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Supercavitating vehicle control

机译:超空洞车辆控制

摘要

A control system for a supercavitating vehicle includes a set of winglets for rapid maneuverability and a segmented ring wing for fine stabilization control. The winglets and ring wing extend from an aft portion of the vehicle. The winglets are supported by a strut attached to the vehicle. The angle of attack of each winglet into the water adjacent the cavity is controlled by a winglet actuator. The winglet assembly may be extended into the water or retracted to be completely within the cavity by means of a spring-loaded actuated mount. The segmented ring wing is controlled by a ring actuator. The ring actuator may be used to control the angle of attack of the ring wing. Alternately, or in combination, the flow over the ring wing may be neutralized by using the cavitator of the vehicle to globally enlarge the cavity and thus limit the flow.
机译:用于超空载飞行器的控制系统包括一组用于快速操纵的小翼和用于精细稳定控制的分段环形翼。小翼和环形翼从车辆的后部延伸。小翼由连接到车辆的支柱支撑。每个小翼进入空腔附近的水中的迎角由小翼致动器控制。小翼组件可以借助于弹簧加载的致动支架而伸入水中或完全缩回空腔内。分段的环形翼由环形致动器控制。环形致动器可用于控制环形机翼的迎角。替代地或组合地,可以通过使用车辆的空化器使环形翼上的流动中和,以整体上扩大空腔并因此限制流动。

著录项

  • 公开/公告号US7690309B1

    专利类型

  • 公开/公告日2010-04-06

    原文格式PDF

  • 申请/专利权人 ROBERT KUKLINSKI;

    申请/专利号US20080284477

  • 发明设计人 ROBERT KUKLINSKI;

    申请日2008-09-19

  • 分类号F42B15/22;

  • 国家 US

  • 入库时间 2022-08-21 18:48:28

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