Adhesion of thermal spray using compression technique

US10526996B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10526996-B2
Application numberUS-201615233254-A
CountryUS
Kind codeB2
Filing dateAug 10, 2016
Priority dateAug 10, 2016
Publication dateJan 7, 2020
Grant dateJan 7, 2020

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

An improved surface activation technique improves the adhesion of thermal spray coatings, which is useful for engine cylinder bores. The new method includes compressing the cylinder bore surface to create a surface profile on the surface, such as through rolling a roller along the surface. An engine block is also provided, which includes a plurality of cylinder bores, each cylinder bore having an inner surface, and each inner surface having a surface profile that includes a helical groove and other surface profiles formed in the inner surface. A thermal spray coating is formed on the inner surface of each cylinder bore, the thermal spray coating being adhered to the surface profile of the inner surface. A roller assembly for activating the surface is also provided.

First claim

Opening claim text (preview).

What is claimed is: 1. An engine block comprising: a plurality of cylinder bores, each cylinder bore having an inner surface, each inner surface having a compressed surface profile that includes a helical groove formed in the inner surface, wherein each cylinder bore surface comprises compressive residual stress having a magnitude of at least 250 MPa; and a thermal spray coating formed on the inner surface of each cylinder bore, the thermal spray coating being adhered to the surface profile of the inner surface. 2. The engine block of claim 1 , the surface profile of each inner surface further comprising a plurality of dimples formed in the inner surface. 3. An engine block comprising: a plurality of cylinder bores, each cylinder bore having an inner surface, each inner surface having a surface profile that includes a first helical groove formed in the inner surface, the first helical groove being defined by a first flank opposite a second flank with an angle defined between walls of the first and second flanks, the surface profile of each inner surface further comprising a second helical groove formed through the first flank of the first helical groove and a third helical groove formed through the second flank of the first helical groove, the surface profile of each inner surface further comprising a plurality of dimples formed in the inner surface, each of the helical grooves having a pitch in the range of about 150 to about 250 μm, the first helical groove having a depth of about 100 to about 250 μm, and each of the dimples having a diameter of about 20 to about 30 μm, the first and the second flanks defining an angle of about 60 to about 75 degrees therebetween; and a thermal spray coating formed on the surface of each cylinder bore, the thermal spray coating being adhered to the surface profile of the inner surface. 4. The engine block of claim 3 , wherein each cylinder bore surface comprises compressive residual stress having a magnitude of at least 250 MPa. 5. The engine block of claim 1 , wherein each cylinder bore includes a plurality of rough textures each having radii greater than 10 μm and developed interfacial area ratio (Sdr) greater than 100% to enhance coating adhesion. 6. The engine block of claim 4 , wherein the each of the inner surfaces of the cylinder bores is formed of aluminum. 7. The engine block of claim 4 , wherein each cylinder bore includes a plurality of rough textures each having radii greater than 10 μm and developed interfacial area ratio (Sdr) greater than 100% to enhance coating adhesion.

Assignees

Inventors

Classifications

  • Manufacturing · CPC title

  • C23C4/02Primary

    Pretreatment of the material to be coated, e.g. for coating on selected surface areas · CPC title

  • for grinding cylindrical surfaces internally (B24B5/40 takes precedence) · CPC title

  • Crankcases of V-engines · CPC title

  • Other cylinders · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US10526996B2 cover?
An improved surface activation technique improves the adhesion of thermal spray coatings, which is useful for engine cylinder bores. The new method includes compressing the cylinder bore surface to create a surface profile on the surface, such as through rolling a roller along the surface. An engine block is also provided, which includes a plurality of cylinder bores, each cylinder bore having …
Who is the assignee on this patent?
Gm Global Tech Operations Llc
What technology area does this patent fall under?
Primary CPC classification C23C4/02. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Jan 07 2020 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).