Patents by Inventor Kirill V. Shcheglov

Kirill V. Shcheglov has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 7093486
    Abstract: The present invention discloses a resonator gyroscope comprising a vibrationally isolated resonator including a proof mass, a counterbalancing plate having an extensive planar region, and one or more flexures interconnecting the proof mass and counterbalancing plate. A baseplate is affixed to the resonator by the one or more flexures and sense and drive electrodes are affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope. The isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.
    Type: Grant
    Filed: February 4, 2005
    Date of Patent: August 22, 2006
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Patent number: 7040163
    Abstract: The present invention discloses an inertial sensor comprising a planar mechanical resonator with embedded sensing and actuation for substantially in-plane vibration and having a central rigid support for the resonator. At least one excitation or torquer electrode is disposed within an interior of the resonator to excite in-plane vibration of the resonator and at least one sensing or pickoff electrode is disposed within the interior of the resonator for sensing the motion of the excited resonator. In one embodiment, the planar resonator includes a plurality of slots in an annular pattern; in another embodiment, the planar mechanical resonator comprises four masses; each embodiment having a simple degenerate pair of in-plane vibration modes.
    Type: Grant
    Filed: August 12, 2003
    Date of Patent: May 9, 2006
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: Kirill V. Shcheglov, A. Dorian Challoner
  • Patent number: 7017410
    Abstract: The present invention discloses a resonator gyroscope comprising a vibrationally isolated resonator including a proof mass, a counterbalancing plate having an extensive planar region, and one or more flexures interconnecting the proof mass and counterbalancing plate. A baseplate is affixed to the resonator by the one or more flexures and sense and drive electrodes are affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope. The isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.
    Type: Grant
    Filed: February 20, 2003
    Date of Patent: March 28, 2006
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Patent number: 6990863
    Abstract: The present invention discloses a resonator gyroscope including an isolated resonator. One or more flexures support the isolated resonator and a baseplate is affixed to the resonator by the flexures. Drive and sense elements are affixed to the baseplate and used to excite the resonator and sense movement of the gyroscope. In addition, at least one secondary element (e.g., another electrode) is affixed to the baseplate and used for trimming isolation of the resonator. The resonator operates such that it transfers substantially no net momentum to the baseplate when the resonator is excited. Typically, the isolated resonator comprises a proof mass and a counterbalancing plate.
    Type: Grant
    Filed: April 25, 2003
    Date of Patent: January 31, 2006
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Patent number: 6955084
    Abstract: The present invention discloses a gyroscope comprising an isolated resonator including a post proof mass and counterbalancing plate. One or more double beam flexures each interconnect the counterbalancing plate and the proof mass with a first and a second beam attached to the post proof mass and a third and a fourth beam attached to the counterbalancing plate. A baseplate is affixed to the resonator by the double beam flexures. The counterbalancing plate and the proof mass transfer substantially no net momentum to the baseplate when the resonator is excited.
    Type: Grant
    Filed: April 10, 2003
    Date of Patent: October 18, 2005
    Assignees: The Boeing Company, California Institute of Technology
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • 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: 6823734
    Abstract: The present invention discloses an isolated electrostatic biased resonator gyroscope. The gyroscope includes an isolated resonator having a first and a second differential vibration mode, a baseplate supporting the isolated resonator, a plurality of excitation affixed to the baseplate for exciting the first differential vibration mode, a plurality of sensing electrodes affixed to the baseplate for sensing movement of the gyroscope through the second differential vibration mode and a plurality of bias electrodes affixed to the baseplate for trimming isolation of the resonator and substantially minimizing frequency split between the first and second differential vibration modes. Typically, the isolated resonator comprises a proof mass and a counterbalancing plate with the bias electrodes disposed on the baseplate below.
    Type: Grant
    Filed: April 25, 2003
    Date of Patent: November 30, 2004
    Assignees: California Institute of Technology, The Boeing Company
    Inventors: Ken J. Hayworth, Kirill V. Shcheglov, Todd E. Humphreys, A. Dorian Challoner
  • Publication number: 20040226370
    Abstract: The present invention discloses an isolated electrostatic biased resonator gyroscope. The gyroscope includes an isolated resonator having a first and a second differential vibration mode, a baseplate supporting the isolated resonator, a plurality of excitation affixed to the baseplate for exciting the first differential vibration mode, a plurality of sensing electrodes affixed to the baseplate for sensing movement of the gyroscope through the second differential vibration mode and a plurality of bias electrodes affixed to the baseplate for trimming isolation of the resonator and substantially minimizing frequency split between the first and second differential vibration modes. Typically, the isolated resonator comprises a proof mass and a counterbalancing plate with the bias electrodes disposed on the baseplate below.
    Type: Application
    Filed: April 25, 2003
    Publication date: November 18, 2004
    Applicants: California Institute of Technology, The Boeing Company
    Inventors: Ken J. Hayworth, Kirill V. Shcheglov, Todd E. Humphreys, A. Dorian Challoner
  • Patent number: 6796179
    Abstract: A split-resonator integrated-post vibratory microgyroscope may be fabricated using micro electrical mechanical systems (MEMS) fabrication techniques. The microgyroscope may include two gyroscope sections bonded together, each gyroscope section including resonator petals, electrodes, and an integrated half post. The half posts are aligned and bonded to act as a single post.
    Type: Grant
    Filed: May 16, 2003
    Date of Patent: September 28, 2004
    Assignee: California Institute of Technology
    Inventors: Youngsam Bae, Ken J. Hayworth, Kirill V. Shcheglov
  • Publication number: 20040055381
    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: Application
    Filed: August 12, 2003
    Publication date: March 25, 2004
    Inventors: Kirill V. Shcheglov, A. Dorian Challoner, Ken J. Hayworth, Dean V. Wiberg, Karl Y. Yee
  • Publication number: 20040055380
    Abstract: The present invention discloses an inertial sensor comprising a planar mechanical resonator with embedded sensing and actuation for substantially in-plane vibration and having a central rigid support for the resonator. At least one excitation or torquer electrode is disposed within an interior of the resonator to excite in-plane vibration of the resonator and at least one sensing or pickoff electrode is disposed within the interior of the resonator for sensing the motion of the excited resonator. In one embodiment, the planar resonator includes a plurality of slots in an annular pattern; in another embodiment, the planar mechanical resonator comprises four masses; each embodiment having a simple degenerate pair of in-plane vibration modes.
    Type: Application
    Filed: August 12, 2003
    Publication date: March 25, 2004
    Inventors: Kirill V. Shcheglov, A. Dorian Challoner
  • Publication number: 20040050160
    Abstract: A split-resonator integrated-post vibratory microgyroscope may be fabricated using micro electrical mechanical systems (MEMS) fabrication techniques. The microgyroscope may include two gyroscope sections bonded together, each gyroscope section including resonator petals, electrodes, and an integrated half post. The half posts are aligned and bonded to act as a single post.
    Type: Application
    Filed: May 16, 2003
    Publication date: March 18, 2004
    Inventors: Youngsam Bae, Ken J. Hayworth, Kirill V. Shcheglov
  • Publication number: 20030205087
    Abstract: The present invention discloses a gyroscope comprising an isolated resonator including a post proof mass and counterbalancing plate. One or more double beam flexures each interconnect the counterbalancing plate and the proof mass with a first and a second beam attached to the post proof mass and a third and a fourth beam attached to the counterbalancing plate. A baseplate is affixed to the resonator by the double beam flexures. The counterbalancing plate and the proof mass transfer substantially no net momentum to the baseplate when the resonator is excited.
    Type: Application
    Filed: April 10, 2003
    Publication date: November 6, 2003
    Applicants: THE BOEING COMPANY, CALIFORNIA INSTITUTE OF TECHNOLOGY
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Publication number: 20030188577
    Abstract: The present invention discloses a resonator gyroscope including an isolated resonator. One or more flexures support the isolated resonator and a baseplate is affixed to the resonator by the flexures. Drive and sense elements are affixed to the baseplate and used to excite the resonator and sense movement of the gyroscope. In addition, at least one secondary element (e.g., another electrode) is affixed to the baseplate and used for trimming isolation of the resonator. The resonator operates such that it transfers substantially no net momentum to the baseplate when the resonator is excited. Typically, the isolated resonator comprises a proof mass and a counterbalancing plate.
    Type: Application
    Filed: April 25, 2003
    Publication date: October 9, 2003
    Applicants: THE BOEING COMPANY, CALIFORNIA INSTITUTE OF TECHNOLOGY
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Publication number: 20030150267
    Abstract: The present invention discloses a resonator gyroscope comprising a vibrationally isolated resonator including a proof mass, a counterbalancing plate having an extensive planar region, and one or more flexures interconnecting the proof mass and counterbalancing plate. A baseplate is affixed to the resonator by the one or more flexures and sense and drive electrodes are affixed to the baseplate proximate to the extensive planar region of the counterbalancing plate for exciting the resonator and sensing movement of the gyroscope. The isolated resonator transfers substantially no net momentum to the baseplate when the resonator is excited.
    Type: Application
    Filed: February 20, 2003
    Publication date: August 14, 2003
    Applicant: THE BOEING COMPANY
    Inventors: A. Dorian Challoner, Kirill V. Shcheglov
  • Patent number: 6219145
    Abstract: An optical profiler is modified in a way which allows it to image a MEMS device at various points during the movement of the MEMS device. The light source is synchronized with a desired movement of the MEMS device. The light source produces pulse at each synchronization period. During each pulse, an interferometric measurement is carried out. So long as the pulse is short enough such that the device does not move significantly, a detection of the position of the device can be accurately obtained.
    Type: Grant
    Filed: February 16, 1999
    Date of Patent: April 17, 2001
    Assignee: California Institute of Technology
    Inventors: Roman C. Gutierrez, Kirill V. Shcheglov, Tony Tang