Damping Patents (Class 74/5.5)
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Publication number: 20140245939Abstract: A swinging motion reducing apparatus includes a flywheel 20, a gimbal 11, a gimbal supporting section 12, a damper 13 and a lock mechanism 14. The gimbal 11 rotatably supports the flywheel 20. The gimbal supporting section 12 supports the gimbal 11 through a gimbal shaft 15 such that the gimbal 11 can swing. The damper 13 brakes a swinging motion of the gimbal 11. The lock mechanism 14 locks a swinging motion of the gimbal 11.Type: ApplicationFiled: March 4, 2013Publication date: September 4, 2014Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Tsuyoshi Nohara, Hiroshi Takeuchi, Katsuya Umemura
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Patent number: 8528429Abstract: Systems and methods are provided for stabilizing an emissions instrument. The emissions instrument includes an emissions sensor. The emissions sensor may be coupled to a gyro stabilizer. The gyro stabilizer may stabilize the emissions sensor, thus resulting in a more accurate and reliable emissions instrument.Type: GrantFiled: January 20, 2010Date of Patent: September 10, 2013Assignee: Babcock & Wilcox Power Generation Group, Inc.Inventor: Mark Wayne Holt
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Patent number: 8002251Abstract: A vibration reduction system is provided for use in conjunction with a rotational device including a stationary body, a rotating body, and a first bearing assembly disposed between the stationary body and the rotating body. The vibration reduction system includes a first plurality of bearing mount actuators residing between the stationary body and the first bearing assembly. The first plurality of bearing mount actuators is configured to adjust the radial position of the first bearing assembly. The vibration reduction system further includes a vibration sensor, which is coupled to the stationary body, and a controller, which is coupled to the vibration sensor and to the first plurality of bearing mount actuators. The controller is configured to reduce vibrations sensed by the vibration sensor by selectively adjusting the radial position of the first bearing assembly utilizing the first plurality of bearing mount actuators.Type: GrantFiled: November 14, 2007Date of Patent: August 23, 2011Assignee: Honeywell International Inc.Inventors: Timothy A. Hindle, Toren S. Davis, Brian J. Hamilton, Robert E. Winkel
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Publication number: 20100275705Abstract: A rotor assembly is provided for deployment within a momentum control device including a rotor assembly housing. In one embodiment, the rotor assembly includes a rotor shaft rotatably mounted within the rotor assembly housing, a floating bearing cartridge disposed around a first end portion of the rotor shaft, and a radially-compliant damping member. The radially-compliant damping member is mechanically coupled between the floating bearing cartridge and the rotor assembly housing, as taken along an emitted disturbance path. The radially-compliant damping member reduces the transmission of vibratory forces from the floating bearing cartridge to the rotor assembly housing to reduce emitted disturbances during operation of the momentum control device.Type: ApplicationFiled: April 30, 2009Publication date: November 4, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventor: Theodis Johnson
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Publication number: 20100058882Abstract: Electric Machines (i.e., electric motors or generators) convert electricity to mechanical work (or vice versa) by applying mechanical power to the shaft of the electric machine or extracting mechanical power form the shaft of the electric machine. This restricts the electrical characteristics, such as frequency or voltage, to the movement of the shaft of the electric machine in accordance to electric machine theory. In some cases, it is desired to perform electromechanical conversion from unorthodox movement, such as pulsating movement, slow movement, or low power movement. In many cases this is not possible with even electronic control without a transmission to convert the mechanical power to a compatible motion.Type: ApplicationFiled: August 21, 2009Publication date: March 11, 2010Inventor: Frederick William Klatt
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Patent number: 7464800Abstract: This invention is directed at torsional vibration dampers of a rotating shaft. The dampers of the invention provide self-tuning to dampen harmonics, over a broad range of shaft angular velocities. Where the shaft rotates with an angular velocity about a longintudinal axis, and rotates perpendicular to a plane of rotation, the damper comprises: at least one passive damping element, and one controlling damping element.Type: GrantFiled: March 16, 2004Date of Patent: December 16, 2008Inventor: George Nerubenko
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Patent number: 7159479Abstract: An active damping method for a stabilized mirror, and a corresponding active damper apparatus, comprising providing a tachometer measuring speed of a motor driving the mirror, employing compensation electronics receiving input from said tachometer and the motor, and employing drive electronics providing output to the motor.Type: GrantFiled: September 25, 2003Date of Patent: January 9, 2007Assignee: Lockheed Martin CorporationInventor: John G. Hughes
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Patent number: 6982538Abstract: An apparatus is described which reduces a time delay and a resultant phase shift in a gyroscope motor drive signal. The motor drive signal originates from a numerically controlled oscillator whose output is sampled at a predetermined rate. The apparatus includes a first element which upsamples the oscillator output signal samples and a band pass filter configured to receive an output from the first element and remove spectral components from the output of the first element. The apparatus further includes a third element which generates a tuning parameter, ??o, for tuning of the band pass filter and a scaling multiplier configured to normalize an output of the filter.Type: GrantFiled: September 6, 2002Date of Patent: January 3, 2006Assignee: Honeywell International Inc.Inventor: Stanley A. White
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Patent number: 6789437Abstract: An apparatus and a method for controlling the path of oscillatory travel of a device within a two-axis system. A device, such as a camera, is held in a two axis gimbal system having motors for driving the azimuth and pitch axes. A two degree-of-freedom gyroscope is fixed to the case of the device. A first derivative circuit is interposed between a first input port for a loop for controlling device movement with respect to a first axis and a second input port for a loop for controlling device movement with respect to a second axis. Likewise, a second derivative circuit is interposed between the two input ports so that a periodic signal driving with respect to one axis generates a derivative function for driving with respect to the cross-axis. The cross axis signal is scaled to counteract the direct torquing of the gyro rotor that otherwise prevents smooth oscillatory slewing or scanning by the device.Type: GrantFiled: July 31, 2001Date of Patent: September 14, 2004Assignee: Northrop Grumman Systems CorporationInventor: Stanley F. Wyse
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Patent number: 6742381Abstract: A damping performance evaluation apparatus for damping devices including: a support member detachably supporting a damping device in a state enabling the device to exhibit a damping effect thereof; a hammer member for applying oscillation force to the device caused by gravitational descent to strike the device; a double-strike preventing member for preventing the hammer member from dropping a second time due to rebound after initially striking the device, to prevent double-strike of the device by the hammer member; a vibration sensor installed at a vibration zone caused to vibrate through oscillation force applied by said hammer member, for outputting an electrical signal in response to vibration at the vibration zone; and a sensing member for sensing a vibration mode in the vibration zone on the basis of an output of said vibration sensor. A damping performance evaluation method is also disclosed.Type: GrantFiled: January 29, 2003Date of Patent: June 1, 2004Assignee: Tokai Rubber Industries, Ltd.Inventor: Hajime Maeno
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Patent number: 6619221Abstract: An oscillation suppression device comprises a base body to be secured to a ship body, a gimbals secured to the base body, a damper, a flywheel provided in the gimbals, and a motor for rotating the flywheel, etc. The gimbals is supported by bearings built into a pair of side walls of the base body, respectively, such that it can rotate around a first axis. The flywheel can rotate around a second axis. A rotor member of the motor is attached to the flywheel, and a stator member is attached to the gimbals. The rotor member and stator member are located inside the locus-of-rotation of the gimbals. The base body includes a cover portion covering the outer surface of the gimbals.Type: GrantFiled: April 3, 2002Date of Patent: September 16, 2003Assignee: Mitsubishi Heavy Industries, Ltd.Inventors: Katsuya Umemura, Youhei Ando
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Patent number: 6598492Abstract: A passive caging system for use in gyro-stabilized sensor platforms and the like, employing a pneumatic dashpot in place of automatic caging gyro brakes, pin-locking devices, springs, fluid damped pistons, or air bladders. A pneumatic dashpot in combination with a normally closed solenoid valve provides effective damping of shock forces while the system is in the unpowered state. When power is applied to the system, the solenoid valve is open and unrestricted movement of the sensor platform is enabled.Type: GrantFiled: November 17, 2000Date of Patent: July 29, 2003Assignee: Wescam Sonoma Inc.Inventor: Brian S. Corzilius
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Patent number: 6301982Abstract: A housed gyro-sensor 31 is housed in a rotation plate 33. The gyro-sensor 31 is mounted so that a rotation operation is enabled in a pitch axis direction about an axis in a mounting hole 24 formed on a housing of an inner face of the car navigation system 21. In this way, as shown in FIG. 8, even when the main body of the car navigation system 21 is not housed horizontally with respect to the vehicle, it is possible to regulate the mounting angle of the housed gyro sensor 31 in a horizontal direction by rotating the rotation plate 33. In order to realize how many times the rotation plate 33 needs to be rotated, standards for angle settings may be provided by directly printing the name of the vehicle type on an outer face of the rotation plate 33 or by printing the major angles.Type: GrantFiled: September 3, 1999Date of Patent: October 16, 2001Assignee: Mitsubishi Denki Kabushiki KaishaInventors: Hirotoshi Kubo, Kazunari Yamakado, Yasushi Takahashi, Hiroaki Sugino
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Patent number: 6191521Abstract: A vibration damper assembly for a ring resonator of a vibrating structure gyroscope has a female portion attachable to a body of the gyroscope so as to have limited resiliency with respect to the body in a direction substantially perpendicular to the body. A male portion is fixedly attachable at one end to a resonator of the gyroscope, projectable into the female portion and fixedly attachable at its other end in and to the female portion. The assembly permits damping of vibratory movement of the resonator in a direction substantially perpendicular thereto whilst retaining stiffness and freedom to vibrate for the resonator in the plane thereof.Type: GrantFiled: October 13, 1999Date of Patent: February 20, 2001Assignee: BAE Systems PLCInventors: Christopher Paul Fell, Ian David Hopkin, Timothy Robert Mason, Kevin Townsend