发明名称 Method and device for calibrating load sensors
摘要 A device and a method for calibrating load sensors which are provided at least one load cross-section of an aerofoil or control surface of an aircraft, the load sensors being calibrated on the basis of load coefficients (αi) of the load sensors, which load coefficients a calculation unit calculates by evaluating a linear system of equations formed by means of mechanical loading of the aerofoil or control surface.
申请公布号 US9250152(B2) 申请公布日期 2016.02.02
申请号 US201213399546 申请日期 2012.02.17
申请人 Airbus Operations GmbH 发明人 Kordt Michael;Reijerkerk Marianne Jacoba
分类号 G01M5/00;G01L1/22;G01L25/00 主分类号 G01M5/00
代理机构 Jenkins, Wilson, Taylor & Hunt, P.A. 代理人 Jenkins, Wilson, Taylor & Hunt, P.A.
主权项 1. A system for calibrating load sensors of an aircraft, comprising: an aerofoil or control surface of the aircraft; load sensors, which are, provided at at least one load cross-section of the aerofoil or control surface of the aircraft, the load sensors being adapted to supply measurement signals to a calculation unit; and the calculation unit being adapted to calibrate the load sensors by load coefficients (αi) of the load sensors, which load coefficients are calculable, by the calculation unit, by evaluating a linear system of equations formed by mechanical loading of the aerofoil or control surface; wherein the calculation unit is adapted to calibrate the load sensors during a loading measurement, in which the aerofoil or control surface is loaded continuously with a preset transverse load profile which is caused in each case by a corresponding flight maneuver of the aircraft located in the air.
地址 Hamburg DE