Airborne flight planning and information system
    31.
    发明授权
    Airborne flight planning and information system 失效
    机载飞行计划和信息系统

    公开(公告)号:US4642775A

    公开(公告)日:1987-02-10

    申请号:US737665

    申请日:1985-05-24

    CPC classification number: G01C23/00 G01C21/00

    Abstract: A flight planning system for obtaining flight plans and/or weather information is provided with a portable computer having a display unit, keyboard, memory, built in modem and a built in disk drive that can be connected via telephone lines to a ground based data center. The basic flight planning data and/or weather request data is input in response to menu driven prompts and reviewed on the display by the pilot. The portable computer is then connected to the data center which generates a series of optimized flight plans and provides desired weather information. After the desired flight plan and/or weather information has been selected by the pilot, it is loaded onto a floppy disk in the disk drive. The aircraft is provided with a data transfer unit which accepts the floppy disk and downloads the flight plan and requested weather information into the onboard computerized navigation system. In addition the aircraft is provided with a VHF radio system for inflight communication with the data center so that the flight plan and/or weather information can be updated.

    Abstract translation: 提供了一种用于获得飞行计划和/或天气信息的飞行计划系统,该便携式计算机具有显示单元,键盘,存储器,内置调制解调器和内置磁盘驱动器,可通过电话线连接到基于地面的数据中心 。 基于菜单驱动的提示输入基本的飞行计划数据和/或天气请求数据,并由飞行员在显示器上进行审查。 然后将便携式计算机连接到数据中心,该数据中心产生一系列优化的飞行计划并提供所需的天气信息。 在飞行员选择所需的飞行计划和/或天气信息之后,将其加载到磁盘驱动器中的软盘上。 该飞机设有数据传输单元,接收软盘并下载飞行计划并将天气信息请求到车载计算机化导航系统中。 此外,该飞机还配备有用于与数据中心进行飞行通信的VHF无线电系统,以便可以更新飞行计划和/或天气信息。

    Angular rate sensor utilizing two vibrating accelerometers secured to a
parallelogram linkage
    32.
    发明授权
    Angular rate sensor utilizing two vibrating accelerometers secured to a parallelogram linkage 失效
    角速率传感器利用两个固定在平行四边形连杆上的振动加速度计

    公开(公告)号:US4510802A

    公开(公告)日:1985-04-16

    申请号:US528774

    申请日:1983-09-02

    Applicant: Rex B. Peters

    Inventor: Rex B. Peters

    CPC classification number: G01P15/14 G01C19/5776

    Abstract: In an inertial system for sensing the angular rotation and translational motion of a structure utilizing a pair of accelerometers in a back-to-back arrangement vibrating substantially linearly along an axis normal to their force sensing axes, a mechanism utilizing a parallelogram structure is used to impart the vibratory motion to the accelerometers.

    Abstract translation: 在用于感测利用一对加速度计的结构的角度旋转和平移运动的惯性系统中,所述结构沿着垂直于其力感测轴线的轴线大致线性振动地进行背对背布置,利用平行四边形结构的机构被用于 将振动运动传递给加速度计。

    Static low tire pressure detection system for aircraft
    33.
    发明授权
    Static low tire pressure detection system for aircraft 失效
    飞机静态低轮胎压力检测系统

    公开(公告)号:US4506328A

    公开(公告)日:1985-03-19

    申请号:US403454

    申请日:1982-07-30

    CPC classification number: G01G19/07

    Abstract: A static low tire pressure detection system for detecting the presence of a low tire mounted on a structural member of an aircraft, such as a bogie beam or nose axle, includes a pair of inclinometers mounted on the structural member and adapted to sense the bend therein. The signals from the inclinometers are stored in a memory once the aircraft is at rest on the ground to provide reference signals indicating the angle of the structural member with respect to an inertial reference and the weight carried thereby. The reference signals are compared against later-developed signals representing instantaneous angle and weight on the structural member to develop difference signals. The difference signals are used to generate an indication of tire pressurization, which is then checked to determine whether the tire pressurization is within acceptable limits. If the tire pressure is outside of the acceptable limits, then an indicating device is energized to provide a warning of a potentially dangerous condition to the aircraft operating personnel.

    Abstract translation: 用于检测安装在诸如转向架梁或前桥的飞机的结构构件上的低轮胎的存在的静态低轮胎压力检测系统包括安装在结构构件上并适于感测其中的弯曲的一对倾斜计 。 飞机在地面静止时,来自倾斜计的信号被存储在存储器中,以提供指示结构构件相对于惯性参考的角度的参考信号和由此承载的重量。 将参考信号与表示结构构件上的瞬时角度和重量的稍后开发的信号进行比较以产生差分信号。 差分信号用于产生轮胎加压的指示,然后检查轮胎加压的指示以确定轮胎加压是否在可接受的限度内。 如果轮胎压力超出可接受的限度,则指示装置被通电以向飞行操作人员提供潜在危险状况的警告。

    Transducer alignment method for weight and balance system
    34.
    发明授权
    Transducer alignment method for weight and balance system 失效
    用于重量和平衡系统的传感器校准方法

    公开(公告)号:US4480912A

    公开(公告)日:1984-11-06

    申请号:US351960

    申请日:1982-02-24

    CPC classification number: G01B11/26

    Abstract: A method of determining the alignment of a first transducer mounting surface relative to a second transducer mounting surface includes utilizing a laser in conjunction with first and second precision ground fixtures secured to the first and second transducer mounting surfaces, respectively. An optically flat mirror is carried by each of the fixtures, with the mirror of the first fixture being partially light-transmissive. The incident light beam from the laser is directed at the partially light-transmissive mirror which, in turn, reflects part of the incident beam to form a first reflected beam. The remaining portion of the incident beam is transmitted and is reflected by the other mirror to form a second reflected beam. The two beams reflected by the mirrors are projected upon a screen disposed in front of the laser, such screen having an aperture through which the incident beam passes. The position of the laser and screen is adjusted so that the reflected beam from one of the mirrors falls at a predetermined location on the screen. The horizontal and vertical distances on the screen of the reflected beams from the incident beam are measured and are used in an equation to determine the angular alignment of the transducer mounting surfaces relative to one another.

    Abstract translation: 确定第一换能器安装表面相对于第二换能器安装表面的对准的方法包括分别与固定到第一和第二换能器安装表面的第一和第二精密接地固定装置相结合地使用激光。 光学平面镜由每个固定装置承载,第一固定装置的反射镜是部分透光的。 来自激光器的入射光束被引导到部分透光镜,其又反射入射光束的一部分以形成第一反射光束。 入射光束的剩余部分被透射并被另一个反射镜反射以形成第二反射光束。 由反射镜反射的两个光束被投影在设置在激光器前面的屏幕上,这样的屏幕具有入射光束通过的孔。 调整激光和屏幕的位置,使得来自其中一个反射镜的反射光束落在屏幕上的预定位置。 测量来自入射光束的反射光束的屏幕上的水平和垂直距离,并在等式中使用以确定换能器安装表面相对于彼此的角度对准。

    Flexure with electrical conductor
    35.
    发明授权
    Flexure with electrical conductor 失效
    电导线弯曲

    公开(公告)号:US4441366A

    公开(公告)日:1984-04-10

    申请号:US283341

    申请日:1981-07-14

    Abstract: A flexure in a transducer such as an inertial guidance accelerometer for suspending a force sensitive element to a mounting base includes a reduced thickness central portion and a pair of relatively thick ribs disposed on opposite sides of the central portion. An electrically conductive coating is disposed on at least one face of the central portion to provide electrical connections to components located on the element. The reduced thickness of the central portion minimizes errors caused by stresses in the interface between the conductive coating and the element and the relatively thick ribs provide a desired strength and spring rate for the element suspension.

    Abstract translation: 用于将力敏元件悬挂在安装基座上的诸如惯性引导加速度计的换能器中的弯曲部包括设置在中心部分的相对侧上的减小厚度的中心部分和一对较厚的肋条。 导电涂层设置在中心部分的至少一个面上,以提供到位于元件上的部件的电连接。 中心部分的减小的厚度最小化由导电涂层和元件之间的界面中的应力引起的误差,并且相对较厚的肋为元件悬浮液提供期望的强度和弹簧刚度。

    Equalization preamplifier with high frequency gain peaking
    36.
    发明授权
    Equalization preamplifier with high frequency gain peaking 失效
    均衡前置放大器具有高频增益峰值

    公开(公告)号:US4433301A

    公开(公告)日:1984-02-21

    申请号:US262372

    申请日:1981-05-11

    Applicant: Henry J. Lukes

    Inventor: Henry J. Lukes

    CPC classification number: H03F1/083 H03G5/025

    Abstract: Gain peaking and attenuation of audio signals above the peak gain frequency are provided in an audio frequency equalization preamplifier that includes an operational amplifier having a feedback network including first and second resistors and a feedback capacitor connected between the output and the second feedback resistor. Two or three low pass RC filter sections are connected between the audio signal source and the noninverting input of the operational amplifier with a circuit connecting a capacitor of the second RC section from the noninverting input to a node between the second feedback resistor and the feedback capacitor.

    Abstract translation: 在音频均衡前置放大器中提供了高于峰值增益频率的音频信号的增益峰值和衰减,该音频均衡前置放大器包括具有包括第一和第二电阻器的反馈网络的运算放大器以及连接在输出端和第二反馈电阻器之间的反馈电容器。 两个或三个低通RC滤波器部分连接在运算放大器的音频信号源和非反相输入端之间,其中电路将第二RC部分的电容器从非反相输入端连接到第二反馈电阻器和反馈电容器之间的节点 。

    Borehole survey apparatus utilizing accelerometers and probe joint
measurements
    37.
    发明授权
    Borehole survey apparatus utilizing accelerometers and probe joint measurements 失效
    利用加速度计和探头接头测量的钻孔测量装置

    公开(公告)号:US4399692A

    公开(公告)日:1983-08-23

    申请号:US224789

    申请日:1981-01-13

    CPC classification number: E21B47/022

    Abstract: To provide for accurate determination of azimuth in a borehole survey apparatus, a downhole probe is provided with two or more sections connected by torsionally rigid, flexible joint assemblies with provisions for generating signals that represent the relative inclination and azimuth of one probe section from another. These signals are combined with inclination signals obtained from a set of accelerometers in one of the probe sections in a signal processing unit to generate signals that represent the direction and depth of the borehole.

    Abstract translation: 为了准确地确定钻孔测量装置中的方位角,井下探针设置有两个或多个通过扭转刚性的柔性接头组件连接的部分,其具有用于产生表示一个探针部分相对于另一探针部分的相对倾斜度和方位角的信号。 这些信号与在信号处理单元中的一个探测部分中的一个加速度计获得的倾斜信号组合,以产生表示井眼的方向和深度的信号。

    Weight, balance, and tire pressure detection systems
    38.
    发明授权
    Weight, balance, and tire pressure detection systems 失效
    重量,平衡和轮胎压力检测系统

    公开(公告)号:US4312042A

    公开(公告)日:1982-01-19

    申请号:US102776

    申请日:1979-12-12

    Abstract: A weight and balance system for an aircraft or the like which measures the bend in a structural member of the aircraft, such as a landing gear element or a wing or fuselage section, by use of inclinometers mounted to the member and each having a signal output representing the angle of the member with respect to a reference plane and then summing signal outputs from the incinometers to determine the angle of the bend which provides an indication of weight. In one example, the landing gear of the aircraft includes a member which bends in response to aircraft weight and a pair of inclinometers, in the form of servoed accelerometers, are mounted to the member adjacent opposite ends thereof and each provide a voltage output representing the angle of the member relative to the reference plane, and a summing device for summing said signal outputs as an indication of weight. For tire pressure detection, a plurality of inclinometers are associated with a bogie beam to determine which one of two or more pairs of tires is underpressured.

    Abstract translation: 用于飞行器等的重量和平衡系统,其通过使用安装到构件的倾斜计测量飞行器的结构构件(例如起落架元件或机翼或机身部分)中的弯曲,并且每个具有信号输出 表示构件相对于参考平面的角度,然后将来自入射计的信号输出相加以确定提供重量指示的弯曲角度。 在一个示例中,飞机的起落架包括响应于飞机重量而弯曲的构件,并且以伺服加速度计的形式的一对倾斜计被安装到邻近其相对端的构件,并且每个提供表示 所述构件相对于所述参考平面的角度以及用于将所述信号输出相加的求和装置作为重量的指示。 对于轮胎压力检测,多个倾斜计与转向架梁相关联,以确定两对或更多对轮胎中的哪一对受到不利影响。

    Capacitive pick-off circuit
    39.
    发明授权
    Capacitive pick-off circuit 失效
    电容式开关电路

    公开(公告)号:US4167697A

    公开(公告)日:1979-09-11

    申请号:US876602

    申请日:1978-02-10

    Inventor: Joseph P. Gerber

    CPC classification number: G01R27/2605

    Abstract: An improved capacitive pick-off circuit is provided by utilizing an operational amplifier wherein a pick-off capacitor to be measured forms a part of a feedback circuit of the operational amplifier resulting in the gain of the operational amplifier becoming inversely proportional to the capacitance or directly proportional to the gap between the plates of the capacitor thereby providing a measure of capacitance. A differential capacitive pick-off circuit is implemented by using a pair of operational amplifiers wherein feedback circuits controlling the gain of the operational amplifiers include pick-off capacitors to be measured and a third differential amplifier is connected to the outputs of the two operational amplifiers to provide a signal representing the difference in capacitance between the two pick-off capacitors.

    Abstract translation: 通过使用运算放大器来提供改进的电容式拾取电路,其中待测量的取样电容器形成运算放大器的反馈电路的一部分,导致运算放大器的增益与电容成反比或直接 与电容器的板之间的间隙成比例,从而提供电容的量度。 通过使用一对运算放大器来实现差分电容性拾取电路,其中控制运算放大器的增益的反馈电路包括要测量的拾取电容器,并且第三差分放大器连接到两个运算放大器的输出端 提供表示两个拾取电容器之间的电容差的信号。

    Oil mist lubricator for metal tape
    40.
    发明授权
    Oil mist lubricator for metal tape 失效
    金属胶带油雾润滑器

    公开(公告)号:US4018303A

    公开(公告)日:1977-04-19

    申请号:US544487

    申请日:1975-01-27

    CPC classification number: F16N7/32 G11B5/725 G11B5/84

    Abstract: In a recording tape lubricating apparatus, a tape is passed through a plenum chamber having a baffling hood therein which substantially encircles a portion of the length of said tape as a mist of oil is directed toward the underside of said tape under said hood. A film of oil is deposited on the underside of said tape with the surplus mist, in part, condensing on the inside of the hood and dropping to the floor of the plenum chamber where both the condensed oil and the balance of the surplus mist is evacuated to prevent escape into the surrounding facilities.

    Abstract translation: 在记录带润滑装置中,带子通过其中具有挡板罩的充气室,其基本上环绕所述带的长度的一部分,因为油雾指向所述罩下面的所述带的下侧。 油墨膜沉积在所述带的下侧,多余的雾部分地冷凝在罩的内侧,并且下落到集气室的地板上,其中冷凝油和剩余雾的余量均被抽真空 以防止逃到周围的设施。

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