri Ali;Cieslak Jérôme
分类号 G01C23/00;B64C13/50;B64D45/00 主分类号 G01C23/00
代理机构 Wood, Herron & Evans, LLP 代理人 Wood, Herron & Evans, LLP
主权项 1. A detection method for an uncontrolled movement of a control surface which is servo-controlled in position by a feedback loop belonging to an electrical flying command system of the aircraft and comprising: the control surface being mobile and the position of which with respect to the aircraft is adjusted by at least one actuator; the actuator that adjusts the position of the control surface as a function of at least one actuating order received as a feedback command; at least one sensor measuring the effective position of the control surface; and at least one calculator developing a control surface command order, that receives the measured effective position and deducts from it an actuating order that is transmitted to the actuator as a feedback command, a method where on an automatic and repetitive way, the following sequence of successive steps is followed: (a) a theoretical feedback current being representative of the feedback command emitted bay the calculator is determined; (b) a parameter being representative of the feedback command is measured with the help of at least one auxiliary sensor at the level of the mechanization of such command into the actuator and an effective feedback current is determined from the measured parameter; (c) the difference between the theoretical feedback current determined at step (a) and the effective feedback current determined at step (b) is calculated so as to form an error signal; and (d) an uncontrolled movement of the control surface is detected if a comparison value depending on the error signal is higher than a threshold value during at least one confirmation time.
地址 Toulouse FR