Micro-electro-mechanical device with compensation of errors due to disturbance forces, such as quadrature components
US-2015377624-A1 · Dec 31, 2015 · US
US9702698B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9702698-B2 |
| Application number | US-201514809941-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 27, 2015 |
| Priority date | Feb 4, 2013 |
| Publication date | Jul 11, 2017 |
| Grant date | Jul 11, 2017 |
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One or more vibration plate layers of a diaphragm part are formed by a thin film forming technique. When a resonance frequency in a resonance vibration mode calculated from dimensions of a structure of an angular velocity sensor and an elastic parameter of a material thereof is defined as f kilohertz, a mass of a weight part is defined as M milligrams, a circumference of the diaphragm part is defined as r meters, a stress applied to a piezoelectric layer is defined as σ p pascals, a thickness thereof is defined as t p meters, a stress applied to an n-th layer from the weight part in a vibration plate portion constituted by a plurality of layers including a lower electrode and the vibration plate layers is defined as σ n pascals, and a thickness thereof is defined as t n meters (where n is a natural number), T eff expressed by T eff =r(σ p t p +Σσ n t n )/M satisfies {(−0.36f 2 +210)/33}≦T eff ≦{(0.44f 2 +210)/33}.
Opening claim text (preview).
What is claimed is: 1. An angular velocity sensor comprising: a flexible diaphragm part including a laminated structure, the laminated structure of the diaphragm part including an upper electrode, a piezoelectric layer, a lower electrode, and one or more vibration plate layers, the upper electrode including a driving electrode part and a detection electrode part, the driving electrode part and the detection electrode part being pattern-arranged; a pedestal section configured to support an outer circumference of the diaphragm part; and a weight section joined to a central part of the diaphragm part, the angular velocity sensor being configured to cause the weight section to vibrate using an inverse piezoelectric effect of a piezoelectric body by applying an electric field to the piezoelectric layer via the driving electrode part, and detect a displacement generated in the weight section based on a Coriolis force, the displacement being detected by a piezoelectric effect from the detection electrode part, the vibration plate layer being formed by a thin film forming technique, and when a resonance frequency in a resonance vibration mode calculated from dimensions of a structural body of the angular velocity sensor and an elastic parameter of a material of the structural body is f kilohertz, a mass of the weight section is M milligrams, a circumferential length of the diaphragm part is r meters, a stress acting on the piezoelectric layer is σ P pascals, a film thickness of the piezoelectric layer is t P meters, a stress acting on an n-th layer of a vibration plate portion constituted by a plurality of layers including the lower electrode and the one or more vibration plate layers is σ n pascals, the n-th layer being n-th from a side of the weight section, and a film thickness of the n-th layer being t n meters, and when n is a natural number, then, an effective tension, T eff that is expressed by an expression: T eff = r ( σ p t p + ∑ n σ n t n ) M satisfies: - 0.36 f 2 + 210 33 ≤ T eff ≤ 0.44 f 2 + 210 33 . 2. The angular velocity sensor as set forth in claim 1 , wherein a following expression is satisfied: - 0.28 f 2 + 210 33 ≤ T eff ≤ 0.32 f 2 + 210 33 . 3. The angular velocity sensor as set forth in claim 1 , wherein a following expression is satisfied: - 0.19 f 2 + 210 33 ≤ T eff ≤ 0.21 f 2 + 210 33
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