Repair of cast iron bore inner diameter surfaces

US10933496B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10933496-B2
Application numberUS-201816159992-A
CountryUS
Kind codeB2
Filing dateOct 15, 2018
Priority dateOct 15, 2018
Publication dateMar 2, 2021
Grant dateMar 2, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A method for repairing a worn portion in an inner diameter surface of a bore of a cast iron part is disclosed. The inner diameter surface of the bore may have an original surface geometry prior to wear. The method may comprise forming a crescent-shaped pocket in the inner diameter surface of the bore to remove the worn portion, installing an insert in the crescent-shaped pocket, and post-machining the insert to form a crescent-shaped insert that is flush with the original surface geometry of the bore inner surface diameter.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for repairing a worn portion on an inner diameter surface of a bore of a cast iron housing of a high-pressure gear pump, the inner diameter surface of the bore having an original surface geometry prior to wear, the method comprising: forming a crescent-shaped pocket in the inner diameter surface of the bore to remove the worn portion, the inner diameter surface of the bore extending along a longitudinal direction; forming a plurality of inner ribs in the crescent-shaped pocket, a peak of each rib of the plurality of inner ribs extending circumferentially about the crescent-shaped pocket, adjacent ribs of the plurality of inner ribs being distributed along the longitudinal direction; installing an insert in the crescent-shaped pocket; and post-machining the insert so that an inner diameter surface of the insert corresponds to the original surface geometry of the bore inner diameter surface, wherein an outer surface of the insert includes a plurality of outer ribs, and wherein installing the insert in the crescent-shaped pocket includes interleaving the plurality of inner ribs with the plurality of outer ribs, such that the plurality of inner ribs overlaps with the plurality of outer ribs along a radial direction, the radial direction being transverse to the longitudinal direction. 2. The method of claim 1 , wherein post-machining the insert comprises machining the insert to a crescent-shaped insert, and wherein the crescent-shaped insert has an inner diameter surface that corresponds to the original surface geometry of the bore inner diameter surface. 3. The method of claim 1 , wherein the insert is half-moon shaped prior to post-machining the insert. 4. The method of claim 1 , wherein installing the insert comprises bonding the insert to the crescent-shaped pocket using an epoxy adhesive. 5. The method of claim 1 , wherein installing the insert comprises bonding the insert to the crescent-shaped pocket by brazing. 6. The method of claim 1 , wherein interleaving the plurality of inner ribs with the plurality of outer ribs forms a box joint. 7. The method of claim 1 , wherein interleaving the plurality of inner ribs with the plurality of outer ribs forms a dovetail joint. 8. The method of claim 1 , wherein forming the crescent-shaped pocket comprises machining the crescent-shaped pocket in the inner diameter surface using a slot-style cutter. 9. The method of claim 1 , wherein the insert is formed from a cast iron alloy. 10. A method for repairing a worn portion on an inner diameter surface of a bore of a high-pressure gear pump, the bore being formed in a cast iron housing of the high-pressure gear pump and being configured to receive a gear, the inner diameter surface of the bore having an original surface geometry prior to wear, the method comprising: forming a crescent-shaped pocket in the inner diameter surface of the bore to remove the worn portion, the inner diameter surface of the bore extending along a longitudinal direction, the crescent-shaped pocket spanning about 90 degrees to about 120 degrees circumferentially around the inner diameter surface of the bore; forming a plurality of inner ribs in the crescent-shaped pocket, a peak of each rib of the plurality of inner ribs extending circumferentially about the crescent-shaped pocket, adjacent ribs of the plurality of inner ribs being distributed along the longitudinal direction, installing an insert in the crescent-shaped pocket; and post-machining the insert into a crescent-shaped insert, the crescent-shaped insert having an inner diameter surface that corresponds to the original surface geometry of the bore inner diameter surface, wherein an outer surface of the insert includes a plurality of outer ribs, and wherein installing the insert in the crescent-shaped pocket includes interleaving the plurality of inner ribs with the plurality of outer ribs, such that the plurality of inner ribs overlaps with the plurality of outer ribs along a radial direction, the radial direction being transverse to the longitudinal direction. 11. The method of claim 10 , further comprising blending the crescent-shaped insert with surrounding areas of the bore inner diameter surface. 12. The method of claim 10 , further comprising forming the insert prior to installing the insert by cutting the insert from a cylindrical shaft such that the insert is half-moon shaped. 13. The method of claim 10 , wherein the insert is formed from a cast iron alloy. 14. The method of claim 10 , wherein installing the insert comprises bonding the insert to a bore wall defining the crescent-shaped pocket using an epoxy adhesive. 15. The method of claim 14 , wherein interleaving the plurality of inner ribs with the plurality of outer ribs forms a box joint. 16. The method of claim 14 , wherein interleaving the plurality of inner ribs with the plurality of outer ribs forms a dovetail joint. 17. The method of claim 10 , wherein the housing of the high-pressure gear pump includes an inlet and an outlet, and wherein the worn portion in the inner diameter surface of the bore is oriented closer to the inlet than the outlet. 18. A method for repairing a worn portion in an inner diameter surface of a bore of a cast iron part, the inner diameter surface of the bore having an original surface geometry prior to wear, the method comprising: forming a crescent-shaped pocket in the inner diameter surface of the bore to remove the worn portion, the inner diameter surface of the bore extending along a longitudinal direction; forming a plurality of inner ribs in the crescent-shaped pocket, a peak of each rib of the plurality of inner ribs extending circumferentially about the crescent-shaped pocket, adjacent ribs of the plurality of inner ribs being distributed along the longitudinal direction; installing a half-moon shaped insert in the crescent-shaped pocket; and post-machining the half-moon shaped insert to form a crescent-shaped insert that is flush with the original surface geometry of the bore inner diameter surface, wherein an outer surface of the half-moon shaped insert includes a plurality of outer ribs, and wherein installing the half-moon shaped insert in the crescent-shaped pocket includes interleaving the plurality of inner ribs with the plurality of outer ribs, such that the plurality of inner ribs overlaps with the plurality of outer ribs along a radial direction, the radial direction being transverse to the longitudinal direction. 19. The method of claim 18 , wherein installing the half-moon shaped insert comprises bonding the half-moon shaped insert to a bore wall defining the crescent-shaped pocket using an epoxy adhesive. 20. The method of claim 18 , wherein interleaving the plurality of inner ribs with the plurality of outer ribs forms one of a box joint and a dovetail joint.

Assignees

Inventors

Classifications

  • Repairing methods · CPC title

  • Outer members for co-operation with rotary pistons; Casings (casings for rotary engines or machines in general F16M) · CPC title

  • with similar tooth forms (F04C2/16 takes precedence) · CPC title

  • B23P6/02Primary

    Pistons or cylinders · CPC title

  • Repairing fractures or cracked metal parts or products, e.g. castings · CPC title

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What does patent US10933496B2 cover?
A method for repairing a worn portion in an inner diameter surface of a bore of a cast iron part is disclosed. The inner diameter surface of the bore may have an original surface geometry prior to wear. The method may comprise forming a crescent-shaped pocket in the inner diameter surface of the bore to remove the worn portion, installing an insert in the crescent-shaped pocket, and post-machin…
Who is the assignee on this patent?
Caterpillar Inc
What technology area does this patent fall under?
Primary CPC classification B23P6/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Mar 02 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).