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 |