Method for manufacturing a metal component, metal component, and turbocharger

US2017370003A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2017370003-A1
Application numberUS-201615548107-A
CountryUS
Kind codeA1
Filing dateJan 21, 2016
Priority dateFeb 3, 2015
Publication dateDec 28, 2017
Grant date

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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 turbocharger compressor wheel with an aluminum proportion of at least 50 atom percent, produced by. etching a turbine wheel base body using an alkaline etchant to produce a specific etch pitting consisting of nano pores and micropores and chemical deposition of a nickel-phosphorous protective layer ( 19 ) onto the etched base body surface.

First claim

Opening claim text (preview).

1 . A method for manufacturing a compressor wheel ( 17 ) for a turbocharger ( 1 ), the compressor wheel ( 17 ) comprising a base body and a nickel-phosphorous protective coating, the method comprising the steps: etching the base body using an alkaline etchant to produce a specific etch pitting, wherein said specific etch pitting consists of nano etch pittings and micro etch pittings, wherein the nano etch pittings have a depth of 0.1 to 1.5 μm and micro etch pittings have a depth of 4 to 12 μm, and chemical deposition of a nickel-phosphorous protective layer ( 19 ) onto the etched metal surface, wherein the nickel-phosphorous protective layer comprises phosphorous, antimony and nickel. 2 . The method according to claim 1 , wherein the etching is carried out in an etching bath. 3 . The method according to claim 2 , wherein a temperature of the etching bath lies between 50 and 80° C. 4 . The method according to claim 2 , wherein an immersion time of the base body into the etching bath is between 20 and 40 seconds. 5 . The method according to claim 2 , wherein a dwell time of the base body in the etching bath is 60 to 110 seconds. 6 . The method according to claim 2 , wherein the base body is moved in the etching bath in a radially extending circular path. 7 . The method according to claim 6 , wherein a rotational speed of the base body in the etching bath is 10-15 rpm. 8 . The method according to claim 1 , wherein a coating composition is used for the chemical deposition which contains nickel ions, more than 10.3 wt. %, of phosphorous, and more than 0.3 wt. % of antimony, maximum 0.5 wt. % antimony, in each case relative to the total weight of the coating composition. 9 . The method according to claim 1 , wherein the base body is treated with a nitric acid solution prior to the chemical deposition of the nickel-containing layer. 10 . The method according to claim 1 , wherein the base body is formed from AlCuMgNi or AlCu 2 MgNi. 11 . A compressor wheel ( 17 ) for a turbocharger ( 1 ), the compressor wheel ( 17 ) having a base body and a nickel-phosphorous protective coating ( 19 ), the base body having an aluminum proportion of at least 50 atom percent, the base body having a specific etch pitting, wherein said specific etch pitting consists of nano etch pittings and micro etch pittings, wherein the nano etch pittings have a depth of 0.1 to 1.5 μm and micro etch pittings have a depth of 4 to 12 μm, and wherein the nickel-phosphorous protective coating ( 19 ) contains nickel, phosphorous, and more than 0.3 wt. % of antimony relative to the total weight of the coating composition. 12 . The compressor wheel according to claim 11 , wherein the coating ( 19 ) has a layer thickness variation of maximum±1.5 μm and a layer thickness of the coating ( 19 ) of approximately 20 μm. 13 . (canceled) 14 . (canceled) 15 . The compressor wheel according to claim 11 , wherein a volume ratio of the nano pittings to the micro pittings is 15:1 through 20:1. 16 . A turbocharger comprising the compressor wheel according to claim 11 . 17 . A compressor wheel according to claim 11 , wherein the coating composition is comprised of more than 10.3 wt. % phosphorous, and more than 0.3 wt. % of antimony, balance nickel, in case relative to the total weight of the coating composition. 18 . A compressor wheel according to claim 11 , wherein the coating composition is comprised of more than 10.5 wt. % phosphorous, and more than 0.3 wt. % but maximum 0.5 wt % antimony, balance nickel, in each case relative to the total weight of the coating composition.

Assignees

Inventors

Classifications

  • metallic substrate · CPC title

  • in turbochargers · CPC title

  • Coating with nickel, cobalt or mixtures thereof with phosphorus or boron (C23C18/50 takes precedence) · CPC title

  • for compressors · CPC title

  • only one step pretreatment · CPC title

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What does patent US2017370003A1 cover?
A turbocharger compressor wheel with an aluminum proportion of at least 50 atom percent, produced by. etching a turbine wheel base body using an alkaline etchant to produce a specific etch pitting consisting of nano pores and micropores and chemical deposition of a nickel-phosphorous protective layer ( 19 ) onto the etched base body surface.
Who is the assignee on this patent?
Borgwarner Inc
What technology area does this patent fall under?
Primary CPC classification C23C18/1827. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu Dec 28 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).