Composite bearing structure

• US 5,675,201 A
• Filed: 08/24/1994
• Issued: 10/07/1997
• Est. Priority Date: 01/08/1993
• Status: Expired due to Term

• Current Assignee: Sumitomo Electric Industries Limited (Sumitomo Corporation)
• Original Assignee: Sumitomo Electric Industries Limited (Sumitomo Corporation)
• Inventors: Katayama, Tetsuya, Komura, Osamu, Matsunuma, Kenji, Yamakawa, Akira, Higuchi, Matsuo, Yasuoka, Norio, Miyake, Masaya
• Primary Examiner(s): LaBalle, Clayton E.
• Application Number:
  US08/295,623
• Time in Patent Office: 1,140 Days
• Field of Search: 310/90, 310/905, 384/100, 384/107, 384/112
• US Class Current: 310/90.5
• 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 32/0402 combined with other supporting means, e.g. hybrid bearings with both magnetic and fluid supporting means
• CPC Class Codes: F16C 32/0427 for axial load mainly
• CPC Class Codes: F16C 32/0431 with bearings for axial load combined with bearings for radial load
• CPC Class Codes: F16C 33/1015 Pressure generating grooves
• CPC Class Codes: F16C 33/107 Grooves for generating pressure
• CPC Class Codes: F16C 39/063 Permanent magnets

Abstract

A composite bearing structure that has a high rotational accuracy and that can withstand high-speed rotation comprises first bearing means, second bearing means, third bearing means and fourth bearing means. The first bearing means supports a radial impact force which is applied to a rotator during rotation, and is formed by an inner ring (1) and an outer ring (2) consisting of silicon nitride ceramics sintered bodies. The second bearing means supports an axial load which is applied to the rotator while maintaining a prescribed clearance with the rotator, and is formed by a magnetic bearing body of two permanent magnets (12) and (13) which are thrust-directionally opposed to each other. The third bearing means maintains the radial rotational accuracy of the rotator, and is formed by a radial dynamic pressure producing groove (5) which is formed in a cylindrical surface of the inner ring (1). The fourth bearing means maintains the thrust-directional rotational accuracy of the rotator, and is formed by an air dome portion (100) which is confined in a semi-closed state by the inner ring (1), the outer ring (2) and a cover (4).

Claims

1. A composite bearing structure for supporting a rotator that is adapted to rotate at a high speed, said composite bearing structure comprising:

first bearing means (1,

     2) including a ceramics sintered body for supporting a radial impact force that is applied to said rotator during rotation thereof;

second bearing means for supporting an axial load that is applied to said rotator while maintaining a prescribed clearance of said second bearing means and said rotator;

third bearing means for maintaining a radial rotational accuracy of said rotator; and

fourth bearing means for maintaining a thrust-directional rotational accuracy of said rotator.

2. The composite bearing structure in accordance with claim 1, wherein said ceramics sintered body includes a silicon nitride ceramics sintered body.

3. The composite bearing structure in accordance with claim 2, wherein said silicon nitride ceramics sintered body includes silicon nitride containing crystal grains with a linear density of at least 35 grains per length of 30 μ

m with a grain boundary phase volume ratio of not more than 15 volume %, and containing pores having a maximum diameter of not more than 20 μ

m, the content of said pores being not more than 3%.

4. The composite bearing structure in accordance with claim 1, wherein said second bearing means includes dynamic gas pressure bearing means (6) for supporting said axial load by a gas pressure produced by rotation of said rotator.

5. The composite bearing structure in accordance with claim 4, wherein said dynamic gas pressure bearing means includes a rotating member (2) rotating with said rotator, and a fixed member (3) arranged opposite said rotating member with said clearance maintained axially therebetween.

6. The composite bearing structure in accordance with claim 5, wherein said rotating member and said fixed member include ceramics sintered bodies, and wherein at least one of said rotating member and said fixed member has a groove (6) therein for introducing a gas into said clearance for producing said gas pressure.

7. The composite bearing structure in accordance with claim 1, wherein said second bearing means includes magnetic bearing means (12, 13;

10, 17;

15,

     16) for supporting said axial load through magnetic attraction or repulsion.

8. The composite bearing structure in accordance with claim 7, wherein said magnetic bearing means includes a rotating member (2) rotating with said rotator, and a fixed member (3;

13) arranged opposite said rotating member with said clearance maintained axially therebetween.

9. The composite bearing structure in accordance with claim 8, wherein said rotating member and said fixed member include magnets (12, 13;

10, 17;

15,

     16) for producing said magnetic attraction or repulsion in said clearance.

10. The composite bearing structure in accordance with claim 1, wherein said third bearing means includes a ceramics sintered body for maintaining said radial rotational accuracy while maintaining a prescribed second clearance of said third bearing means and said rotator.

11. The composite bearing structure in accordance with claim 1, wherein said third bearing means includes dynamic gas pressure bearing means (5) for maintaining said rotational accuracy by a gas pressure produced by rotation of said rotator.

12. The composite bearing structure in accordance with claim 11, wherein said dynamic gas pressure bearing means includes a rotating member (2, 4) rotating with said rotator, and a fixed member (1) arranged opposite said rotating member with a radial clearance therebetween.

13. The composite bearing structure in accordance with claim 12, wherein said rotating member and said fixed member include ceramics sintered bodies, and wherein at least one of said rotating member and said fixed member has a groove (5) therein for introducing a gas into said radial clearance for producing said gas pressure.

14. The composite bearing structure in accordance with claim 1, wherein said third bearing means includes magnetic bearing means (8, 10, 11;

7, 8, 9, 10;

7, 8, 14,

     15) for maintaining said rotational accuracy through magnetic attraction or repulsion while maintaining a prescribed second clearance of said third bearing means and said rotator.

15. The composite bearing structure in accordance with claim 14, wherein said magnetic bearing means includes a rotating member (2) rotating with said rotator, and a fixed member (1) arranged opposite said rotating member with said second clearance maintained radially therebetween.

16. The composite bearing structure in accordance with claim 15, wherein said rotating member and said fixed member include magnets (8, 10, 11;

7, 8, 9, 10;

7, 8, 14,

     15) for producing said magnetic attraction or repulsion in said second clearance.

17. The composite bearing structure in accordance with claim 16, wherein said rotating member and said fixed member consist of bodies including said ceramics sintered body, and wherein said magnets (11) are embedded in an interior of said bodies.

18. The composite bearing structure in accordance with claim 1, wherein said fourth bearing means includes a rotating member (4) rotating with said rotator, a fixed member (1) arranged at least axially opposite said rotating member, and a gas dome (100) confined in a semi-closed state between said rotating member and said fixed member.

19. The composite bearing structure in accordance with claim 18, wherein said rotating member includes a first rotating portion (2) that is arranged radially opposite said fixed member (1) with a second clearance radially therebetween, and a second rotating portion (4) that is arranged axially opposite said fixed member (1) with said gas dome (100) axially interposed therebetween, and that is fixed to said first rotating portion (2).

20. The composite bearing structure in accordance with claim 19, wherein said second bearing means includes dynamic gas pressure bearing means (6) that introduce a gas into said prescribed clearance by rotation of said rotator, for supporting said axial load by a gas pressure produced by said rotation of said rotator, and wherein said second rotating portion (4) has a hole (101) for discharging said gas introduced into said prescribed clearance by said dynamic gas pressure bearing means.

21. The composite bearing structure in accordance with claim 19, wherein said third bearing means includes dynamic gas pressure bearing means (5) that introduce a gas into said prescribed clearance by rotation of said rotator, for maintaining said rotational accuracy by a gas pressure produced by said rotation of said rotator,

and wherein said second rotating portion (4) has a hole (101) for discharging said gas introduced into said prescribed clearance by said dynamic gas pressure bearing means.

22. A composite bearing comprising:

a fixed member including a base plate and a cylindrical stub extending from said base plate;

a rotatable member including a cylindrical sleeve rotatably arranged coaxially and radially outwardly around said cylindrical stub and axially adjacent said base plate, and an axial end cover axially adjacent an axial end of said cylindrical stub opposite said base plate;

a radial impact supporting first bearing formed by said cylindrical sleeve rotatably arranged on said cylindrical stub, wherein at least one of said sleeve and said stub is a sintered ceramic body;

an axial load supporting second bearing that is arranged between said cylindrical sleeve and said base plate and that maintains therebetween an axial clearance during rotation of said rotatable member relative to said fixed member;

a radial rotational accuracy maintaining third bearing that is arranged between said cylindrical sleeve and said cylindrical stub and that maintains therebetween a radial clearance during rotation of said rotatable member relative to said fixed member; and

an axial rotational accuracy maintaining fourth bearing that is arranged between said axial end of said cylindrical stub and said axial end cover;

wherein said second bearing comprises at least one of a magnetic repulsion bearing and a dynamic gas pressure bearing, and said fourth bearing comprises a gas dome at least partially enclosed in a space formed between said axial end of said cylindrical stub, said axial end cover and an end portion of said cylindrical sleeve.

23. The composite bearing in accordance with claim 22, wherein said sintered ceramic body comprises silicon nitride containing crystal grains with a linear density of at least 50 grains per length of 30 μ

m and a grain boundary phase volume ratio of not more than 15 volume %, and containing pores having a maximum diameter of not more than 20 μ

m with a pore content of not more than 3%.