| 摘要 |
The invention relates to a Coriolis gyro having an arrangement which comprises a substrate (5, 22, 24, 26), at least two individual structures (61, 62, 63, 64, 500, 600, 700, 800) and spring elements (for example 1, 2, 3, 21, 23, 25), with the spring elements (for example 1, 2, 3, 21, 23, 25) coupling the individual structures (61, 62, 63, 64, 500, 600, 700, 800) to the substrate (5, 22, 24, 26) and to one another, having force transmitters (for example 514, 614, 714, 814) and having taps (for example 534, 634, 734, 834), wherein the arrangement has at least one excitation mode (7) which can be excited by the force transmitters (for ex-ample 514, 614, 714, 814) and at least one detection mode (8) which can be measured by the taps (for example 534, 634, 734, 834), wherein the excitation mode (7) and the de-tection mode (8) are closed off, as a result of which no dis-turbance excitations of the excitation mode and of the de-tection mode can be caused by linear accelerations and/or vibrations if there is no need to take account of manufactur-ing tolerances.
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