发明名称 FLAP ADJUSTING SYSTEM OF AN AIRCRAFT WITH A REGULATING FLAP
摘要 Embodiments pertain to a flap adjusting system including a regulating flap mounted on an airfoil using at least two bearing devices and movable relative to the airfoil, and an adjusting device. The adjusting device includes an actuator and adjusting kinematics with a drive rod that couples the actuator to the regulating flap using a first and a second joint, as well as a load sensor. The adjusting kinematics are configured such that, at a maximum adjustment travel of the regulating flap, the second joint between the drive rod and the regulating flap is adjusted by an angle less than 50% of the angle by which the first joint is adjusted. The load sensor is arranged in at least one adjusting device and in the second joint, which couples the drive rod to the regulating flap. The load sensor is configured to measure the forces in this load path.
申请公布号 EP2499044(A2) 申请公布日期 2012.09.19
申请号 EP20100779716 申请日期 2010.11.15
申请人 AIRBUS OPERATIONS GMBH 发明人 RECKSIEK, MARTIN;GREIF, STEFAN;SCHWINN, ROBERT
分类号 B64C9/16 主分类号 B64C9/16
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