Microfabricated microengine with constant rotation rate

• US 5,955,801 A
• Filed: 12/01/1997
• Issued: 09/21/1999
• Est. Priority Date: 12/01/1997
• Status: Expired due to Term

• Current Assignee: National Technology & Engineering Solutions Of Sandia LLC (Honeywell International Inc.)
• Original Assignee: Sandia Corporation (Martin Marietta Corporation)
• Inventors: Dickey, Fred M., Romero, Louis A.
• Primary Examiner(s): Dougherty, Thomas M.
• Assistant Examiner(s): MULLINS, BURTON S
• Application Number:
  US08/982,098
• Time in Patent Office: 659 Days
• Field of Search: 310/309, 310/40 MM, 310/42, 310/45, 310/75 R, 310/83, 310/80, 310/37, 310/112, 427/128, 427/129, 427/130, 427/131, 427/132, 29/596, 29/598
• US Class Current: 310/40.0MM
• CPC Class Codes: F01C 1/082 Details specially related to intermeshing engagement type machines or engines
• CPC Class Codes: F01C 1/14 with toothed rotary pistons
• CPC Class Codes: F04C 2230/00 Manufacture
• CPC Class Codes: F16H 31/005 with pawls driven by a reciprocating or oscillating transmission member F16H31/002, F16H31/004 take precedence
• CPC Class Codes: H02K 99/20 Motors

Abstract

A microengine uses two synchronized linear actuators as a power source and converts oscillatory motion from the actuators into constant rotational motion via direct linkage connection to an output gear or wheel. The microengine provides output in the form of a continuously rotating output gear that is capable of delivering drive torque at a constant rotation to a micromechanism. The output gear can have gear teeth on its outer perimeter for directly contacting a micromechanism requiring mechanical power. The gear is retained by a retaining means which allows said gear to rotate freely. The microengine is microfabricated of polysilicon on one wafer using surface micromachining batch fabrication.

Claims

1. A microengine comprising:

a) a substrate base;

b) a mechanical output gear rotatably attached to said substrate base, said gear for providing direct rotational power to a micromechanism;

c) a first linear actuator formed on said substrate base, characterized by a mass M₁ and a spring constant k₁, and linked to said mechanical output gear near the outer perimeter thereof by a first linkage having a length l₁ ;

d) a second linear actuator formed on said substrate base, characterized by a mass M₂ and a spring constant k₂, and linked to said first linkage by a second linkage having a length l₂ at a point a distance d₁ from the connection between said first linkage and said first linear actuator;

e) wherein the mass M₂ is substantially equal to the mass M₁ divided by the square of the ratio of the distance d₁ to the length l₁ ; and

f) wherein the spring constant k₂ is substantially equal to the spring constant k₁ divided by the square of the ratio of the distance d₁ to the length l₁.

2. The microengine of claim 1, wherein said first linear actuator is driven with a first forcing function wherein the square of the forcing voltage is sinusoidal, and wherein said second linear actuator is driven with a second forcing function wherein the square of the forcing voltage plus a constant is sinusoidal.

3. The microengine of claim 1, wherein the first forcing function is shifted 90 degrees in phase from the second forcing function.

4. The microengine of claim 1, wherein said linear actuators are electrostatic comb drive actuators.

5. The microengine of claim 1, wherein said mechanical output gear comprises teeth at its outermost perimeter.

6. The microengine of claim 1, wherein said invention is fabricated of polysilicon on one wafer using surface micromachining batch fabrication.

7. The microengine of claim 1, wherein said linkage means is flexible to allow rotational motion at said mechanical output gear.

8. A microengine batch fabricated by polysilicon surface micromachining techniques comprising:

a) a mechanical output gear formed upon and rotatably attached to a substrate base;

b) a first linear actuator, responsive to a first drive function and characterized by a mass M₁ and a spring constant k₁, formed on said substrate base and positioned along an X axis relative to said output gear;

c) a second linear actuator, responsive to a second drive function and characterized by a mass M₂ and a spring constant k₂, formed on said substrate base and positioned along a Y axis, substantially orthogonal to the X axis, relative to said output gear and said first linear actuator wherein said second actuator is positioned between said output gear and said first linear actuator;

d) a first linkage means, having a length l₁, for rotatably linking said first linear actuator to said output gear, wherein said first linkage means is connected to said output gear near said output gear'"'"'s outer perimeter; and

e) a second linkage means, having a length l₂, for linking said second linear actuator to said first linkage means at a distance d₁ from said first linear actuator;

f) wherein the mass M₂ is substantially equal to the mass M₁ divided by the square of the ratio of the distance d₁ to the length l₁ ; and

g) wherein the spring constant k₂ is substantially equal to the spring constant k₁ divided by the square of the ratio of the distance d₁ to the length l₁.

9. The microengine of claim 8, wherein said first drive function comprises a first forcing function wherein the square of the forcing voltage is sinusoidal, and wherein said second drive function comprises a second forcing function wherein the square of the forcing voltage plus a constant is sinusoidal, and wherein the second drive function is 90 degrees out of phase with said first drive function.

10. The microengine of claim 8, wherein said actuators are electrostatic comb drive actuators.

11. The microengine of claim 8, wherein said mechanical output gear further comprises teeth on its outer perimeter, said teeth adapted for directly contacting a micromechanism.

12. The microengine of claim 8, wherein said microengine output gear is fabricated on a silicon substrate and is smaller than 40 micrometers in diameter.

13. The microengine of claim 8, wherein said first linkage means is flexible to allow rotational motion at said output mechanical gear.

14. A microfabricated microengine made of polysilicon on a silicon substrate base comprising:

a) a mechanical output gear having teeth on its outermost surface adapted for providing rotational motion to a mechanical load;

b) a retaining hub formed on and attached to said substrate base for rotatably securing said output gear and allowing the output gear to rotate;

c) a first linear actuator, responsive to a first drive function and characterized by a mass M₁ and a spring constant k₁, formed on said substrate base and positioned along an X axis relative to said output gear;

d) a second linear actuator, responsive to a second drive function and characterized by a mass M₂ and a spring constant k₂, formed on said substrate base and positioned along a Y axis, substantially orthogonal to the X axis, relative to said output gear wherein said second actuator is positioned between said output gear and said first linear actuator;

e) a first linkage means, having a length l₁, for rotatably linking said first linear actuator to said output gear, wherein said linkage is rotatably connected to said output gear near said output gear'"'"'s perimeter; and

f) a second linkage means, having a length l₂, for flexibly linking said second linear actuator to said first linkage means at a distance d₁ from said first linear actuator;

g) wherein the mass M₂ is substantially equal to the mass M₁ divided by the square of the ratio of the distance d₁ to the length l₁ ; and

h) wherein the spring constant k₂ is substantially equal to the spring constant k₁ divided by the square of the ratio of the distance d₁ to the length l₁.

15. The microfabricated microengine of claim 14, wherein said first drive function comprises a first forcing function wherein the square of the forcing voltage is sinusoidal, and wherein said second drive function comprises a second forcing function wherein the square of the forcing voltage plus a constant is sinusoidal.

16. The microfabricated microengine of claim 14, wherein said actuators are electrostatic comb drive actuators.

17. The microfabricated microengine of claim 14, wherein said linkage means is flexible to allow rotational motion at said mechanical output gear.

18. The microfabricated microengine of claim 14, wherein said mechanical output gear is retained by a retaining means which allows said mechanical output gear to rotate freely.

19. The microfabricated microengine of claim 14, wherein said mechanical output gear is smaller than 40 micrometers and said microengine is smaller than 9 micrometers in thickness.