Micro-scale and meso-scale hydraulically or pneumatically powered devices capable of rotational motion

• US 8,382,423 B1
• Filed: 07/07/2008
• Issued: 02/26/2013
• Est. Priority Date: 12/03/2001
• Status: Active Grant

• Current Assignee: Microfabrica Incorporated (Technoprobe S.P.A.)
• Original Assignee: Microfabrica Incorporated (Technoprobe S.P.A.)
• Inventors: Frodis, Uri, Cohen, Adam L., Lockard, Michael S.
• Primary Examiner(s): White, Dwayne J
• Application Number:
  US12/168,787
• Time in Patent Office: 1,695 Days
• Field of Search: 415/904, 415/83, 415/84, 415/85, 415/86, 415/87, 415/903, 433/131, 433/132, 433/103, 433/120, 606/180, 606/170
• US Class Current: 415/83
• CPC Class Codes: A61B 17/22012 in direct contact with, or very close to, the obstruction or concrement for removing obstructions in blood vessels by laser A61B18/245
• CPC Class Codes: A61B 17/32002 with continuously rotating, oscillating or reciprocating cutting instruments
• CPC Class Codes: A61B 17/3201 Scissors for biopsy A61B10/02
• CPC Class Codes: A61B 17/320758 with a rotating cutting instrument, e.g. motor driven A61B17/320725, A61B17/32075 and A61B17/320783 take precedence; for removing intra-ocular material A61F9/00763; endoscopic rotatable cutting instruments A61B17/32002
• CPC Class Codes: A61B 2017/00345 Micromachines, nanomachines, microsystems
• CPC Class Codes: A61B 2017/00526 Methods of manufacturing
• CPC Class Codes: A61B 2017/00539 hydraulically
• CPC Class Codes: A61B 2017/00544 pneumatically
• CPC Class Codes: A61B 2017/00553 using a turbine
• CPC Class Codes: A61B 2017/320775 Morcellators, impeller or propeller like means

Abstract

Embodiments are directed to micro-scale or meso-scale devices having hydraulic or pneumatic actuation mechanisms incorporating bearings elements (such as ball bearings, cylindrical bearings, interference bearings, or hydrostatic bearings. Devices of some embodiments are turbines. Some devices may function as medical devices. Other embodiments are directed to multi-layer, multi-material electrochemical fabrication methods for producing such devices.

Claims

1. A device capable of converting a flow of a fluid into rotational mechanical motion, comprising:

a. a stator;

b. a rotor capable of rotational motion relative to the stator, wherein the rotational motion occurs about a rotational axis;

c. a plurality of bearing elements positioned between the rotor and stator to hold the rotor and the stator in desired relative positions;

d. an inlet in said stator for receiving a fluid and an outlet in said stator for removing fluid;

wherein at least a portion of the stator and the rotor are formed using a multi-layer, multi-material electrochemical fabrication process, and

wherein at least one bearing element is located within a slot in the rotor and a slot in the stator.

2. The device of claim 1 wherein the slot in the rotor faces radially outward and the slot in the stator faces radially inward.

4. The device of claim 1 wherein the slot in the rotor faces axially upward and the slot in the stator faces radially downward.

5. The device of claim 4 wherein at least two rotor slots and at least two stator slots exist wherein the two rotor slots face in opposite directions and the two stator slots face in opposite directions.

3. The device of claim wherein the slot in the rotor faces radially inward and the slot in the stator faces radially outward.

6. A method for fabricating a rotary device, comprising:

a. forming at least a portion of a stator and a rotor from a plurality of adhered layers of material wherein the stator comprises a stator bearing surface, wherein the rotor comprises a rotor bearing surface, and wherein the forming of each layer of material comprises,

i. depositing at least a first material;

ii. depositing at least a second material; and

iii. planarizing the first and second materials to a common level;

b. removing at least a portion of the first or second material after formation of the plurality of layers;

c. supplying a plurality of bearing elements;

d. inserting the bearing elements into an opening between the stator bearing surface and the rotor bearing surface.

7. The method of claim 6 wherein bearing elements are inserted after formation of the stator and rotor are completed.

8. The method of claim 6 additionally comprising:

a. forming at least one additional layer to complete formation of the stator and the rotor after inserting the bearing elements, wherein the forming of the at least one additional layer comprises;

i. depositing at least a first material;

ii. depositing at least a second material; and

iii. planarizing the first and second materials to a common level; and

b. removing least a portion of the first or second material after formation of the at least one additional layer.

9. The method of claim 6 wherein the stator and the rotor are formed in substantially assembled positions relative to each other.

10. The method of claim 6 wherein the stator and the rotor are formed separately from one another and are thereafter inserted into assembled positions and bearing elements are inserted.

11. The method of claim 6 wherein the forming of the plurality of adhered layers comprises forming lower portions of the stator and rotor in assembled positions forming upper portions of the stator and rotor in assembled positions but laterally spaced from the lower portions and upside down relative to the lower portions and wherein the method additionally comprises removing sacrificial material from inside a gap region on the lower portions intended to receive bearing elements and a gap region on the upper portions intended to receiving bearing elements, applying bearing elements into at least one of the gap region in the lower portion or in the upper portion and then bring a mating surface of the lower portion and a mating surface of the upper portion into desired relative positions and affixing the lower portions and upper portions together.

12. The method of claim 11 wherein the affixing occurs via a bonding material.

13. The method of claim 11 wherein the affixing occurs via one or more catches formed along with one or both of the lower portion and the upper portion.

14. A method for fabricating a rotary device, comprising:

a. forming at least a portion of a stator, a rotor, and a plurality of bearing elements from a plurality of adhered layers of material wherein the stator comprises a stator bearing surface including a plurality of protrusions separated by indentations, wherein the rotor comprises a rotor bearing surface including a plurality of protrusions separated by indentations, and wherein the bearing elements comprise an outer surface including a plurality of protrusions separated by indentations, and wherein the forming of each layer of material comprises;

i. depositing at least a first material;

ii. depositing at least a second material; and

iii. planarizing the first and second materials to a common level;

b. removing least a portion of the first or second material after formation of the plurality of layers; and

c. supplying a plurality of bearing elements, and

wherein during formation, at least some protrusions on the stator bearing surface and on the rotor bearing surface align with indentations on the outer surface of the bearing elements and wherein at least some indentations on the rotor bearing surface and on the stator bearing surface align with protrusions on the outer surface of the bearing elements, such that gaps between the bearing elements and the rotor and stator surfaces on any given layer are larger than a minimum feature size but wherein on at least some adjacent layers, gaps are substantially less than the minimum feature size.