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Hoist System and Process for Sway Control

机译:升降系统和摇摆控制过程

摘要

An aircraft hoist system includes hoist equipment arranged in an aircraft, the hoist equipment including a motor, a cable, and a hook portion. The aircraft hoist system also includes at least one sensor configured to obtain measurements and a processor configured to analyze the measurements from the at least one sensor. The aircraft hoist system also includes the processor configured to determine motor control signals to control the motor based on an analysis of the measurements from the at least one sensor to reduce sway and/or oscillations of the cable while lifting a load. The aircraft hoist system also includes the processor configured to control the motor to lift the load with the cable based on the determined motor control signals.
机译:飞机葫芦系统包括布置在飞机中的提升设备,提升设备包括电动机,电缆和钩部。飞机升降机系统还包括至少一个传感器,该传感器被配置为获得测量和处理器,该处理器被配置为分析来自所述至少一个传感器的测量值。飞机提升系统还包括处理器,该处理器被配置为基于从至少一个传感器的测量分析来确定电动机控制信号以控制电动机,以减少电缆的摇摆和/或振荡的升降负载。飞机升降机系统还包括处理器,该处理器被配置为控制电动机基于所确定的电动机控制信号控制电动机用电缆提升负载。

著录项

  • 公开/公告号US2021197970A1

    专利类型

  • 公开/公告日2021-07-01

    原文格式PDF

  • 申请/专利权人 BREEZE-EASTERN LLC;

    申请/专利号US202016857947

  • 发明设计人 IAN AZEREDO;PATRICK DOYLE;BRIANNA STEWART;

    申请日2020-04-24

  • 分类号B64D1/22;B64C27/04;B66D1/48;B66C1/40;

  • 国家 US

  • 入库时间 2022-08-24 19:42:52

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