Patents Represented by Attorney Origin Law
  • Patent number: 7100444
    Abstract: The present invention discloses a resonator gyroscope comprising a resonator including two bodies, each with a center of mass and transverse inertia symmetry about an axis that are substantially coincident and each supported by one or more elastic elements and wherein the bodies together forming two differential rocking modes of vibration transverse to the axis with substantially equal frequencies and wherein the two bodies transfer substantially no net momentum to the baseplate when the resonator is excited. The gyroscope further includes a baseplate affixed to the resonator by the one or more elastic elements.
    Type: Grant
    Filed: April 2, 2003
    Date of Patent: September 5, 2006
    Assignee: The Boeing Company
    Inventor: A. Dorian Challoner
  • Patent number: 7027476
    Abstract: Tunable semiconductor lasers are disclosed requiring minimized coupling regions. Multiple laser embodiments employ ring resonators or ring resonator pairs using only a single coupling region with the gain medium are detailed. Tuning can be performed by changing the phase of the coupling coefficient between the gain medium and a ring resonator of the laser. Another embodiment provides a tunable laser including two Mach-Zehnder interferometers in series and a reflector coupled to a gain medium.
    Type: Grant
    Filed: August 11, 2003
    Date of Patent: April 11, 2006
    Assignee: California Institute of Technology
    Inventors: Shervin Taghavi-Larigani, Jakob J. Vanzyl, Amnon Yariv
  • Patent number: 6999658
    Abstract: The invention discloses a semi-ring Fabry-Perot (SRFP) optical resonator structure comprising a medium including an edge forming a reflective facet and a waveguide within the medium, the waveguide having opposing ends formed by the reflective facet. The performance of the SRFP resonator can be further enhanced by including a Mach-Zehnder interferometer in the waveguide on one side of the gain medium. The optical resonator can be employed in a variety of optical devices. Laser structures using at least one SRFP resonator are disclosed where the resonators are disposed on opposite sides of a gain medium. Other laser structures employing one or more resonators on one side of a gain region are also disclosed.
    Type: Grant
    Filed: June 30, 2003
    Date of Patent: February 14, 2006
    Assignee: California Institute of Technology
    Inventors: Shervin Taghavi-Larigani, Jakob J. Vanzyl, Amnon Yariv
  • Patent number: 6944931
    Abstract: The present invention discloses an inertial sensor having an integral resonator. A typical sensor comprises a planar mechanical resonator for sensing motion of the inertial sensor and a case for housing the resonator. The resonator and a wall of the case are defined through an etching process. A typical method of producing the resonator includes etching a baseplate, bonding a wafer to the etched baseplate, through etching the wafer to form a planar mechanical resonator and the wall of the case and bonding an end cap wafer to the wall to complete the case.
    Type: Grant
    Filed: August 12, 2003
    Date of Patent: September 20, 2005
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: Kirill V. Shcheglov, A. Dorian Challoner, Ken J. Hayworth, Dean V. Wiberg, Karl Y. Yee
  • Patent number: 6915215
    Abstract: Embodiments of the invention generally encompass a digital, application specific integrated circuit (ASIC) has been designed to perform excitation of a selected mode within a vibratory rate gyroscope, damping, or “force-rebalance,” of other modes within the sensor, and signal demodulation of the in-phase and quadrature components of the signal containing the angular rate information. The ASIC filters dedicated to each channel may be individually programmed to accommodate different rate sensor designs/technology or variations within the same class of sensors. The ASIC architecture employs a low-power design, making the ASIC, particularly suitable for use in power-sensitive applications.
    Type: Grant
    Filed: June 25, 2003
    Date of Patent: July 5, 2005
    Assignees: The Boeing Company, California Institute of Technology, The Regents of the University of California
    Inventors: Robert M'Closkey, A. Dorian Challoner, Eugene Grayver, Ken J. Hayworth