Monolithic accelerometer with flexurally mounted force transducer

• US 5,165,279 A
• Filed: 07/06/1989
• Issued: 11/24/1992
• Est. Priority Date: 07/06/1989
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Peters, Rex B., Norling, Brian L.
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US07/544,221
• Time in Patent Office: 1,237 Days
• Field of Search: 73/517 AV, 73/516 R, 73/517 R, 73/DIG. 1, 73/DIG. 4
• US Class Current: 73/514.14
• CPC Class Codes: G01P 1/003 used for damping
• CPC Class Codes: G01P 15/0802 Details
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: G01P 2015/0828 the mass being of the paddle type being suspended at one of its longitudinal ends
• CPC Class Codes: Y10S 73/01 Vibration

Abstract

An accelerometer comprising a monolithic crystalline substrate, the substrate comprising a support, a proof mass, and a force transducer. The proof mass is connected to the support by one or more proof mass flexures that permit the proof mass to rotate with respect to the support about a hinge axis. One end of the force transducer is connected to the support, and the other end is connected to the proof mass by a transducer flexure. The transducer flexure has a thickness substantially less than the thickness of the transducer, such that when the proof mass rotates, the transducer rotates with respect to the proof mass about a transducer axis that passes through the transducer flexure. Preferably, the transducer axis is offset from the hinge axis in a manner so as to cancel nonlinearities in the force transducer, and the length of the proof mass along the pendulous axis is less than half the length of the transducer. Damping plates are positioned above and below the proof mass, and provide shock stops and damping.

Claims

1. An accelerometer for measuring acceleration up to a predetermined full-scale input acceleration, the accelerometer comprising a monolithic crystalline substrate, the substrate comprising:

a support;

a proof mass;

at least one proof mass flexure connecting the proof mass to the support such that the proof mass can rotate with respect to the support about a hinge axis in response to acceleration directed along a sensitive axis normal to the hinge axis;

a force transducer having a longitudinal force sensing axis that is parallel to a pendulous axis, the pendulous axis being normal to the hinge axis and to the sensitive axis, the force transducer being characterized by a predetermined relationship between applied force and output frequency, said relationship including a second order nonlinearity; and

a transducer flexure connecting the second end of the transducer to the proof mass, the transducer flexure having a thickness substantially less than the thickness of the transducer such that when the proof mass rotates with respect to the support, the transducer rotates with respect to the proof mass about a transducer axis that passes through the transducer flexure, the transducer axis being offset from the hinge axis in a direction along the pendulous axis, said offset being selected so as to reduce said nonlinearity between applied force and frequency.

2. The accelerometer of claim 1, wherein said offset is selected so as to substantially cancel said nonlinearity.

3. The accelerometer of claim 1, wherein the support, proof mass and force transducer all have a common thickness along the sensitive axis, and all lie in a common plane.

4. The accelerometer of claim 1, wherein the force transducer is a dual vibrating beam force transducer.

5. The accelerometer of claim 4, wherein said offset is selected so as to substantially cancel said nonlinearity.

6. The accelerometer of claim 4, wherein the force transducer comprises first and second beams extending between first and second end sections, and a connecting member between one of the end sections and the transducer flexure, the transducer, proof mass and connecting member all having a common thickness along the sensitive axis, and all lying in the same plane.

7. The accelerometer of claim 1, further comprising first and second damping plates positioned above and below the substrate, the damping plates being spaced from the proof mass by gaps, the gaps being sized such that the damping plates function to limit travel of the proof mass in response to over range inputs.

8. The accelerometer of claim 7, wherein the gaps serve to damp vibration of the proof mass, such that the proof mass has a Q no larger than about 10 at resonance.

9. The accelerometer of claim 1, wherein the length of the proof mass along the direction parallel to the pendulous axis is less than half the length of the force transducer along the same direction.