Micromachined Tuning Fork Gyroscopes With Ultra-High Sensitivity And Shock Rejection
Tech ID: 19585 / UC Case 2009-748-0
Brief Description
University researchers have designed a family of new dual mass and quadruple mass tuning fork architectures addressing the limitations of the conventional designs. In the dual mass design, the spurious in-phase drive-mode is shifted above the operational frequency to improve the response characteristics.
Full Description
Unlike conventional tuning fork gyroscopes, the proposed architecture prioritizes the quality factor of the sense-mode by mechanical design, where the linearly coupled anti-phase sense-mode is balanced in both the linear momentum as well as moment of reaction forces (torque) in order to minimize dissipation of energy through the substrate and enable ultra-high mechanical sensitivity to the input angular rate.
The second, quadruple mass design builds upon the dual mass architecture by coupling together two dual mass devices to achieve completely symmetric, mode-matched mechanical structure with ultra-high quality factor in both the drive- and the sense-mode. The quadruple mass design of the sensor element preserves the ultra-high sensitivity of the dual mass design. At the same time, the quadruple mass design provides complete mechanical rejection of external vibrations and shocks along both drive and sense axes, and improved robustness to fabrication imperfections and temperature induced frequency drifts.
Applications
These new ultra-high resolution tuning fork gyroscope architectures provide a path to silicon MEMS-based gyrocompassing and inertial navigation systems.
Background
The operation of micromachined vibratory gyroscopes is based on a transfer of energy between two modes of vibration caused by the Coriolis effect. When the drive- and sense-mode resonant frequencies are equal, or mode-matched, the sensor output is increased proportionally to the sense-mode quality factor. Anti-phase driven tuning fork architectures are often used due to their ability to reject common mode acceleration inputs. Conventional tuning fork designs with linear anti-phase drive-modes present several major drawbacks: presence of the parasitic low-frequency structural mode of in-phase vibrations, limitation of the maximal achievable sense-mode quality factor by approximately half of the drive-mode quality factor due to substrate energy dissipation caused by the torque imbalance, and difficulty of maintaining mode-matched condition over the practical temperature ranges.
Patent Status
| Country | Type | Number | Dated | Case |
| United States Of America | Issued Patent | 8,322,213 | 12/04/2012 | 2009-748 |
Inventors
- Shkel, Andrei M.
Other Information
Categorized As
Related cases
2009-748-0
Keywords
gyronavigation, gyroscope, inertial naviagation
Contact
Demetri Andrikos / dandriko@uci.edu / tel: View Phone Number. Please reference Tech ID #19585.
ADDITIONAL TECHNOLOGIES BY THESE INVENTORS
- Micromachined Gyroscope Design Allowing for Both Robust Wide-Bandwidth and Precision Mode-Matched Operation
- Three-Dimensional Wafer-Scale Batch-Micromachined Angle/Angular Rate Microshell Resonator Gyroscope
- 3-D Folded MEMS Technology For Multi-Axis Sensor Systems
- High Range Digital Angular Rate Sensor Based On Frequency Modulations
- Multi-Axis Chip-Scale Mems Inertial Measurement Unit (Imu) System Based On Frequency Modulation