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Automatic hull height control system for a hydrofoil vehicle

机译:水翼飞行器的船体高度自动控制系统

摘要

934,094. Automatic control of hydrofoil craft. NORTH AMERICAN AVIATION Inc. Jan. 8, 1962 [Feb. 27, 1961], No. 642/62. Class 38 (4). [Also in Group XXXIII] In an automatic control system for a waterborne vehicle having a hull and hydrofoils a reference signal is generated representing the height at which it is desired that the hull travel above the sea and means are provided for limiting said signal to prevent contact with the sea and broaching of the hydrofoils. As shown, Fig. 6A, an adjustable height reference signal is fed from a generator 30 to a limiter 31 which modifies the amplitude of the reference signal to prevent it exceeding an upper limit or falling below a lower limit. The modified reference signal is compared with the output of an height senser 32 in a summing means 33 to provide a signal indicative of deviation from the desired height. The height senser 32 has a flat response from zero frequency to a frequency representative of the highest wave frequency to which the control system is to be subjected. The deviation signal is fed to a hydrofoil servo actuator 34 to control the attitude of the hydrofoils so as to tend to reduce the deviation to zero. A low-frequency filter 35 prevents high-frequency components of the actual height signal from affecting the response of the servo system; alternatively, the filter can be connected between the summing means 33 and servo 34. The upper and lower reference limits provided by limiter 31 are dependent on the output of a wave height detector 37 which is connected to the wave height senser 32. The elements 31, 37, 32, 35 are arranged so that the limiting is in accordance with Fig. 4 where 2H is the waveheight, trough to crest, and the hatched lines are the upper and lower limits of the hull. The wave-height detection function of detector 37 is accomplished by a high-pass filter having a cut-off frequency approximately equal to the cut-off frequency of the low-pass filter 35. Vertical acceleration is reduced by feeding the servo 34 from an accelerometer 38 through an equalization device 40 which provides a signal to the servo which is a function of both the vertical acceleration and the first integral of vertical acceleration. A signal from an accelerometer switch 41 is fed to the servo 34 and a throttle servo 42 to reduce the vehicle speed and cause the hydrofoil effect to become inoperative under sea state conditions which cause excessive contouring by an automatically controlled vehicle. An integrator 39 is connected in parallel to the output of the summing means 32 and servo 34 to reduce the steady-state height error to a minimum.
机译:934,094。自动控制水翼艇。北美航空公司1962年1月8日[Feb. [1961年1月27日],第642/62号。 38级(4)。 [也属于第XXXIII组]在用于具有船体和水翼的水运车辆的自动控制系统中,产生表示期望船体在海上行驶的高度的参考信号,并且提供了用于限制所述信号以防止与海接触并拉出水翼。如图6A所示,可调节高度的参考信号从发生器30馈送到限幅器31,限幅器31修改参考信号的幅度以防止其超过上限或低于下限。在求和装置33中将修改的参考信号与高度检测器32的输出进行比较,以提供指示与期望高度的偏差的信号。高度感测器32具有从零频率到代表控制系统要经受的最高波频率的频率的平坦响应。偏差信号被馈送到水翼伺服致动器34以控制水翼的姿态,从而趋于将偏差减小到零。低频滤波器35防止实际高度信号的高频分量影响伺服系统的响应。可替代地,滤波器可以连接在求和装置33和伺服器34之间。由限制器31提供的上下参考极限取​​决于连接到波高传感器32的波高检测器37的输出。元件31布置图1、3、37、32、35,以使限制符合图4,其中2H是波高,波峰到波谷,阴影线是船体的上限和下限。检测器37的波高检测功能是通过具有截止频率近似等于低通滤波器35的截止频率的高通滤波器来实现的。加速度计38通过均衡装置40提供信号给伺服器,该信号是垂直加速度和垂直加速度的第一积分的函数。来自加速计开关41的信号被馈送到伺服器34和节气门伺服器42,以降低车速并导致水翼效应在海况下失效,海况导致自动控制的车辆轮廓过大。积分器39与求和装置32和伺服器34的输出并联连接,以将稳态高度误差减小到最小。

著录项

  • 公开/公告号GB934094A

    专利类型

  • 公开/公告日1963-08-14

    原文格式PDF

  • 申请/专利权人 NORTH AMERICAN AVIATION INC.;

    申请/专利号GB19620000642

  • 发明设计人

    申请日1962-01-08

  • 分类号B63B1/28;

  • 国家 GB

  • 入库时间 2022-08-23 16:58:13

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