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    • 3. 发明专利
    • EXCITING DEVICE FOR CABLE
    • JPS5821536A
    • 1983-02-08
    • JP12014681
    • 1981-07-31
    • NIPPON KOKAN KK
    • FUJISAWA NOBUMITSUMURATA MAMORU
    • G01M7/02G01L5/04
    • PURPOSE:To easily excite a cable by a normal mode and to perfrom a high- precise measurement of a natural frequency, by a method wherein an exciting frequency and an exciting force are caused to change continuously, and a cushioning spring is located between a connection cable and a slide metal. CONSTITUTION:A variable speed motor 6 is secured to a base bed 6 to turn a fly wheel consisting of a crank metal 7. A crank pin 8 is situated so that an eccentric distance from the crank metal 7 can be adjusted, and is moved by a crank pin moving device 10. With the crank metal 7 turned, a slide metal 16 is guided by a guide member 18 attached to the base bed 5, and reciprocates in a direction of radius. A displacement gauge 19 outputs the reciprocating displacement distance of the slide metal, and a pulse meter 20 outputs the number of revoutions or the number of exciting frequencies of the motor 6. A connection wires 25, stretched between the other end of the slide metal 16 and a cable 3 to be excited, is provided with a cushioning spring 26 in the middle of the wire, and the wire 25 is connected to the cable 3 through a sleeve 27 for connecting the wire.
    • 5. 发明专利
    • AIR TUNNEL TESTER
    • JPS6366434A
    • 1988-03-25
    • JP21078886
    • 1986-09-09
    • NIPPON KOKAN KK
    • FUJISAWA NOBUMITSUKITAGAWA KIICHISONOBE YOSHIHIROKATO SHINJI
    • G01M7/02G01M7/00G01M9/00G01M9/08
    • PURPOSE:To enhance the ratio between torsion and flexure frequencies without an increase in the polar inertial moment, by applying a spring constant of a coil spring for flexure and a spring constant of a coil spring for torsion independently. CONSTITUTION:Coil springs 11 and 11a for vertical flexure and coil springs 12-12c for horizontal torsion are arranged independently and when wind 8 is provided from the direction of the arrow, this apparatus vibrates, where flexure frequency is determined by the springs 11 and 11a, and the torsion frequency by the springs 12-12c and the interval (b) therebetween. When a model 5 vibrates in vertical flexure, the springs 11 and 11a extend or reduce but the springs 12-12c little do and hence the flexure frequency can be determined by the springs 11 and 11a only. Likewise, when the model 5 vibrates in torsion, the springs 11 and 11a will not extend or reduce and hence the torsion frequency can be determined by the springs 12-12c only. A larger ratio between torsion and flexure frequencies can be obtained simply by increasing the strength of the springs 12-12c. Thus, an increase in the torsion frequency (f) in noway contributes to a larger polar inertial moment.
    • 6. 发明专利
    • DAMPING METHOD FOR AERODYNAMIC VIBRATION OF STRUCTURE
    • JPH04198507A
    • 1992-07-17
    • JP32607090
    • 1990-11-29
    • NIPPON KOKAN KK
    • FUJISAWA NOBUMITSUSONOBE YOSHIHIRO
    • E01D1/00E01D2/04E01D11/02E01D11/04
    • PURPOSE:To suppress aerodynamic vibration of the main girder by a method in which a plurality of nozzles are set at given intervals in the longitudinal direction of the main girder on the corners of the box-like main girder of bridge and air is jetted from the nozzles to the opposite directions (longitudinal direction, widthwise direction, or vertical direction of main girder). CONSTITUTION:Nozzles 20 are set at a given interval in the longitudinal direction (X-direction) on the corners of a main girder 2, and ports 20a and 20b through which air is jet to opposite directions are provided to the nozzles 20. When the main girder 2 receives wind 6 in the sideward direction (Y-direction), the nozzles 20 operate to form air stream 21, where swirl produced on the girder 2 is disturbed to vary the flow and rate of the swirl. The air stream 21 is formed intermittently in the longitudinal direction (X-direction), and nonsteady air force by swirl on the girder 2 is also varied to suppress the vibration in the Z-direction of the main grider 2. Since the downflow rate of swirl is also varied, the resonance of nonsteady air force and vibration can be prevented. Aerodynamic vibration of the main girder can thus be suppressed.
    • 7. 发明专利
    • BRIDGE EQUIPPED WITH PREVENTIVE MEASURES FOR AERODYNAMIC VIBRATION
    • JPH02232404A
    • 1990-09-14
    • JP5008189
    • 1989-03-03
    • NIPPON KOKAN KK
    • FUJISAWA NOBUMITSUTAKEDA KATSUAKIWADA HIROHISA
    • E01D1/00E01D2/04E01D11/02E01D11/04
    • PURPOSE:To contrive to reduce amplitude of vortex excitation by providing gratings over the deck surface between each of both end parts of a main girder of a bridge and each of side stringers provided on both ends of the bridge, and by further providing guide plates on the underside of the bridge at each of positions a little closer to the center of the bridge. CONSTITUTION:Gratings 20 are formed over a deck 3 at positions near side stringers 5 installed at the opposite sides of a bridge 1, and at the side ends of the deck, a little closer to the center of the bridge 1, guide plates 21 are provided facing downwardly aslant, with their lower ends made lower than the lower ends of the side stringers 5. The bridge is made in such structure that lateral wind blowing to the bridge runs from the underside through the gratings 20 to the surface of the deck 3 being guided by the guide plates 21. Air flow 22 is then made to form a second boundary layer 23 along the surface of the deck 3. Then the second boundary layer, interacting with a strong boundary layer 7, decreases negative pressure applying to the deck surface and restrains generation of vortex excitation, dislocating the phase. Thereby amplitude of the vortex excitation can be reduced and the vortex produced at the surface of the deck 3 becomes smaller.
    • 8. 发明专利
    • HORIZONTAL PENDULUM TYPE DYNAMIC VIBRATION REDUCER
    • JPS62209244A
    • 1987-09-14
    • JP4157986
    • 1986-02-28
    • NIPPON KOKAN KK
    • TSUJI MATSUOFUJISAWA NOBUMITSUTSUMURA NAONOBUHORIUCHI HIROSHIKANO ISAMU
    • F16F15/02F16F7/10
    • PURPOSE:To exhibit the suppressing effect of vibration by changing the value of a weight even in accordance with a variation in weight, by providing an arm and weight to a shaft which may be inclined to a vertical plane and to rotated, and by providing a damper between the arm and a stationary point. CONSTITUTION:A structure 1 to be subjected to suppression of vibration and a pendulum rotary shaft 10 are arranged, making an inclined angle therebetween, and a viscous damper 20 is arranged between pendulum arms 11, 11a suspending a weight 13 and an upper arm 3 as another stationary point. When the structure 1 is subjected to forced oscillation due to, for example, Karman vortices, this vibration is turned into the vibration of the pendulum of dynamic vibration reducer which is damped by the damper 20 as possible as it can. Further, when the natural frequency of the structure 1 varies, the natural frequency of the pendulum also varies if the inclined angle of the pendulum shaft 10 or the position of the weight 10 on the arms 11, 11a, so that it widely cope with various kind of vibration, and further, if the value W of the weight 1 is changed, this arrangement may cope with variations in the mass of the structure 1.