Micromachined rate and acceleration sensor

• US 5,627,314 A
• Filed: 09/01/1995
• Issued: 05/06/1997
• Est. Priority Date: 02/08/1991
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Hulsing, Rand H. II
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US08/522,812
• Time in Patent Office: 613 Days
• Field of Search: 73/504.04, 73/504.12, 73/504.14, 73/504.15, 73/504.16, 73/510
• US Class Current: 73/504.04
• CPC Class Codes: F02G 1/044 having at least two working members, e.g. pistons, delivering power output
• CPC Class Codes: F02G 1/0445 Engine plants with combined cycles, e.g. Vuilleumier
• CPC Class Codes: F02G 2250/18 Vuilleumier cycles
• CPC Class Codes: F02G 2253/03 Stem seals
• CPC Class Codes: F16F 2230/0052 Physically guiding or influencing
• CPC Class Codes: F16F 2230/34 Flexural hinges
• CPC Class Codes: F16L 37/24 in which the connection is made by inserting one member axially into the other and rotating it to a limited extent, e.g. with bayonet action
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis
• CPC Class Codes: G01C 19/5747 each sensing mass being connected to a driving mass, e.g. driving frames
• CPC Class Codes: G01P 15/0802 Details
• CPC Class Codes: G01P 15/097 by vibratory elements
• CPC Class Codes: G01P 15/18 in two or more dimensions
• 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

A sensor (10) is disclosed for measuring the specific force and angular rotation rate of a moving body and is micromachined from a silicon substrate (16). First and second accelerometers (32a and b) are micromachined from the silicon substrate (16), each having a force sensing axis (38) and producing an output signal of the acceleration of the moving body along its force sensing axis (38). The first and second accelerometers (32a and b) are mounted within the substrate (16) to be moved along a vibration axis (41). The first and second accelerometers (32a and b) are vibrated or dithered to increase the Coriolis component of the output signals from the first and second accelerometers (32a and b). A sinusoidal drive signal of a predetermined frequency is applied to a conductive path (92) disposed on each of the accelerometers. Further, magnetic flux is directed to cross each of the conductive paths (92), whereby the interaction of the magnetic flux and of the drive signal passing therethrough causes the desired dithering motion. A link (72) is formed within the silicon substrate (16) and connected to each of the accelerometers (32a and b), whereby motion imparted to one results in a like, but opposite motion applied to the other accelerometer (32). Further, a unitary magnet (20) and its associated flux path assembly direct and focus the magnetic flux through the first and second accelerometers (32a and b) formed within the silicon substrate (16).

Claims

1. In an apparatus for measuring the specific force and angular rotation rate of a moving body, a micromachined silicon structure comprising:

a) a monolithic silicon substrate having first and second substantially planar surfaces disposed substantially parallel to each other;

b) a first accelerometer formed of said substrate and having a first force sensing axis for producing a first output signal indicative of the acceleration of the moving body along said first force sensing axis, said first accelerometer having a first proof mass, a first support frame, and first flexure means for connecting said first proof mass to said first support frame;

c) a second accelerometer formed of said substrate and having a second force sensing axis for producing a second output signal indicative of the acceleration of the moving body along said second force sensing axis, said second accelerometer having a second proof mass, a second support frame, and second flexure means for connecting said second proof mass to said second support frame; and

d) mounting means formed of said substrate for mounting said first and second accelerometers to be moved along a vibration axis substantially parallel to said first and second planar surfaces;

wherein dithering of said first and second accelerometers along said vibration axis permits measurement of said specific force and angular rotation rate of said moving body.

2. The measuring apparatus as claimed in claim 1, wherein said first and second flexure means respectively comprise first and second pairs of flexures.

3. The measuring apparatus as claimed in claim 2, wherein each flexure of said first and second pairs of flexures is an "S-bend" flexure.

4. The measuring apparatus as claimed in claim 1, wherein said first force sensing axis extends in a direction opposite to that of said second sensing axis.

5. In an apparatus for measuring the specific force and angular rotation rate of a moving body, a micromachined silicon structure comprising:

a) a monolithic silicon substrate having first and second substantially planar surfaces disposed substantially parallel to each other;

b) a first accelerometer formed of said substrate and having a first force sensing axis for producing a first output signal indicative of the acceleration of the moving body along said first force sensing axis, said first accelerometer having a first proof mass, a first support frame, and first flexure means for connecting said first proof mass to said first support frame;

c) a second accelerometer formed of said substrate and having a second force sensing axis for producing a second output signal indicative of the acceleration of the moving body along said second force sensing axis, said second accelerometer having a second proof mass, a second support frame, and second flexure means for connecting said second proof mass to said second support frame;

d) a dither frame formed of said substrate; and

e) a first pair of S-bend flexures connected between said first support frame and said dither frame, and a second pair of S-bend flexures connected between said second support frame and said dither frame, said first and second pairs of S-bend flexures being formed of said substrate for mounting said first and second accelerometers such that said first and second force sensing axes are both oriented at the same angle with respect to said first and second surfaces and such that said first and second accelerometers can be moved along a vibration axis perpendicular to each of said first and second sensing axes;

wherein dithering of said first and second accelerometers along said vibration axis permits measurement of said specific force and angular rotation rate of said moving body.

6. The measuring apparatus as claimed in claim 5, wherein said first and second flexure means respectively comprise first and second pairs of flexures.

7. The measuring apparatus as claimed in claim 6, wherein each flexure of said first and second pairs of flexures is an "S-bend" flexure.

8. The measuring apparatus as claimed in claim 5, wherein said first force sensing axis extends in a direction opposite to that of said second force sensing axis.

9. In an apparatus for measuring the specific force and angular rotation rate of a moving body, a micromachined silicon structure comprising:

a) a monolithic silicon substrate having first and second substantially planar surfaces disposed substantially parallel to each other;

b) an accelerometer formed of said substrate and having a force sensing axis for producing an output signal indicative of the acceleration of the moving body along said force sensing axis, said accelerometer comprising an accelerometer frame, a proof mass, and hinge means interconnected between said accelerometer frame and said proof mass for rotating said proof mass about a hinge axis when the moving body is subjected to a force along said force sensing axis; and

c) mounting means formed of said substrate for mounting said accelerometer such that said accelerometer can be moved along a vibration axis perpendicular to said force sensing axis;

wherein dithering said accelerometer along one of said vibration axis or said force sensing axis enables measurement of said specific force and angular rotation rate of said moving body.

10. The measuring apparatus as claimed in claim 9, wherein said proof mass has a first end interconnected by said hinge means to said frame and a free end permitted to rotate freely about said hinge axis with respect to said frame.

11. The measuring, apparatus as claimed in claim 10, wherein said proof mass includes a center of gravity and a pendulous axis aligned to intersect said center of gravity and said hinge axis, and there is further included flexible means interconnected between said frame and said free end of said proof mass for flexibly restraining the pivoting of said proof mass about said pendulous axis.

12. The measuring apparatus as claimed in claim 11, wherein said accelerometer frame has an external periphery of substantially rectangular configuration including first and third opposing peripheral edges and second and fourth opposing peripheral edges, said mounting means comprising a mounting frame having an inner periphery of substantially rectangular configuration including first and third opposing, inner peripheral edges and second and fourth opposing, inner peripheral edges, and at least one flexure having a first end affixed to said third inner peripheral edge of said mounting frame and a second end connected to said second external peripheral edge of said accelerometer frame, said flexure extending at rest along a path substantially parallel to said second and fourth inner peripheral edges of said mounting frame and being aligned with said second, external peripheral edge of said accelerometer frame, said accelerometer frame having a cut away portion such that the unrestricted length of said flexure is selected to impart an "S-bend" flexure thereto.

13. In an apparatus for measuring the specific force and angular rotation rate of a moving body, a micromachined silicon structure comprising:

a) a monolithic silicon substrate having first and second substantially planar surfaces disposed substantially parallel to each other;

b) first and second accelerometers formed of said substrate, each of said accelerometers having a force sensing axis for producing a first output signal indicative of the acceleration of the moving body along said force sensing axis, each of said accelerometers further having an accelerometer frame, a proof mass, and hinge means interconnected between said frame and said proof mass for allowing said proof mass to rotate about a hinge axis when the moving body is subjected to a force along said force sensing axis, said proof mass having a first end interconnected by said hinge means to said frame and a free end permitted to rotate freely about said hinge axis with respect to said frame, said proof mass further having a center of gravity and a pendulous axis aligned to intersect said center of gravity and said hinge axis, flexible means interconnected between said frame and said free end of said proof mass for flexibly restraining the pivoting of said proof mass about said pendulous axis, and a dither frame;

said structure further comprising flexure means for connecting the accelerometer frame of each of said first and accelerometers to said dither frame;

said flexure means being generally compliant to allow dithering of said first and second accelerometers along a dither axis, said dither axis being generally perpendicular to said force sensing axes of said first and second accelerometers;

wherein dithering of said first and second accelerometers along said dither axis enables measuring said force and angular rotation rate of said moving body.

14. The measuring apparatus as claimed in claim 13, wherein said flexure means respectively comprise first and second pairs of flexures.

15. The measuring apparatus as claimed in claim 14, wherein each flexure of said first and second pairs of flexures is an "S-bend" flexure.

16. The measuring apparatus as claimed in claim 13, wherein respective force sensing axes of said accelerometers extend in opposite directions.

17. A combined angular rate and acceleration sensor comprising a structure formed from a substantially planar, monolithic body having first and second major surfaces, said structure having an outer frame portion disposed around first and second inner frame portions, each of said inner frame portions being disposed around an associated proof mass and connected thereto through a plurality of flexures, said structure further comprising drive means interposed between said first and second inner frame portions for imparting a dithering motion to said first and second proof masses, said first and second inner frame portions being connected to said outer frame portion through a plurality of suspensory flexures.

18. A combined angular rate and acceleration sensor comprising:

a first accelerometer and a second accelerometer each formed from a substantially planar body comprised of monocrystalline silicon, said planar body having first and second oppositely disposed major surfaces, each of said accelerometers including a first frame and a proof mass suspended from said first frame by first flexures, each of said accelerometers having an associated sensitive axis and an associated rate axis that is orthogonally disposed to said sensitive axis;

a second frame that is disposed about each of said first frames, each of said first frames being connected to said second frame by second flexures;

means for sensing a displacement of each of said proof masses; and

means for dithering each of said proof masses along a dither axis that is disposed perpendicularly to said rate axis.

19. A combined angular rate and acceleration sensor as claimed in claim 18, wherein said first and second flexures respectively comprise first and second pairs of flexures.

20. A combined angular rate acceleration sensor comprising:

a first accelerometer and a second accelerometer each formed from a substantially planar body comprised of monocrystalline silicon, said planar body having first and second oppositely disposed major surfaces, each of said accelerometers including a first frame and a proof mass suspended from said first frame by hinges and flexible connectors, each of said accelerometers having an associated sensitive axis and an associated rate axis that is orthogonally disposed to said sensitive axis;

a second frame that is disposed about each of said first frames, each of said first flames being connected to said second frame by flexures;

means for sensing a displacement of each of said proof masses; and

means for dithering each said proof masses along a dither axis that is disposed perpendicularly to said rate axis.

21. A combined angular rate and acceleration sensor as claimed in claim 20, wherein said flexures comprise pairs of flexures.

22. A combined angular rate and acceleration sensor as claimed in claim 21, wherein said pair of flexures comprise S-bend flexures and said flexible connectors comprise S-bend flexures.