Abstract:
A micromechanical inertial sensor having at least one seismic mass which may be deflected relative to a substrate, and at least one electrode surface which in terms of circuitry, together with at least portions of the seismic mass forms at least one capacitor having a capacitance which is dependent on the deflection of the seismic mass. At least one additional auxiliary electrode is included which is located outside the region which forms the capacitor and which may be set at a potential that deviates from the potential of the seismic mass.
Abstract:
A yaw rate sensor is described which includes a substrate having a main plane of extension and a Coriolis element, the Coriolis element being excitable to a driving oscillation along a first direction parallel to the main plane of extension, using a driving arrangement, and a deflection of the Coriolis element along a second direction perpendicular to the first direction being detectable, and the yaw rate sensor having an interference element for exciting the Coriolis element to an interference oscillation.
Abstract:
A rotation rate sensor for detecting a rotation rate about a rotational axis parallel to a main extension plane of a substrate of the sensor includes: a first oscillating mass; and a second oscillating mass mechanically coupled to the first oscillating mass. The first oscillating mass is (i) deflectable along a first oscillations plane parallel to the main extension plane, (ii) extends in a planar manner parallel to the first oscillations plane in a rest position, and (iii) deflectable out of the first oscillations plane into a first deflection position. The second oscillating mass is (i) deflectable along a second oscillations plane parallel to the first oscillations plane, (ii) extends in a planar manner parallel to the second oscillations plane in a rest position, and (iii) deflectable out of the second oscillations plane into a second deflection position.
Abstract:
A yaw rate sensor is described which includes a substrate having a main plane of extension and a Coriolis element, the Coriolis element being excitable to a driving oscillation along a first direction parallel to the main plane of extension, using a driving arrangement, and a deflection of the Coriolis element along a second direction perpendicular to the first direction being detectable, and the yaw rate sensor having an interference element for exciting the Coriolis element to an interference oscillation.
Abstract:
A micromechanical inertial sensor having at least one seismic mass which may be deflected relative to a substrate, and at least one electrode surface which in terms of circuitry, together with at least portions of the seismic mass forms at least one capacitor having a capacitance which is dependent on the deflection of the seismic mass. At least one additional auxiliary electrode is included which is located outside the region which forms the capacitor and which may be set at a potential that deviates from the potential of the seismic mass.
Abstract:
The invention relates to a gas sensor comprising a membrane layer (3) formed on a semiconductor substrate (2), an evaluation structure (7) being arranged on said substrate in an evaluation area (8) and a heating structure (9) outside the evaluation area (8), in addition to a gas-sensitive layer (10) arranged above the evaluation structure (7) and the heating structure (9), wherein said gas-sensitive layer (10) can be heated by the heating structure (9) and the electrical resistance of the gas-sensitive layer (10) can be evaluated by the evaluation structure (7). The heating structure (9) is arranged on an adhesion-promoting oxide layer (6) on the top surface of the membrane layer (3) and is separated from the gas-sensitive layer by a cover oxide layer (11). In order to enable reliable functionality of the gas sensor, that in the evaluation area (8), an adhesion-promoting layer (13) insensitive to oxide etching is arranged between the membrane layer (3) and the evaluation structure (7) or the evaluation structure (7) in the evaluation area (8) corresponding to the heating structure (9) is separated from the gas-sensitive layer (10) by the cover oxide layer (11), wherein the cover oxide layer (11) has contact holes (12) which uncover a central area of the surface of the evaluation structure (7) in order to produce a direct contact between the evaluation structure (7) and the gas-sensitive layer (10).