Hydrodynamic bearing for use in an electric motor and an electric motor having the hydrodynamic bearing

• US 6,066,903 A
• Filed: 03/15/1999
• Issued: 05/23/2000
• Est. Priority Date: 03/16/1998
• Status: Expired due to Fees

• Current Assignee: Nidec Corporation
• Original Assignee: Nidec Corporation
• Inventors: Ichiyama, Yoshikazu
• Primary Examiner(s): Ramirez, Nestor
• Assistant Examiner(s): LE, DANG D
• Application Number:
  US09/267,621
• Time in Patent Office: 435 Days
• Field of Search: 310/90, 57/133, 384/93, 384/107, 384/133, 384/193, 384/226, 384/227, 384/228, 384/234, 384/238, 384/241, 384/271, 384/272, 384/290, 384/291, 384/375, 384/376, 384/381, 384/95, 384/263 , 384/378, 384/100, 384/111, 384/112, 384/113, 384/115, 384/118, 384/120
• US Class Current: 310/90
• CPC Class Codes: F16C 17/107 with at least one surface for radial load and at least one surface for axial load
• CPC Class Codes: F16C 2370/12 Hard disk drives or the like
• CPC Class Codes: F16C 33/745 by capillary action
• CPC Class Codes: H02K 5/1677 radially supporting the rotor around a fixed spindle; radially supporting the rotor directly

Abstract

A spindle motor includes a stationary shaft and a rotor. A thrust bearing, a first radial bearing and a second radial bearing are defined between the shaft and rotor. A first annular air gap is established between the thrust bearing and the first radial bearing. A second annular air gap is established between the first radial bearing and the second radial bearing. The first annular air gap is able to vent to outside of the spindle motor via a breathing bore formed in a thrust plate of a stationary shaft. The second annular air gap is able to vent to outside the spindle motor only while the rotor is rotating about the shaft.

Claims

1. A hydrodynamic bearing device for rotatably supporting a rotor on a stationary shaft, the stationary shaft having a shaft portion and a disk-shaped thrust plate, the shaft portion extending from a base to a distal end thereof, the thrust plate formed on a portion of the shaft portion proximate the distal end, the rotor having a recess defining thrust surfaces and having first and second journal portions, the first and second journal portion having inner radial surfaces facing outer radial surfaces of the shaft portion, the thrust surfaces axially facing upper and lower surfaces of the thrust plate, and said hydrodynamic bearing device comprising:

a thrust bearing defined at axial faces of the thrust plate of the stationary shaft and the thrust surfaces of the rotor, lubricant being disposed between the thrust plate and the thrust surfaces of the rotor;

a first radial bearing defined at the first journal portion of the rotor and adjacent surfaces of the shaft portion, lubricant being disposed between the surface of the first journal portion and the adjacent surfaces of the shaft portion;

a second radial bearing defined at the second journal portion of the rotor and adjacent surfaces of the shaft portion, lubricant being disposed between the surface of the second journal and the adjacent surfaces of the shaft portion, said first and second radial bearings being axially spaced apart from one another;

a first tapered seal and a second tapered seal defined at first and second sides of said first radial bearing for retaining lubricant in said first radial bearing, a first oil separating gap defined between said first radial bearing and said thrust bearing, said first oil separating gap being filled with gas separating lubricant in said thrust bearing and lubricant in said first radial bearing;

a third tapered seal and a fourth tapered seal defined on first and second sides of said second radial bearing, respectively, for retaining lubricant in said second radial bearing, a second oil separating gap being defined between said first radial bearing and said second radial bearing, said second oil separating gap being filled with gas for separating lubricant in said first radial bearing and lubricant in said second radial bearing, said second tapered seal and said third tapered seal being adjacent to one another;

means for connecting said second oil separating gap to the outside of said hydrodynamic bearing device during rotation of the rotor, said second tapered seal provided with an axial length such that an interface of the lubricant defined by a meniscus at said second radial bearing is located adjacent to said second side of said first radial bearing;

wherein

said axial length of said second tapered seal relative to the shaft portion is shorter than an axial lenght of said third tapered seal and is shorter than an axial length of said fourth tapered seal portion;

each of said first, second, third and fourth tapered scale defines a corresponding gap, each of said corresponding gaps having a radial width larger than a radial width of a gap defined between the surfaces of the first journal portion and the adjacent surfaces of the shalt portion, and larger than a radial width of a gap defined between the surfaces of the second journal portion and the adjacent surfaces of the shaft portion;

said second tapered seal is tapered such that a corresponding surface of the shaft portion defining said second tapered seal is inclined having an axial length shorter than a radial length thereof and extending radially inward in a direction toward said second radial bearing; and

said third tapered seal is partially defined by a surface of the shaft portion which extends radially inward toward said second tape red seal and has an axial length larger than a radial length thereof.

2. The hydrodynamic bearing device as set forth in claim 1, wherein the second journal of the rotor is formed with a means for urging a lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of the rotor.

3. The hydrodynamic bearing device as set forth in claim 1, wherein said means for connecting said second oil separating gap to outside said hydrodynamic bearing device during rotation of the rotor is restricted by the lubricant with the rotor being stationary with respect to the shaft portion.

4. The hydrodynamic bearing device as set forth in claim 3, further comprising a means for urging lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of the rotor, wherein

said means for connecting said second oil separating gap to outside said hydrodynamic bearing device during rotation of the rotor comprises a bore formed in said shaft connected to a first opening and a second opening formed in the shaft portion, said first opening being open to said second oil separating gap and said second opening being adjacent to said fourth tapered seal,

said second opening of said bore being covered with lubricant with the rotor in a stationary position with respect to the shaft portion, said second opening being open to the outside of said hydrodynamic bearing device in response to rotation of the rotor with respect to the shaft portion and operation of said means for urging lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of the rotor.

5. The hydrodynamic bearing device as set forth in claim 1, wherein

said first radial bearing generates dynamic pressure in the lubricant such that the lubricant is urged toward said thrust bearing in response to rotation of the rotor.

6. The hydrodynamic bearing device as set forth in claim 1, further comprising

a lubricant retaining means for retaining lubricant moving from said second side of said second radial bearing, said lubricant retaining means being formed adjacent to said second side of said second radial bearing.

7. The hydrodynamic bearing device as set forth in claim 6, wherein

said lubricant retaining means comprises an annular recess formed on the shaft portion adjacent to said second side of said second radial bearing and adjacent to said fourth tapered seal, and the rotor is similarly formed with a protrusion which extends into said recess.

8. The hydrodynamic bearing device as set forth in claim 6, wherein

said lubricant retaining means comprises an annular recess formed on the rotor adjacent to said fourth taper seal, said annular recess having a first tapered surface and a second tapered surface, said first tapered surface being closer to said fourth taper seal than said second tapered surface, said first tapered surface having an axial length shorter than an axial length of said second tapered surface.

9. The hydrodynamic bearing device as set forth in claim 1, further comprising

a breathing bore formed on an inner peripheral end of the stationary shaft for connecting said first oil separating gap to the outside of said hydrodynamic bearing device.

10. A hydrodynamic bearing device for rotatably supporting a rotor on a stationary shaft, the stationary shaft having a shaft portion and a disk-shaped thrust plate, the shaft portion extending from a base side to a distal end thereof, the thrust plate formed proximate the distal end of the shaft portion, the rotor having a journal portion and thrust surfaces, the journal portion having an inner peripheral surface radially facing an outer radial surface of the shaft portion, the thrust surfaces axially facing upper and lower surfaces of the thrust plate, and said hydrodynamic bearing device comprising:

thrust bearing defined by said thrust surfaces, upper and lower surfaces of said thrust plate and lubricant retained therebetween;

a first radial bearing and a second radial bearing axially spaced apart from one another, each having lubricant retained between the shaft portion and the journal portion of the rotor defining said first and second radial bearings, an air gap interposing between said first radial bearing and said second radial bearing;

said thrust bearings being formed with dynamic pressure generating gooves, and said first and second radial bearings being formed with dynamic pressure generating grooves for generating hydraulic forces in said lubricant in response to rotation of said rotor;

said gap being fild with air so as to separate the lubricant retained in the first and second radial bearings, said gap being formed by an upper inclined surface extending away from said first radial bearing and a lower inclined surface extending away from said second radial bearing, said upper inclined surface having an axial length that is shorter than an axial length of said lower inclined surface such that a meniscus between said lubricant retained in said first radial bearing and the air within said gap is located adjacent to an axially lower end portion of said dynamic pressure generating grooves of said first radial bearing;

wherein, said meniscus moves in response to upward movement of said lubricant in said first radial bearing thereby exposing said axially lower portion of said dynamic pressure generating grooves of said first radial bearing to the air within said gap thereby causing a reduction in further upward movement of said lubricant caused by said axially lower portion of said dynamic pressure generating grooves of said first radial bearing; and

means for connecting said gap between said first and second radial bearings to outside of said hydrodynamic bearing device during rotation of the rotor.

11. The hydrodynamic bearing device as set forth in claim 10, wherein

said means for connecting is open in response to rotation of the rotor and is closed with the rotor being stationary with respect to the shaft portion.

12. The hydrodynamic bearing device as set forth in claim 11, further comprising

a means for urging lubricant in said second radial bearing towards said first radial bearing in response to rotation of the rotor, wherein

said means for connecting is a bore formed in the shaft portion having a first opening and a second opening, said first opening being open to said gap between said first radial bearing and said second radial bearing and said second opening being open to base side of said second radial bearing;

and

said second opening of said bore being covered with lubricant with the rotor in a stationary position with respect to said shaft portion, said bore being connected to outside the hydrodynamic bearing device in response to rotation of the rotor as said means for urging lubricant draws the lubricant towards said first radial bearing to expose said second opening.

13. A spindle motor comprising:

a stationary shaft having a shaft portion and a disk-shaped thrust plate fixed thereto, said shaft portion extending from the base to the distal end thereof, and said thrust plate formed proximate the distal end of said shaft portion, said shaft portion being further formed with a first and second radial bearing surfaces;

a rotor having first and second journal portions and a recess which defines thrust surfaces, said first and second journal portions having inner radial surfaces facing corresponding outer radial surfaces of said shaft portion, and said thrust surfaces axially facing upper and lower surfaces of said thrust plate, said thrust surfaces and said thrust plate defining a thrust bearing, said first journal portion and said first radial bearing surface define a first radial bearing, and said second journal portion and said second radial bearing surface define a second radial bearing;

a first tapered seal and a second tapered seal arc defined at first and second sides of said first radial bearing for retaining lubricant in said first radial bearing, said first tapered seal having a first oil separating gap filled with gas separating lubricant in said thrust bearing and lubricant in said first radial bearing;

a third tapered seal and a fourth tapered seal defined on first and second sides of said radial bearing, respectively, for retaining lubricant in said second radial bearing, said third tapered seal having a second oil separating gap filled with gas for separating lubricant in said first radial bearing and lubricant in said second radial bearing, aid second tapered seal and said third tapered seal being adjacent to one another;

means for connecting said second oil separating gap to outside said spindle motor during rotation of the rotor; and

wherein;

said second tapered seal has an axial length, relative to said shaft portion, which is shorter than an axial length of said third tapered seal and is shorter than an axial length of said fourth tapered seal portion;

each of said first, second, third and fourth tapered seals defines a corresponding gap, each of said corresponding gaps having a radial width larger than a radial width of a gap defined between surfaces of said first journal portion and said first radial bearing surfaces of said shaft portion, and larger than a radial width of a gap defined between surfaces of said second journal portion and said second radial bearing surfaces of said shaft portion;

said second tapered seal is tapered such that a corresponding surfaces of said shaft portion defining said second tapered seal is inclined radially inward having an axial length shorter than a radial length thereof and extends radially inward in a direction toward said second radial bearing; and

said third tapered seal is partially defined by a surface of said shaft portion which extends radially inward toward said second tapered seal and said surface an axial length larger than a radial length thereof.

14. The spindle motor as set forth in claim 13, further comprising means for connecting said first oil separating gap to outside said spindle motor.

15. The spindle motor as set forth in claim 14, wherein said means for connecting said first oil separating gap to outside said spindle motor comprises a passage formed in said thrust plate.

16. The spindle motor as set forth in claim 13, wherein, said second tapered seal has an axial length which is relatively short such that an interface of the lubricant defined by a meniscus at said second radial bearing is located adjacent to said second side of said first radial bearing.

17. The spindle motor as set forth in claim 13, wherein said second tapered seal has an axial length, relative to said shaft portion, which is shorter than an axial length of said third tapered seal and is shorter than an axial length of said fourth tapered seal portion.

18. The spindle motor as set forth in claim 17, wherein each of said first, second, third and fourth tapered seals defines a corresponding gap, each of said corresponding gaps having a radial width larger than a radial width of a gap defined between surfaces of said first journal portion and said first radial bearing surfaces of said shaft portion, and larger than a radial width of a gap defined between surfaces of said second journal portion and said second radial bearing surfaces of said shaft portion;

said second tapered seal is tapered such that a corresponding surface of said shaft portion defining said second tapered seal is inclined radially inward having an axial length shorter than its radial length and extends radially inward in a direction toward said second radial bearing; and

said third tapered seal is partially defined by a surface of said shaft portion which extends radially inward toward said second tapered seal and has an axial length larger than its axial length.

19. The spindle motor as set forth in claim 13, wherein said second journal of said rotor is formed with a means for urging lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of said rotor.

20. The spindle motor as set forth in claim 13, wherein said means for connecting said second oil separating gap to outside said spindle motor during rotation of said rotor is restricted by the lubricant with said rotor being stationary with respect to said shaft portion.

21. The spindle motor as set forth in claim 20, further comprising a means for urging lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of said rotor, wherein

said means for connecting said second oil separating gap to outside said spindle motor during rotation of said rotor comprises a bore formed in said shaft connected to a first opening and a second opening formed in said shaft, said first opening being open to said second oil separating gap and said second opening being adjacent to said fourth tapered seal,

said second opening of said bore being covered with lubricant with said rotor in a stationary position with respect to the shaft, said second opening being open to the outside of the spindle motor in response to rotation of said rotor with respect to the shaft and operation of said means for urging lubricant in said second bearing radial bearing toward said first radial bearing in response to rotation of said rotor.

22. The spindle motor as set forth in claim 13, wherein said first radial bearing generates dynamic pressure in the lubricant such that the lubricant is urged toward said thrust bearing in response to rotation of the rotor.

23. The spindle motor as set forth in claim 13, further comprising a lubricant retaining means for retaining lubricant moving from said second side of said second radial bearing, said lubricant retaining means being formed adjacent to said second side of said second radial bearing.

24. The spindle motor as set forth in claim 23, wherein said lubricant retaining means comprises an annular recess formed on said shaft portion adjacent to said second side of said second radial bearing and adjacent to said fourth tapered seal, and said rotor is similarly formed with a protrusion which extends into said recess.

25. The spindle motor as set forth in claim 23, wherein said lubricant retaining means comprises an annular recess formed on said rotor adjacent to said fourth taper seal, said annular recess having a first tapered surface and a second tapered surface, said first tapered surface being closer to said fourth taper seal than said second tapered surface, said first tapered surface having an axial length shorter than an axial length of said second tapered surface.

26. The spindle motor as set forth in claim 13, further comprising a breathing bore formed on an inner peripheral end of said shaft portion for connecting said first oil separating gap to outside said spindle motor.

27. A hydrodynamic bearing device comprising:

a stationary shaft formed upper and lower journal surfaces;

a rotor disposed about said stationary shaft, said rotor being formed with first and second journal portions, said first and second journal portions having inner radial surfaces facing said upper and lower journal surfaces, respectively, of said stationary shaft;

a first radial bearing defined at said first journal portion of said rotor and said upper journal surface of said shaft portion, lubricant being disposed between said first journal portion and said upper journal surface of said shaft portion, and at least one of said first radial surface and said upper journal surface being formed with dynamic pressure generating grooves;

a second radial bearing defined at said second journal portion of said rotor and said lower journal surface of said shaft portion, lubricant being disposed between said second journal portion and said lower journal surface of said shaft portion;

a first tapered seal and a second tapered seal defined at first and second sides of said first radial bearing for retaining lubricant in said first radial bearing;

a third tapered seal and a fourth tapered seal defined on first and second sides of said second radial bearing, respectively, for retaining lubricant in said second radial bearing, an oil separating gap being defined between said first radial bearing and said second radial bearing, said oil separating gap being filled with gas for separating lubricant in said first radial bearing and lubricant in said second radial bearing;

a means for connecting said oil separating gap to the outside of said hydrodynamic bearing device in response to rotation of the rotor, said second tapered seal provided with length such that a meniscus on the lubricant defined at said second radial bearing is located adjacent to said second side of said first radial bearing;

the axial length of said second tapered seal relative to said shaft portion is shorter than an axial length of said third tapered seal and is shorter than an axial length of said fourth tapered seal portion, said second tapered seal being tapered such that a corresponding surface of said shaft portion defining said second tapered seal is inclined radially inward having an axial length shorter than a radial length thereof and extending radially inward in, a direction toward said second radial bearing; and

the inclination of said second tapered seal is such that in response to upward movement of lubricant in said upper radial bearing, said second tapered seal allows upward movement of the lubricant thereby exposing a lower portion of said dynamic pressure generating grooves in said upper radial bearings thereby reducing upward movement of the lubricant.

28. The hydrodynamic bearing device as set forth in claim 27, wherein:

each of said first, second, third and fourth tapered seals defines a corresponding gap, each of said corresponding gaps having a radial width, larger than a radial width of a gap defined between said first journal portion and said upper journal surface, and each of said corresponding gaps has a radial width that is larger than a radial width of a gap defined between said second journal portion and said lower journal surface; and

said third tapered seal is partially defined by a surface of the shaft portion which extends radially inward toward said second tapered seal and has an axial length larger than a radial length thereof.

29. The hydrodynamic bearing device as set forth in claim 27, wherein said oil separating gap is located between said second and third tapered seals.

30. The hydrodynamic bearing device as set forth in claim 29, wherein:

said second radial bearing is formed with herringbone grooves that are configured to urge lubricant in the second radial bearing upward toward said second oil separating gap in response to rotation of said rotor;

said shaft portion is formed with an opening that is open to said oil separating gap, and said opening is open to a lower portion of said herringbone grooves of said second radial bearing; and

said means for connecting said second oil separating gap to the outside of said hydrodynamic bearing device comprises said opening and said herringbone grooves in said second radial bearing.

31. A hydrodynamic bearing device for rotatably supporting a rotor on a stationary shaft, the hydrodynamic bearing device comprising:

the shall having a shaft portion and a disk-shaped thrust plate formed on the shaft portion,

the rotor having thrust surfaces facing upper and lower surfaces of the thrust plate to form thrust bearings with lubricant being retained between the surfaces of the thrust plate and the rotor, the rotor further having a sleeve portion surrounding the shaft portion to form upper and lower radial bearings, dynamic pressure generating grooves being formed on at least one of the shaft portion and the sleeve portion at each of the upper and lower radial bearings,

the upper and lower radial bearing being axially separated from each other by an air separating gap, said air separating gap being at least partially defined by an upper tapered surface and a lower tapered surface formed on the shaft portion,

wherein a portion of said air separating gap between the shaft portion and the sleeve portion at said upper tapered surface increases in a downward direction, and a portion of said intermediate air separating gap between the shaft portion and the sleeve portion at said lower tapered surface decreases in the downward direction, said upper tapered surface being shorter in axial length than an axial length of said lower tapered surface, lubricant being retained at each of the upper and lower radial bearings with gas being filled in said air separating gap thereby separating the lubricant of the upper radial bearing from the lubricant in the lower radial bearings, a meniscus on the surface of the lubricant in the upper radial bearing exposed to said air separating gap being moveable from said upper tapered surface into the upper radial bearing in response to rotation of the rotor about the shaft thereby exposing the dynamic pressure generating grooves in the upper radial bearing thereby suppressing further movement of the meniscus.

32. The hydrodynamic bearing device as set forth in claim 31, wherein said upper tapered surface has an axial length relative to the shaft shorter than a radial length thereof.

33. The hydrodynamic bearing device as set forth in claim 32, wherein said axial length of said upper tapered surface is shorter than an axial length of said lower tapered surface.

34. The hydrodynamic bearing device as set forth in claim 33, wherein said lower tapered surface has an axial length long than a radial length of said lower tapered surface.