作者: Simon John Parker
DOI:
关键词: Engineering 、 Rotation 、 Pinion 、 Drive shaft 、 Signal 、 Leading-edge slats 、 Rotary actuator 、 Controller (computing) 、 Control theory 、 Leading edge
摘要: A system and method for determining whether the relative rate of deployment all slats extending from a leading edge an aircraft wing is same as predetermined deployment. Each slat includes at least one mechanism that drive pinion drivingly coupled to each rotary actuator having output shaft driven by common input shaft. The invention comprises sensor associated with generate signal indicative rotation corresponding supply controller. controller configured analyze signals supplied sensors alarm if any shafts differs rotation.