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Hydrofoil cavitation sensing and control apparatus

机译:水翼空化传感与控制装置

摘要

A cavitation detection and control system for controlling the movement of a hydrofoil within a safe, cavitation-free, acceleration and speed region. The system utilizes transducers, associated with the hydrofoil propulsion apparatus and associated with the foil/strut apparatus, for sensing the onset and duration of cavitation in the liquid working medium adjacent to or within these apparatus and a receiver for converting the sensed cavitation data into a signal. An alarm device is responsive to that signal so that the helmsman can reduce the thrust for operating the hydrofoil movement within a cavitation-free region. A data storing device is connected to the receivers output for retaining occurrence of the onset and duration of cavitation.
机译:一种气蚀检测和控制系统,用于控制水翼在安全,无气蚀,加速和速度区域内的运动。该系统利用与水翼推进装置相关联且与箔/支柱装置相关联的换能器,以感测在这些装置附近或内部的液体工作介质中空化的开始和持续时间,以及用于将感测到的空化数据转换为水汽的接收器。信号。警报装置响应该信号,从而舵手可以减小用于在无气蚀区域内进行水翼运动的推力。数据存储设备连接到接收器输出,以保持空化的发生和持续时间。

著录项

  • 公开/公告号US3910216A

    专利类型

  • 公开/公告日1975-10-07

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US19740478117

  • 发明设计人 SHULTZ;WILLIAM M.;

    申请日1974-06-10

  • 分类号H04B11/00;

  • 国家 US

  • 入库时间 2022-08-23 03:26:06

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