Magnetically levitated high-speed spindle for shaping irregular surfaces

• US 7,264,430 B2
• Filed: 02/24/2005
• Issued: 09/04/2007
• Est. Priority Date: 02/26/2004
• Status: Expired due to Fees

• Current Assignee: Federal-Mogul Worldwide Incorporated (Apollo Global Management, Inc.)
• Original Assignee: Federal-Mogul Worldwide Incorporated (Apollo Global Management, Inc.)
• Inventors: Zdeblick, William J., Bischof, Kenneth R.
• Primary Examiner(s): Carter; Monica
• Assistant Examiner(s): Addisu; Sara
• Application Number:
  US11/065,618
• Publication Number:
  US 20050188798A1
• Time in Patent Office: 922 Days
• Field of Search: 409/231, 409/186, 409/193, 409/135, 408/147, 82/11.1, 821/58, 82 12- 15, 310/90.5
• US Class Current: 409/231
• CPC Class Codes: B23B 2260/0045 Two elements adjustable relative to each other in three mutually perpendicular directions
• CPC Class Codes: B23B 2270/38 Using magnetic fields magnets B23B2260/10
• CPC Class Codes: B23B 2270/58 Oblique elements
• CPC Class Codes: B23B 5/36 for turning specially-shaped surfaces by making use of relative movement of the tool and work produced by geometrical mechanisms, i.e. forming-lathes
• CPC Class Codes: B23Q 1/4876 a single sliding pair followed parallelly by a single rotating pair
• CPC Class Codes: B23Q 5/10 driven essentially by electrical means
• CPC Class Codes: F16C 2322/39 General build up of machine tools, e.g. spindles, slides, actuators in general B23Q
• CPC Class Codes: F16C 32/0489 with active support of five degrees of freedom, e.g. two radial magnetic bearings combined with an axial bearing
• CPC Class Codes: Y10T 408/85 to move radially
• CPC Class Codes: Y10T 409/309352 Cutter spindle or spindle support
• CPC Class Codes: Y10T 82/10 Process of turning
• CPC Class Codes: Y10T 82/122 Forming non-circular bore

Abstract

A magnetically levitated high-speed spindle assembly (20) is provided for forming non-circular holes (22) in workpieces (24) or non-circular surfaces on pins. The non-circular holes (22) can be formed with dimensionally varying axial trajectories at high speeds and with great accuracy. This is accomplished by supporting a rotating spindle (26) between first (58) and second (60) magnetic bearing clusters and independently controlling these bearing clusters (58, 60) to move a shaping tool (32) at the end of the spindle (26) in a predetermined orbital path (B). A multiple input-multiple output control strategy is used to control spindle (26) movements in the X and Y axes. The tilt angle between the cutting edge (34) of the shaping tool (32) and the orbital path (B) is maintained perpendicular under this multiple input-multiple output control of the magnetic bearing clusters (58, 60) to further improve shaping precision and spindle (26) stability during high-speed operations.

Claims

1. A magnetically levitated high-speed spindle assembly for forming a non-circular surface in a workpiece, said assembly comprising:

an elongated spindle extending along an ax al axis between a rear end and a shaping end;

a shaping tool extending radially outwardly front said spindle adjacent said shaping end and terminating in a point-like cutting edge;

a first magnetic bearing cluster supporting said spindle proximate said shaping end for magnetically levitated rotation about said axial axis;

a second magnetic bearing cluster spaced from said first magnetic bearing cluster and supporting said spindle remote from said shaping end for magnetically levitated rotation about said axial axis;

a radial bearing controller for independently controlling said first and second magnetic bearing clusters to adjust the radial position of said axial axis during magnetically levitated rotation of said spindle and move said shaping end in a predetermined non-circular orbital path so that said cutting edge will form a correspondingly shaped non-circular hole in the workpiece; and

a cutting edge controller for maintaining a continuous tilt angle between said cutting edge and said orbital path so that said cutting edge remains in continued contact with the workpiece while said shaping end of said spindle traverses said orbital path, wherein said tilt angle comprises an optimal cutting angle defined by the angle between a radius extending from said axial axis to said cutting edge and a tangent line to any point along said orbital path whereby the non-circular hole can be shaped by said cutting edge with improved precision and said assembly can operate at higher rotational speeds and with greater spindle stability.

2. The assembly of claim 1 wherein said tilt angle is a substantially right angle.

3. The assembly of claim 1 wherein said orbital path is an irregular shape.

4. The assembly of claim 1 wherein said first magnetic bearing cluster includes at least three magnet stators spaced in generally equal arcuate increments in a common plane about said axial axis.

5. The assembly of claim 4 further including at least three first position sensors spaced in generally equal arcuate increments in a common plane about said axial axis proximate to said at least three magnet stators of slid first magnetic bearing cluster.

6. The assembly of claim 5 wherein said second magnetic bearing cluster includes at least three magnet stators spaced in generally equal arcuate increments in a common plane about said axial axis.

7. The assembly of claim 6 further including at least three second position sensors spaced in generally equal arcuate increments in a common plane about said axial axis proximate to said at least three magnet stators of said second magnetic bearing cluster.

8. The assembly of claim 1 wherein said first magnetic bearing cluster includes a pair of opposing X-coordinate magnet stators and a pair of opposing Y-coordinate magnet stators, said X-coordinate magnet stators spaced between and generally co-planar with said Y-coordinate magnet stators.

9. The assembly of claim 8 wherein said radial bearing controller includes a pair of opposing X-coordinate position sensors adjacent to said pair of opposing X-coordinate magnet stators of said first magnetic bearing cluster, and a pair of opposing Y-coordinate position sensors adjacent to said pair of opposing Y-coordinate magnet stators of said first magnetic bearing cluster.

10. The assembly of claim 9 wherein said first magnetic bearing cluster includes a first rotor disposed on a first region of said spindle within said common plane formed between corresponding said X-coordinate and Y-coordinate magnet stators.

11. The assembly of claim 10 wherein said second magnetic bearing cluster includes a pair of opposing X-coordinate magnet stators and a pair of opposing Y-coordinate magnet stators, said X-coordinate magnet stators spaced between and generally co-planar with said opposing Y-coordinate magnet stators.

12. The assembly of claim 11 wherein said radial bearing controller includes a pair of opposing X-coordinate position sensors adjacent to said pair of opposing X-coordinate magnet stators of said second magnetic bearing cluster, and a pair of opposing Y-coordinate position sensors adjacent to said pair of opposing, Y-coordinate magnet stators of said second magnetic bearing cluster.

13. The assembly of claim 12 wherein said second magnetic bearing cluster includes a second rotor disposed on a second region of said spindle within said common plane formed between said corresponding X-coordinate and Y-coordinate magnet stators.

14. The assembly of claim 11 wherein said radial bearing controller includes a variable current generator for varying the supply of current to each of said pair of X-coordinate magnets of said first bearing cluster in non-linearly proportional increments.

15. The assembly of claim 1 further including a rotary position sensor for determining the angular position of said shaping tool about said axial axis.

16. The assembly of claim 15 wherein said shaping tool completes one revolution about said axial axis simultaneously with shaping end completing one lap around said orbital path.

17. The assembly of claim 1 further including an axial motion controller for moving said shaping tool relative to the workpiece along said axial axis while simultaneously varying the shape of said orbital path whereby a non-circular hole of continuously axially varying trajectory can be formed in the workpiece at high speeds and with great accuracy.

18. The assembly of claim 17 wherein said axial motion controller includes a workpiece holder.

19. The assembly of claim 1 further including a housing.

20. The assembly of claim 19 further including a magnetic thrust bearing associated with said spindle for limiting axial movement of said spindle relative to said housing.

21. The assembly of claim 19 further including a drive motor disposed within said housing for forcibly rotating said spindle about said axial axis.

22. The assembly of claim 19 wherein said housing includes at least two auxiliary bearings.

23. A method for magnetically levitating a high-speed spindle assembly for forming a non-circular hole in a work piece, said method comprising the steps of:

forming a cutting edge on a shaping tool;

affixing the shaping tool to one end of a spindle having an axial axis such that the cutting edge is positioned radially outwardly from the axial axis;

establishing a magnetic levitation field about a first region of the spindle proximate the shaping tool for rotation about the axial axis;

establishing a magnetic levitation field about a second region of the spindle spaced from the first region and remote from the shaping tool;

rotating the spindle within the first and second magnetic levitation fields about the axial axis;

adjusting the radial position of the axial axis at the first and second regions during rotation of the spindle by varying the first and second magnetic levitation fields to thereby move the cutting edge in a predetermined non-circular orbital path to form the non-circular hole in the workpiece;

and maintaining a continuous tilt angle between the cutting edge and the orbital path so that the cutting edge remains in continued contact with the workpiece while traversing the orbital path, wherein the tilt angle comprises an optimal cutting angle defined by the angle between a radius extending from the axial axis to the cutting edge and a tangent line to any point along the non-circular orbital path whereby the non-circular hole can be shaped by the cutting edge with improved precision and the spindle can operate at higher rotational speeds and with greater stability.

24. The method of claim 23 wherein step of maintaining a continuous tilt angle includes maintaining the tilt angle at a substantially) right angle.

25. The assembly of claim 23 further including the step of directing the orbital path in an irregular shape.

26. The method of claim 23 further including the step of determining the instantaneous angular position of the shaping tool about the axial axis during said step of forming the hole.

27. The method of claim 26 further including the step of timing the angular speed of the shaping tool so that the shaping tool completes one revolution about the axial axis simultaneously with the shaping end completing one lap around the orbital path.

28. The method of claim 23 further including the step of forming a hole of irregular and axially varying trajectory in the workpiece by moving the shaping tool relative to a workpiece along the axial axis simultaneously with said step of adjusting the radial position of the axial axis at the first and second regions.

29. The method of claim 28 wherein said step of moving the shaping tool relative to the workpiece includes moving the workpiece while maintaining the spindle axially fixed.

30. The method of claim 23 wherein said step of establishing a magnetic levitation field about the first region of the spindle includes positioning at least three magnet stators spaced in generally equal arcuate increment;

in a common plane about the axial axis.

31. The method of claim 30 wherein said step of establishing a magnetic levitation field about the second region of the spindle includes positioning at least three magnet stators in generally equal arcuate increments in a common plane about the axial axis.

32. The method of claim 31 wherein the step of adjusting the radial position of the axial axis at the first and second regions includes spacing at least three first position sensors in generally equal arcuate increments in a common plane about the axial axis proximate to the at least three magnet stators the first region, and spacing at least three first position sensors in generally equal arcuate increments in a common plane about the axial axis proximate to the at least three magnet stators the second region.

33. The method of claim 23 wherein said step of establishing a magnetic levitation field about the first region of the spindle includes positioning a pair of opposing X-coordinate magnet stators and a pair of opposing Y-coordinate magnet stators, and spacing the X-coordinate magnet stators between and generally co-planar with the Y-coordinate magnet stators.

34. The method of claim 33 wherein said step of establishing a magnetic levitation field about the second region of the spindle includes positioning a pair of opposing X-coordinate magnet stators and a pair of opposing Y-coordinate magnet stators, and spacing the X-coordinate magnet stators between and generally co-planar with the Y-coordinate magnet stators.

35. The method of claim 34 further including the step of varying the supply of current to each of the pair of X-coordinate magnets of said first bearing cluster in non-linearly proportional increments.

36. The method of claim 34 wherein the step of adjusting the radial position of the axial axis at the first and second regions includes fixing a position sensor adjacent to each of said magnet stators.