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    • 1. 发明授权
    • Angle sensing device and angle sensing system
    • 角度检测装置和角度检测系统
    • US07957930B2
    • 2011-06-07
    • US12334458
    • 2008-12-13
    • Ruh-Hua Wu
    • Ruh-Hua Wu
    • G01C1/00G01C19/18
    • B62D15/021B62D15/0245
    • An angle sensing system for sensing a rotating angle of a steering wheel includes a sensing unit, a processing unit, and a storage unit. The sensing unit detects the rotating angle of a steering column connected to the steering wheel and outputting a sensing signal based on the rotating angle. When the steering column rotates for a circle, the sensing signal presents a non-continuous status. The processing unit calculates the relative angle in a single loop of the steering column based on the sensing signal and the number of loops according to the number of the non-continuous status. The storage unit stores the information of the relative angle and the number of loops. Based on the number of loops and the relative angle, the rotating angle of the steering wheel is detected.
    • 用于感测方向盘的旋转角度的角度感测系统包括感测单元,处理单元和存储单元。 感测单元检测连接到方向盘的转向柱的旋转角度并基于旋转角输出感测信号。 当转向柱旋转一圈时,感测信号呈现非连续状态。 处理单元基于感测信号和根据非连续状态的数量的循环数来计算转向柱的单个回路中的相对角度。 存储单元存储相对角度和循环次数的信息。 根据回路的数量和相对角度,检测方向盘的旋转角度。
    • 2. 发明授权
    • Rotor
    • 转子
    • US6127762A
    • 2000-10-03
    • US142735
    • 1998-09-15
    • Moananui Michael Kenneth Pedlar
    • Moananui Michael Kenneth Pedlar
    • A63H1/00F01D25/00G01C19/02G01C19/06G01C19/18H02K1/22A63H1/08H02K15/02
    • G01C19/06Y10T29/49012Y10T74/12Y10T74/1282
    • A rotor (1) is of a substantially spherical shape with one complete half of the sphere (2) still remaining. The rotor (1) effective takes the shape of the head of a "mushroom." The other half of the sphere has had its material removed or omitted forming the stem (3). The depth of the cut "D" and the length "L," the radius of the sphere, will determine the ratio of the respective weights of the complete half sphere (2) and the stem portion (3). Suitably the weight of the one half to the other half of the spherical body is between about 0.75 and 0.85 and more preferably 0.8. When an external force is applied to the rotor (1), it rotates simultaneously about a pair of orthogonal axes one of which is defined by the edge (6) of the spherical body between the two halves.
    • PCT No.PCT / NZ97 / 00012 Sec。 371日期:1998年9月15日 102(e)日期1998年9月15日PCT提交1997年2月3日PCT公布。 公开号WO97 / 36093 日期1997年10月2日转子(1)具有基本上球形的形状,球体(2)的一半完全仍然存在。 转子(1)有效采取“蘑菇”头部的形状。 球体的另一半已经将其材料去除或省略,从而形成杆(3)。 切割深度“D”和长度“L”是球体的半径,将决定完整的半球体(2)和杆部分(3)的各个重量的比例。 适当地,球体的一半到另一半的重量在约0.75和0.85之间,更优选地为0.8。 当向转子(1)施加外力时,它同时围绕一对正交轴旋转,其中一个正交轴由两个半部之间的球体的边缘(6)限定。
    • 4. 发明授权
    • Multi-sensor pickoff assembly
    • 多传感器检测装置
    • US4621529A
    • 1986-11-11
    • US745055
    • 1985-06-17
    • Roland Pittman
    • Roland Pittman
    • G01C19/18G01C19/28G01C19/42G01P9/02
    • G01C19/28Y10T74/1293
    • A navigation sensor, including a gyroscopic element, which has a spin axis, and which has flexure hinge for resiliently mounting the element on a base, and a torque sensing assembly, which has a first piezoelectric beam that is mounted in coaxial relation to the spin axis, and which has a first beam restraining member that mounts a first edge portion of the first piezoelectric beam, and which has a second beam restraining member that mounts an opposite edge portion of the first piezoelectric beam. The first piezoelectric beam is adapted to generate an electrical signal proportional to the angular velocity of the navigation sensor about an axis perpendicular to the spin axis.
    • 一种导航传感器,包括具有旋转轴线的陀螺仪元件,并且具有用于将元件弹性地安装在基座上的挠曲铰链,以及扭矩传感组件,其具有与旋转同轴的方式安装的第一压电梁 并且其具有安装所述第一压电梁的第一边缘部分并且具有安装所述第一压电梁的相对边缘部分的第二束限制构件的第一束限制构件。 第一压电波束适于产生与导航传感器围绕垂直于旋转轴线的轴线的角速度成比例的电信号。
    • 5. 发明授权
    • Rate gyroscope having an optical sensor system
    • 具有光学传感器系统的陀螺仪
    • US4339959A
    • 1982-07-20
    • US81503
    • 1979-10-03
    • Benjamin Klaus, Jr.Gordon C. MacKenzie
    • Benjamin Klaus, Jr.Gordon C. MacKenzie
    • G01C19/18G01C19/28G01C19/42
    • G01C19/28G01C19/18G01C19/42Y10T74/1264
    • A rate gyroscope having a spinning mass flexibly coupled to a rotor through a pair of orthogonally disposed, diametrically extending suspension arms. The spinning mass is adapted to pivot about the arms in response to a pair of orthogonal angular rates being measured by the gyroscope. The angular orientation of the mass with respect to the gyroscope housing provides an indication of the angular rates. An optical sensor system disposed within the housing of the gyroscope and supporting electronics are used to produce an electrical signal representative of the angular orientation of the mass and, hence, such signal provides a measurement of a pair of angular rates being measured by the gyroscope. Such sensor system includes a tilted mirror attached to an axial end of the spinning mass which reflects collimated light rays from a light emitting diode, through a reticle, to a silicon diode detector. The light passing through the reticle is modulated in accordance with the angular orientation of the spinning mass, and hence, in accordance with the angular rates being measured. The signal data is converted into an electrical signal, which after amplification and processing provides a measurement of the angular rates, such as pitch and yaw.
    • 具有旋转质量的速率陀螺仪通过一对正交设置的径向延伸的悬挂臂柔性地联接到转子。 旋转体适于响应由陀螺仪测量的一对正交角速度而围绕臂枢转。 质量相对于陀螺仪外壳的角度取向提供角速率的指示。 设置在陀螺仪和支撑电子装置的壳体内的光学传感器系统用于产生表示质量的角度定向的电信号,因此,这种信号提供由陀螺仪测量的一对角速度的测量。 这种传感器系统包括一个倾斜的反射镜,该反射镜附着在旋转质量体的轴向端部,将来自发光二极管的准直光线通过掩模版反射到硅二极管检测器。 根据旋转质量的角度取向调制通过标线的光,因此根据所测量的角速度来调制。 信号数据被转换成电信号,其在放大和处理之后提供角速率的测量,例如俯仰和偏航。
    • 6. 发明授权
    • Flexure-pivot assemblies and methods of making them
    • US4122689A
    • 1978-10-31
    • US702827
    • 1976-07-06
    • Geoffrey Beardmore
    • Geoffrey Beardmore
    • F16C11/12F16D3/50F16F1/14F16F1/18G01C19/16G01C19/18B23P11/00
    • G01C19/16F16C11/12F16F1/14Y10T74/1293
    • A flexure-pivot for providing resilient restraint that opposes relative angular displacement between two members involves two flat springs, that are held at one end between pairs of pins carried by one member and at the other end between pairs of pins carried by the other member, the flat springs each having two parallel rib portions that are linked at one end and are interlaced with one another. In one form of flexure-pivot the unlinked end of both the rib portions of each spring is secured between a pair of pins carried by one member and the linked end of both the rib portions of each spring is secured between a pair of pins carried by the other member. In another form of flexure-pivot the pairs of pins carried by one member are axially aligned with the pairs of pins carried by the other member, when there is no relative displacement between the members, and the unlinked end of one of the rib portions is secured to one of the pairs of pins carried by one member and the unlinked end of the other one of the rib portions is secured to the axially aligned pair of pins carried by the other member, so that there is a resilient interconnection between the axially aligned pairs of pins. In both forms of flexure-pivot, further pins are mounted with one or other of the members to limit relative angular displacement between the two members by engagement with pairs of pins mounted on an opposite member. Manufacture of both forms of flexure-pivot is initially the same and is carried out by inserting the ends of four pairs of pins in holes in one member, securing each end of the two flat springs between opposite pairs of pins, inserting the other ends of the four pairs of pins in holes in the other member, and brazing the assembly formed to secure the springs to the pins and the pins to the members. One form of flexure-pivot is subsequently formed by cutting two adjacent pairs of pins close to one member and the other two adjacent pairs of pins close to the other member. The other form of flexure-pivot however is formed by cutting through two adjacent pairs of pins at points between the rib portions and cutting through the other two adjacent pairs of pins at one point close to one member and at another point close to the other member.
    • 7. 发明授权
    • Gyroscope flexure hinge suspension
    • GYROSCOPE FLEXURE HINGE暂停
    • US3585866A
    • 1971-06-22
    • US3585866D
    • 1969-07-01
    • SINGER GENERAL PRECISION
    • ENSINGER WILLIS B
    • G01C19/18G01C19/22
    • G01C19/22Y10T74/1293Y10T403/54
    • An improved flexure hinge suspension for use in free-rotor displacement type gyroscopes is provided comprising an inner hinge unit and an outer hinge unit concentrically nested one within the other in a generally parallel manner coaxial with the gyro''s spin or reference axis. Each hinge unit, in turn, comprises a frictionless, four-bar, two-axis, universal-joint suspension element for supporting the gyro''s inertial flywheel relative to the spin axis in a particular directional mode. That is, in the outer hinge unit, the flexure bars have their respective longitudinal axes arranged perpendicular to the spin axis so as to support the flywheel against torsional and radial displacements relative to the spin axis while in the inner hinge unit the flexure bars have their respective longitudinal axes oriented parallel to the spin axis so as to support the flywheel against axial displacements along the spin axis. In each hinge unit the flexure bars comprise locally thin necked-down sections formed by machining a corresponding pair of closely spaced holes completely through the peripheral wall of each unit as the case may be. Thus, when the two units are positioned relative to each other before being rigidly fastened together, the desired exact orthogonal alignment between the flexure bars in the outer unit and the corresponding flexure bars in the inner unit may be facilitated by a simple visual inspection thereof. The flexure hinge assembly furthermore includes angle stop means for safely limiting the angular displacement of its hinge gimbals thereby preventing the delicate thin flexure bars from being overstressed or ruptured in operation.