Method for measurement of rotation rates/accelerations using...

Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C073S504120, C073S504140

Reexamination Certificate

active

07340954

ABSTRACT:
A Coriolis gyro includes a first and a second resonator, each in the form of a coupled system comprising first and second linear oscillators. The first resonator can be caused to oscillate in antiphase with respect to the second resonator along a common oscillation axis. A system coupled in this way has the advantage that it is possible to measure rotation rate and acceleration simultaneously, with insensitivity to disturbances (e.g., externally or internally acting vibrations).

REFERENCES:
patent: 6067858 (2000-05-01), Clark et al.
patent: 6934665 (2005-08-01), Rober
patent: 7159460 (2007-01-01), Nicu et al.
patent: 4442033 (1996-05-01), None
patent: 10107327 (2001-08-01), None
patent: 1253399 (2002-10-01), None
patent: 1359391 (2003-11-01), None
patent: 0216871 (2002-02-01), None
patent: 02066927 (2002-08-01), None
patent: 03014669 (2003-02-01), None
Article: Geiger et al., “New Designs of Micromachined Vibrating Rate Gyroscopes with Decoupled Oscillation Modes”,1997 International Conference on Solid-State Sensors and Actuators(Chicago Jun. 16-19, 1997), pp. 1129-1132.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Method for measurement of rotation rates/accelerations using... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method for measurement of rotation rates/accelerations using..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for measurement of rotation rates/accelerations using... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3973143

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.