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    • 81. 发明授权
    • Method and apparatus for measuring flying height of the slider and in-situ monitoring a slider-disk interface
    • 用于测量滑块的飞行高度并原位监测滑块 - 磁盘接口的方法和装置
    • US06404504B2
    • 2002-06-11
    • US09951724
    • 2001-09-14
    • Bo LiuYaolong ZhuTeck Seng Low
    • Bo LiuYaolong ZhuTeck Seng Low
    • G01B1102
    • G01B11/14G01B11/168
    • A method and apparatus for measuring the flying height of a slider above a disk surface and in-situ monitoring the slider disk interface comprising the steps of: providing a beam of light; providing a slider disk interface comprising a disk having a substantially transparent substrate and a thin film layer, a slider for carrying a read/write element, the slider having a reflective surface; and an air bearing having a thickness d3 for supporting the slider above the disk; directing the beam of light to the slider disk interface through the disk, the thin film layer, the air bearing and then to the reflective surface of the slider; and measuring one of the intensity and phase information of the light reflected from the slider disk interface to provide an indication of the thickness d3 of the air bearing and/or of the thin film layer.
    • 一种用于测量滑块在盘表面上方的飞行高度并原位监测滑动盘接口的方法和装置,包括以下步骤:提供光束; 提供一种滑动盘接口,其包括具有基本上透明的基板和薄膜层的盘,用于承载读/写元件的滑块,所述滑块具有反射表面; 以及具有用于在盘上方支撑滑块的厚度d3的空气轴承; 通过盘,薄膜层,空气轴承,然后到滑块的反射表面将光束引导到滑块盘接口; 并且测量从滑动盘接口反射的光的强度和相位信息之一,以提供空气轴承和/或薄膜层的厚度d3的指示。
    • 83. 发明授权
    • Angular displacement measuring device
    • 角位移测量装置
    • US5137353A
    • 1992-08-11
    • US774490
    • 1991-10-10
    • H. Lee B. Seegmiller
    • H. Lee B. Seegmiller
    • G01B11/16G01M9/06
    • G01M9/06G01B11/168
    • A system for measuring the angular displacement of a point of interest on a structure, such as aircraft model within a wind tunnel, includes a source of polarized light located at the point of interest. A remote detector arrangement detects the orientation of the plane of the polarized light received from the source and compares this orientation with the initial orientation to determine the amount or rate of angular displacement of the point of interest. The detector arrangement comprises a rotating polarizing filter and a dual filter and light detector unit. The latter unit comprises an inner aligned filter and photodetector assembly which is disposed relative to the periphery of the polarizer so as to receive polarized light passing the polarizing filter and an outer aligned filter and photodetector assembly which recives the polarized light directly, i.e., without passing through the polarizing filter. The purpose of the unit is to compensate for the effects of dust, fog and the like. A polarization preserving optical fiber conducts polarized light from a remote laser source to the point of interest.
    • 用于测量诸如风洞内的飞行器模型的结构上的兴趣点的角位移的系统包括位于感兴趣点处的偏振光源。 远程检测器装置检测从源接收的偏振光的平面的取向,并将该取向与初始取向进行比较,以确定感兴趣点的角位移量或速率。 检测器装置包括旋转偏振滤光器和双滤光器和光检测器单元。 后一单元包括内部对准的滤光器和光电检测器组件,其相对于偏振器的周边设置,以便接收通过偏振滤光器的偏振光和外部对准的滤光器和光电检测器组件,其直接接收偏振光,即不经过 通过偏振滤光片。 该单元的目的是补偿灰尘,雾等的影响。 偏振保留光纤将来自远程激光源的偏振光传导到感兴趣点。
    • 84. 发明授权
    • Rotating polarizer angle sensing system
    • 旋转偏光片角度感应系统
    • US4688934A
    • 1987-08-25
    • US863654
    • 1986-05-15
    • Larry T. Clark
    • Larry T. Clark
    • G01B11/16
    • G01B11/168
    • A system for measuring aeroelastic deformation of an aircraft wing in flight or in a wind tunnel utilizing light from a linearly polarized light source (101). The light is transmitted through modulating elements (104, 105) to provide a carrier beam, and a small portion of the beam is reflected through a linear polarizer (107) into a photo-detector (108) for utilization as a reference electrical signal (208). The remainder of the beam is reflected back from a retro-reflector target (700) located on the wing into another photo-detector (114) to provide the target electrical signal (209). The two amplified electrical signals are compared in a phase detector (FIG. 3) for providing an angle measurement output signal E.sub.0.
    • 一种用于利用来自线偏振光源(101)的光测量飞行中或在风洞中的飞机机翼的气动弹性变形的系统。 光通过调制元件(104,105)传输以提供载波束,并且光束的一小部分通过线性偏振器(107)反射成光检测器(108)以用作参考电信号( 208)。 光束的剩余部分从位于机翼上的后向反射器靶(700)反射回到另一光电检测器(114)中以提供目标电信号(209)。 两个放大的电信号在相位检测器(图3)中进行比较,以提供角度测量输出信号E0。
    • 85. 发明授权
    • Angular deflection sensing apparatus for load, force, and other types of
measurements
    • 用于负载,力和其他类型测量的角度偏转感测装置
    • US4263810A
    • 1981-04-28
    • US884557
    • 1978-03-08
    • Hong-Yee Chiu
    • Hong-Yee Chiu
    • G01B11/16G01G3/12G01G23/36
    • G01B11/168G01G23/361G01G3/12
    • A method and apparatus of measurement of angular deformation of a body, and in particular, a method and apparatus of load or force sensing are disclosed. Chief applications are found in electronic weighing and related devices. Deformation of a body in the form of angular deflection, or a deformation that can be transformed into angular deflection by mechanical or other means, changes the angle between the polarization axes of a pair of light polarizers, thus changing the intensity of light that is transmitted through the pair of polarizers. A photodetector converts the transmitted light into an electric signal. This signal contains information regarding the amount of deformation of the body and may be used in its analog form to operate a voltmeter to give a visual readout, or converted into a digital form for activating a visual digital display, or for inputing into a digital data processing device. A specially designed feedback-stabilized light source produces an output whose D.C. level stays constant regardless of variations in certain of the properties of the photodetectors and the light source.
    • 公开了一种测量身体的角变形的方法和装置,特别是负载或力感测的方法和装置。 主要应用于电子衡器及相关设备。 以角度偏转的形式的身体变形,或通过机械或其他方式变形成角度偏转的变形,改变一对光偏振器的偏振轴之间的角度,从而改变被传输的光的强度 通过一对偏光器。 光电检测器将透射光转换成电信号。 该信号包含关于身体的变形量的信息,并且可以以其模拟形式用于操作电压表以给出视觉读数,或者转换成用于激活视觉数字显示的数字形式或用于输入数字数据 处理装置。 特别设计的反馈稳定光源产生直流电平保持恒定的输出,而与光电检测器和光源的某些特性的变化无关。