Method and apparatus for thermally actuated self testing of silicon structures
First Claim
1. A method of testing a machined silicon structure, said silicon structure including at least one flexure beam means for permitting one portion of said silicon structure to move relative to another portion of said silicon structure in a flexure direction, said flexure beam means having a neutral axis, said silicon structure having a means for providing an output when flexed, said silicon structure including at least one thermal actuator beam having an axis of expansion and a length connecting said one portion of said silicon structure with said another portion of said silicon structure, said axis of expansion of said thermal actuator beam displaced from said neutral axis of said flexure beam means in a direction parallel to said flexure direction, said method comprising the steps of:
- changing said length of said at least one thermal actuator beam thereby displacing said another portion with respect to said one portion and flexing said flexure beam; and
comparing said flexure beam output when flexed to a value and indicating the operability of said means for providing an output, wherein said means for providing an output comprises a piezoresistive portion of said flexure beam means, and said comparing step includes comparing resistance of said piezoresistive portion with a fixed value of resistance, wherein said silicon structure comprises a pressure sensor and said one portion of said silicon structure is a diaphragm and said another portion of said silicon structure is a support frame, said flexure beam means comprises a silicon structure surrounding a periphery of said diaphragm and connecting said diaphragm periphery to said support frame, said changing step includes displacing said diaphragm with respect to said support frame.
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Abstract
The present invention discloses a method and apparatus for testing the operational capability of flexure area equipped sensors especially those made of micromachined silicon. A thermal actuator beam is provided to bridge the structures which are joined by the flexure area. During the test, the beam'"'"'s temperature is changed relative to that of the flexure area so as to provide a differential expansion or contraction. The result is that the flexure area bends and conventional bending sensors for the flexure area can sense the amount of bend. By comparing the actual amount of bend sensed with the amount expected from the temperature change applied to the beam, the operational capability can be determined.
114 Citations
13 Claims
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1. A method of testing a machined silicon structure, said silicon structure including at least one flexure beam means for permitting one portion of said silicon structure to move relative to another portion of said silicon structure in a flexure direction, said flexure beam means having a neutral axis, said silicon structure having a means for providing an output when flexed, said silicon structure including at least one thermal actuator beam having an axis of expansion and a length connecting said one portion of said silicon structure with said another portion of said silicon structure, said axis of expansion of said thermal actuator beam displaced from said neutral axis of said flexure beam means in a direction parallel to said flexure direction, said method comprising the steps of:
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changing said length of said at least one thermal actuator beam thereby displacing said another portion with respect to said one portion and flexing said flexure beam; and comparing said flexure beam output when flexed to a value and indicating the operability of said means for providing an output, wherein said means for providing an output comprises a piezoresistive portion of said flexure beam means, and said comparing step includes comparing resistance of said piezoresistive portion with a fixed value of resistance, wherein said silicon structure comprises a pressure sensor and said one portion of said silicon structure is a diaphragm and said another portion of said silicon structure is a support frame, said flexure beam means comprises a silicon structure surrounding a periphery of said diaphragm and connecting said diaphragm periphery to said support frame, said changing step includes displacing said diaphragm with respect to said support frame. - View Dependent Claims (2, 3)
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4. A thermally actuated self test mechanism for a micro machined silicon structure, said silicon structure including at least one flexure beam means for permitting one portion of said silicon structure to move relative to another portion of said silicon structure in a flexure direction, said flexure beam means having a neutral axis, said silicon structure having a means for providing an output when flexed, said self test mechanism comprising:
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at least one thermal actuator beam having an axis of expansion and a length connecting said one portion of said silicon structure with said another portion of said silicon structure, said axis of expansion of said at least one thermal actuator beam displaced from said neutral axis of said flexure beam means in a direction parallel to said flexure direction; means for thermally changing said length of said at least one thermal actuator beam thereby displacing said another portion with respect to said one portion and flexing said flexure beam means; and means for comparing said output when said flexure beam means is flexed to a value and indicating the operability of said means for providing an output. - View Dependent Claims (5, 6, 7, 8, 9, 10, 11, 12, 13)
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Specification