Turbocharger compressor wheels having a bi-layered coating and methods for manufacturing the same

Patent metadata

Field	Value
Publication number	US-11566631-B2
Application number	US-202117301169-A
Country	US
Kind code	B2
Filing date	Mar 29, 2021
Priority date	Mar 29, 2021
Publication date	Jan 31, 2023
Grant date	Jan 31, 2023

Abstract

A compressor wheel for a turbocharger includes a hub portion defining a rotational axis and a plurality of blades extending radially outward from the hub portion. Each blade of the plurality of blades includes a leading edge, the leading edges of each blade of the plurality of blades forming an inducer portion of the compressor wheel. Each blade of the plurality of blades further includes a trailing edge, the trailing edges of each blade of the plurality of blades forming an exducer portion of the compressor wheel. The inducer portion is positioned longitudinally forward from the exducer portion along a rotational axis with respect to a flow of air along the compressor wheel. The hub portion and the plurality of blades include a substrate metal. The substrate metal of the hub portion and the plurality of blades has coated directly thereon a first coating layer including electroless nickel-phosphorous. The first coating layer has coated directly thereon a second coating layer including hard chrome. The second coating layer has a thickness that is greatest at the inducer portion, with the thickness of the second coating layer decreasing rearward towards the exducer portion such that the thickness of the second coating layer is about zero microns at or longitudinally forward of the trailing edges of each blade of the plurality of blades.

First claim

What is claimed is:

1. A compressor wheel for a turbocharger, comprising:
a hub portion defining a rotational axis; and
a plurality of blades extending radially outward from the hub portion, wherein each blade of the plurality of blades comprises a leading edge, the leading edges of each blade of the plurality of blades forming an inducer portion of the compressor wheel, wherein each blade of the plurality of blades comprises a trailing edge, the trailing edges of each blade of the plurality of blades forming an exducer portion of the compressor wheel, the inducer portion being positioned longitudinally forward from the exducer portion along a rotational axis with respect to a flow of air along the compressor wheel,
wherein the hub portion and the plurality of blades comprise a substrate metal,
wherein the substrate metal of the hub portion and the plurality of blades has coated directly thereon a first coating layer comprising electroless nickel-phosphorous,
wherein the first coating layer has coated directly thereon a second coating layer comprising hard chrome, and
wherein the second coating layer has a thickness that is greatest at the inducer portion, the thickness of the second coating layer decreasing in a tapering manner rearward towards the exducer portion such that the thickness of the second coating layer is zero microns at or longitudinally forward of the trailing edges of each blade of the plurality of blades.

2. The compressor wheel of claim 1 , wherein the substrate metal comprises aluminum or an alloy thereof.

3. The compressor wheel of claim 1 , wherein the first coating layer comprising electroless nickel-phosphorous has a constant thickness across the hub portion and the plurality of blades from about 5 microns to about 30 microns.

4. The compressor wheel of claim 1 , wherein the first coating layer comprising electroless nickel-phosphorous comprises a phosphorous content of about 10 wt.-% to about 15 wt.-%.

5. The compressor wheel of claim 1 , wherein the second coating layer comprising hard chrome has a hardness of greater than about 800 HV.

6. The compressor wheel of claim 1 , wherein the thickness of the second coating layer at the inducer portion is from about 5 microns to about 25 microns.

7. A method for manufacturing a bi-layer coated compressor wheel for a turbocharger, comprising:
providing or obtaining a substrate compressor wheel, wherein the substrate compressor wheel comprises:
a hub portion defining a rotational axis, and
a plurality of blades extending radially outward from the hub portion, wherein each blade of the plurality of blades comprises a leading edge, the leading edges of each blade of the plurality of blades forming an inducer portion of the substrate compressor wheel, wherein each blade of the plurality of blades comprises a trailing edge, the trailing edges of each blade of the plurality of blades forming an exducer portion of the substrate compressor wheel, the inducer portion being positioned longitudinally forward from the exducer portion along a rotational axis with respect to a flow of air along the substrate compressor wheel,
wherein the hub portion and the plurality of blades comprise a substrate metal;

forming on the substrate metal of the hub portion and the plurality of blades a first coating layer comprising electroless nickel-phosphorous, wherein forming the first coating layer comprises immersing the substrate compressor wheel in an electroless nickel-phosphorous plating bath comprising nickel cations and phosphorous oxide anions; and
forming on the first coating layer a second coating layer comprising hard chrome, wherein the second coating layer has a thickness that is greatest at the inducer portion, the thickness of the second coating layer decreasing in a tapering manner rearward towards the exducer portion such that the thickness of the second coating layer is zero microns at or longitudinally forward of the trailing edges of each blade of the plurality of blades, and wherein forming the second coating layer comprises immersing the compressor wheel coated with the first coating layer in a chromium plating bath comprising an oxide of chromium and an acid of sulfur, and applying an electric current using an anode and a cathode, the compressor wheel coated with the first coating layer functioning as the cathode, wherein the inducer portion is oriented facing the anode in the chromium plating bath.

8. The method of claim 7 , further comprising performing a heat treatment step after forming the second layer comprising hard chrome.

9. The method of claim 8 , wherein the heat treatment step is performed for a time period of about 1 hour to about 4 hours at a temperature of up to about 300° C.

Assignees

• Garrett Transportation I Inc

Inventors

• Murukesan Palaniappa
• Renaud Philippe

Classifications

• F04D17/025

  comprising axial flow and radial flow stages · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D29/285 Primary

  the compressor wheel comprising a pair of rotatable bladed hub portions axially aligned and clamped together · CPC title

• F05D2240/303

  related to the leading edge of a rotor blade · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title