Fabrication means for in-hub spindle with separate fluid dynamic bearings

• US 6,148,501 A
• Filed: 04/14/1998
• Issued: 11/21/2000
• Est. Priority Date: 04/14/1998
• Status: Expired due to Term

• Current Assignee: Seagate Technology LLC (Seagate Technology Holdings Plc)
• Original Assignee: Seagate Technology LLC (Seagate Technology Holdings Plc)
• Inventors: Byl, Marten, Parsoneault, Norbert, Leuthold, Hans, Shumway, Matt L., Grantz, Alan Lyndon, Addy, Roger Allen, Wolff, Etoli
• Primary Examiner(s): Bryant, David P.
• Assistant Examiner(s): Omgba, Essama
• Application Number:
  US09/060,030
• Time in Patent Office: 952 Days
• Field of Search: 29/603.03, 29/593, 29/596, 29/407.01, 29/898.07, 29/898.09
• US Class Current: 29/603.03
• CPC Class Codes: F16C 17/105 with at least one bearing surface providing angular contact, e.g. conical or spherical bearing surfaces
• CPC Class Codes: F16C 2370/12 Hard disk drives or the like
• CPC Class Codes: F16C 33/107 Grooves for generating pressure
• CPC Class Codes: F16C 43/02 Assembling sliding-contact bearings
• CPC Class Codes: G11B 19/2018 Incorporating means for passive damping of vibration, either in the turntable, motor or mounting
• CPC Class Codes: H02K 15/14 Casings; Enclosures; Supports
• CPC Class Codes: H02K 15/16 Centering rotors within the stator; Balancing rotors
• CPC Class Codes: Y10T 29/49009 Dynamoelectric machine
• CPC Class Codes: Y10T 29/49025 Making disc drive
• CPC Class Codes: Y10T 29/49696 Mounting
• CPC Class Codes: Y10T 29/497 Pre-usage process, e.g., preloading, aligning
• CPC Class Codes: Y10T 29/49764 with testing or indicating

Abstract

A method of fabricating a spindle hub assembly (90) including precision machining critical surfaces of the hub components (60, 33) that mount onto a spindle shaft (30) and accurately locate the critical surfaces for positioning of bearing cones (35, 36) on the shaft in spaced relationship of bearing seats (34) on the hub (60, 33) to ensure stable rotation of the hub on the shaft.

Claims

1. A method of fabricating a spindle assembly that includes the following components:

a two piece hub, each piece of the hub defining one of two opposing bearing surfaces of a conical hydrodynamic bearing, a shaft, first and second opposed bearing cones each having a second bearing surface of the conical hydrodynamic bearing, and a stator assembly, comprising the steps of

(a) mounting the stator assembly onto the shaft,

(b) inserting the shaft through an opening in a first piece of the two-piece hub,

(c) positioning the second piece of the two piece hub onto the shaft opposite the stator assembly from the first piece so that the stator assembly is enclosed within the hub and the one surface of each conical hydrodynamic bearing is located at opposite ends of the hub and surrounding the shaft,

(d) securing together the first and second pieces of the hub, after executing steps (a), (b), (c), and (d), then

(e) securely positioning the first bearing cone about the shaft, and then

(f) progressively positioning the second bearing cone along the shaft toward the first bearing cone until the gaps between the bearing surfaces of the bearing cone and the hub are within a preselected tolerance.

2. The method of claim 1 wherein,

step (d) is performed first by precision machining critical surfaces of the hub in a single set-up process to ensure accurate location of the critical surfaces with respect to each other.

3. The method of claim 2 wherein,

the two pieces of the hub are mounted together at their respective critical surfaces.

4. The method of claim 2 wherein,

the critical surfaces also include surfaces that engage surfaces of the shaft and bearing cone, and wherein all critical surfaces of the hub components are precision machined in one set-up process.

5. The method of claim 1 wherein,

steps (e) and (f) include press fitting the bearing cones onto the shaft.

6. The method of claim 1 wherein,

step (d) includes joining the first and second hub pieces by means of an interference fit.

7. The method of claim 1 wherein,

step (f) is performed by measuring, by means of an air gauge, air flow through the gaps in order to determine the width of the gaps.

8. The method of claim 1 wherein,

step (f) is performed by measuring the axial play between the shaft and the hub.

9. A method of fabricating a spindle assembly that includes the following components:

a two piece hub, each piece of the hub defining one of two opposing bearing surfaces of a conical hydrodvnamic bearing, a shaft, first and second opposed bearing cones each having a second bearing surface of the conical hydrodynamic bearing, and a stator assembly, comprising the steps of

(a) first precision machining critical surfaces of the pieces of the hub where the two pieces are joined and where the hub engages the shaft and the bearing cones in one set up process to ensure accurate location of the critical surfaces, and thereafter

(b) mounting the stator assembly onto the shaft,

(b) inserting the shaft through an opening in a first piece of the two-piece hub,

(c) positioning the second piece of the two piece hub onto the shaft opposite the stator assembly from the first piece so that the stator assembly is enclosed within the hub and critical surfaces of each hub piece engage each other,

(d) securing together the first and second pieces of the hub and the one surface of each conical hydrodynamic bearing is located at opposite ends of the hub and surrounding the shaft, after executing steps (a), (b), (c) and (d), then

(e) securely positioning the first bearing cone about the shaft, and

(f) thereafter progressively positioning the second bearing cone along the shaft toward the first bearing cone until the gaps between the bearing surfaces of the bearing cone and the hub are within a preselected tolerance.

10. The method of claim 9 and further comprising the step of

machining the bearing cones so that their cone angles are greater than the desired cone angle once the bearing cones are secured onto the shaft.

11. The method of claim 10 wherein

the cone angles are machined to approximately 30.04°

, so that once bearing cones are secured onto the shaft, the cone angle becomes 30.00°

.

12. The method of claim 9 wherein,

steps (e) and (f) include press fitting the bearing cones onto the shaft.

13. The method of claim 9 wherein,

step (d) includes joining the first and second hub pieces by means of an interference fit.

14. The method of claim 9 wherein,

step (f) is performed by measuring, by means of an air gauge, air flow through the gaps in order to determine the width of the gaps.

15. The method of claim 9 wherein,

step (f) is performed by measuring the axial play between the shaft and the hub.

16. The method of claim 9 and further comprising the step of

precision machining the inside diameter and outside diameter of the bearing cones on one set-up to insure accurate angular alignment.

17. A method of fabricating a spindle assembly that includes the following components:

a two piece hub, each piece of the hub defining one of two opposing bearing surfaces of a conical hydrodynamic bearing, a shaft, first and second opposed bearing cones each having a second bearing surface of the conical hydrodynamic bearing, and a stator assembly, comprising

(a) mounting the stator assembly onto the shaft,

(b) inserting the shaft through an opening in a first piece of the two-piece hub,

(c) positioning the second piece of the two piece hub onto the shaft opposite the stator assembly from the first piece so that the stator assembly is enclosed within the hub, and the one surface of each conical hydrodynamic bearing is located at opposite ends of the hub and surrounding the shaft,

(d) a step for securing together the first and second pieces of the hub,

(e) a step for securing the first bearing cone about the shaft, and after completing steps (a)-(e), then

(f) a step for progressively positioning the second bearing cone along the shaft toward the first bearing cone until the gaps between the bearing surfaces of the bearing cone and the hub are within a preselected tolerance.

18. The method of claim 17 wherein,

steps (e) and (f) include press fitting the bearing cones onto the shaft.

19. The method of claim 17 wherein,

step (d) includes joining the first and second hub pieces by means of an interference fit.

20. The method of claim 17 wherein,

step (f) is performed by measuring, by means of an air gauge, air flow through the gaps in order to determine the width of the gaps.