Method of remanufacturing an engine block
US-2016297039-A1 · Oct 13, 2016 · US
US10933496B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10933496-B2 |
| Application number | US-201816159992-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 15, 2018 |
| Priority date | Oct 15, 2018 |
| Publication date | Mar 2, 2021 |
| Grant date | Mar 2, 2021 |
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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.
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.
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