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Micromachined rate and acceleration sensor

Patent 5241861 Issued on September 7, 1993. Estimated Expiration Date: Icon_subject February 8, 2011. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Resonator force transducer
Patent #: 4372173
Issued on: 02/08/1983
Inventor: EerNisse ,   et al.

Apparatus and method for measuring specific force and angular rate
Patent #: 4445376
Issued on: 05/01/1984
Inventor: Merhav

Method for determining acceleration
Patent #: 4467651
Issued on: 08/28/1984
Inventor: Peters ,   et al.

Angular rate sensor utilizing two vibrating accelerometers secured to a parallelogram linkage
Patent #: 4510802
Issued on: 04/16/1985
Inventor: Peters

Two axis angular rate and specific force sensor utilizing vibrating accelerometers
Patent #: 4512192
Issued on: 04/23/1985
Inventor: Peters

Accelerometer with beam resonator force transducer
Patent #: 4517841
Issued on: 05/21/1985
Inventor: Peters ,   et al.

Digital processor for use with an accelerometer based angular rate sensor
Patent #: 4522062
Issued on: 06/11/1985
Inventor: Peters

Vibratory angular rate sensing system
Patent #: 4538461
Issued on: 09/03/1985
Inventor: Juptner ,   et al.

Counting apparatus and method for frequency sampling
Patent #: 4541105
Issued on: 09/10/1985
Inventor: Lee ,   et al.

Apparatus for measuring inertial specific force and angular rate of a moving body
Patent #: 4590801
Issued on: 05/27/1986
Inventor: Merhav

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Inventor

Assignee

Application

No. 653533 filed on 02/08/1991

US Classes:

73/514.02, Angular acceleration73/504.04Vibratory mass

Examiners

Primary: Chapman, Jeanette E.

Attorney, Agent or Firm

International Classes

G01P 009/04
G01P 015/08

Abstract

A sensor (10) is disclosed for measuring the specific force and angular rotation rate of a moving body and is micromachined from a silicon substrate (16). First and second accelerometers (32a and b) are micromachined from the silicon substrate (16), each having a force sensing axis (38) and producing an output signal of the acceleration of the moving body along its force sensing axis (38). The first and second accelerometers (32a and b) are mounted within the substrate (16) to be moved along a vibration axis (41). The first and second accelerometers (32a and b) are vibrated or dithered to increase the Coriolis component of the output signals from the first and second accelerometers (32a and b). A sinusoidal drive signal of a predetermined frequency is applied to a conductive path (92) disposed on each of the accelerometers. Further, magnetic flux is directed to cross each of the conductive paths (92), whereby the interaction of the magnetic flux and of the drive signal passing therethrough causes the desired dithering motion. A link (72) is formed within the silicon substrate (16) and connected to each of the accelerometers (32a and b), whereby motion imparted to one results in a like, but opposite motion applied to the other accelerometer (32). Further, a unitary magnet (20) and its associated flux path assembly direct and focus the magnetic flux through the first and second accelerometers (32a and b) formed within the silicon substrate (16).

Other References

  • Albert P. Pisano, "Resonant-Structure Micromotors," Micro Electro Mechanical Systems, Feb. 20-22, 1989, IEEE Catalog No. 89TH0249-3, Library of Congress No. 88-83988
  • William C. Tang, et al., "Laterally Driven Polysilicon Resonant Microstructures," Micro Electro Mechanical Systems, Feb. 20-22, 1989, IEEE Catalog No. 89TH0249-3, Library of Congress No. 88-8398
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