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US4651402A
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Method of making an assembly of a metal bearing ring and a solid or hollow cylindrical metal part, and an assembly so obtained
Assignee: EUROPEENNE POUR LA DEFENSE DE 1'INVENTION ET de la CREATION Ste
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Filing: 1984-04-19
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Granted: 1987-03-24
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Expires: 2004-04-19
Abstract
Abstract The cylinder may be an aircraft landing gear axle. The items may be pick- to sense axle deformation. A ring (30) for supporting the pick-ups is made of highly resilient material. It is initially of such a size that its cylinder-engaging surface overlaps the cylindrical surface it is to engage. The ring is then deformed by urging at least two points (34 to 37) around its circumference to increase the degree of overlap. While maintaining the deforming force on the ring, its cylinder-engaging surface (31) is machined so that there is no longer any overlap, and still maintaining the force, the ring is engaged with the cylinder. The force is then removed. The said points move resiliently away from the cylinder, but intermediate points are consequently resiliently urged into contact with the cylinder. The contact is smooth and progressive, thus avoiding the kind of stress concentrations that could reduce cylinder life by fatigue, etc.
Inventors
- 👤 Georges Bonfils
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 05:40
CPC Classifications
G; G01; G01G; G01G19/00; G01G19/02; G01G19/07; B; B23; B23P; B23P11/00; B23P15/00; B23P15/003; B64; B64D; B64D45/00; B64D2045/008; Y; Y10; Y10S; Y10S384/00; Y10S384/90; Y10S384/912; Y10T; Y10T29/00; Y10T29/49; Y10T29/49636; Y10T29/49643; Y10T29/49647; Y10T29/49668; Y10T29/49826; Y10T29/49863; Y10T29/49876; Y10T83/00; Y10T83/04; Y10T83/0405; Y10T83/0419; Y10T83/0424; Y10T83/0429
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
231 words
A method of making an assembly of a metal bearing ring and a cylindrical metal part for supporting an item inside a hollow metal cylindrical part on said bearing ring or outside a solid or hollow cylindrical metal part, said method comprising the following steps: providing a bearing ring of highly resilient metal having a cylinder-engaging surface of a diameter that overlaps the diameter of the corresponding ring-engaging surface of the metal cylindrical part; applying localized forces to at least two circumferentially spaced points on the ring to locally, elastically deform the ring such that said overlap increases at said points; machining the deformed cylindrical part-engaging surface of the ring while applying said localized forces thereto during and after said machining so that there is no overlap between the diameter thereof and the diameter of the corresponding ring-engaging surface of the cylindrical part; engaging the machined metal ring against the metal cylindrical part while still applying said localized forces thereto; and removing the applied localized forces; whereby, before machining, a first set of exterior localized forces produces a series of elastic deformations at certain points to said ring, and after machining and after assembly, a second set of localized internal forces tends to produce a series of elastic deformations at other points on said ring, and wherein said second set of localized internal forces ensure the deformation holding of the assembly.
Claim 2
Independent Claim
231 words
A method of making an assembly of a metal bearing ring and a cylindrical metal part for supporting an item inside a hollow metal cylindrical part on said bearing ring or outside a solid or hollow cylindrical metal part, said method comprising the following steps: providing a bearing ring of highly resilient metal having a cylinder-engaging surface of a diameter that overlaps the diameter of the corresponding ring-engaging surface of the metal cylindrical part; applying localized forces to at least two circumferentially spaced points on the ring to locally, elastically deform the ring such that said overlap increases at said points; machining the deformed cylindrical part-engaging surface of the ring while applying said localized forces thereto during and after said machining so that there is no overlap between the diameter thereof and the diameter of the corresponding ring-engaging surface of the cylindrical part; engaging the machined metal ring against the metal cylindrical part while still applying said localized forces thereto; and removing the applied localized forces; whereby, before machining, a first set of exterior localized forces produces a series of elastic deformations at certain points to said ring, and after machining and after assembly, a second set of localized internal forces tends to produce a series of elastic deformations at other points on said ring, and wherein said second set of localized internal forces ensure the deformation holding of the assembly.
Claim 3
Dependent Claim
17 words
A method according to claim 1, wherein the said ring is made in a single, closed piece.
Claim 4
Dependent Claim
16 words
A method according to claim 1, wherein said ring is slotted to form an open piece.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-23 | 1990-09-22 | 1991-03-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-23 | 1994-09-22 | 1995-03-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-23 | 1998-09-22 | 1999-03-24 | $7700.00 | Window Closed / Lapsed |