Pulse plated abrasive grit

Patent metadata

Field	Value
Publication number	US-11078588-B2
Application number	US-201715401579-A
Country	US
Kind code	B2
Filing date	Jan 9, 2017
Priority date	Jan 9, 2017
Publication date	Aug 3, 2021
Grant date	Aug 3, 2021

Abstract

A method for forming an abrasive surface includes applying an electric current through a plating solution so as to cause an abrasive grit to be deposited onto a workpiece and varying a waveform of the electric current while building up a matrix material at least partially around the abrasive grit.

First claim

What is claimed:

1. A method for forming an abrasive surface on a tip of a rotor blade, comprising:
applying an electroplated strike/flash layer on the tip of the rotor blade via a plating solution that contains a matrix material, the electroplated strike/flash layer facilitating bonding of subsequent plating layers, the electroplated strike/flash layer between about 0.00005-0.001 inches (0.00127-0.0254 mm) thick, the rotor blade is one of a multiple of rotor blades that extend from an integrally bladed rotor (IBR) workpiece;
applying an electroplated electrolytic base layer on the strike/flash layer, the electrolytic base layer is between 0.0001-0.0004 inches (0.00254-0.01016 mm) thick;
placing the rotor blade in a first plating bath containing a plating solution and an abrasive grit therein then submerging the basket in the plating solution, the basket comprising a mesh bottom section that permits the plating solution to flow up into the abrasive grit;
flowing current through the basket and the abrasive grit, thence the blade tip, the abrasive grit in contact with the blade tip such that the nickel plating forms around the abrasive grit forming an electroplated tack layer on the electroplated electrolytic base layer by pulse plating within the first plating bath with a step wave waveform causing codeposition of a nickel layer matrix material and an abrasive grit onto the tip until the abrasive grit is tacked to the electroplated electrolytic base layer, the electroplated tack layer is 0.002 inches (0.0508 mm) thick;
placing the tip of the rotor blade in a second plating bath containing a fresh supply of plating solution without an abrasive grit therein;
applying an electroplated overplate layer on the electroplated tack layer by pulse plating within the second plating bath with a step wave waveform causing new nucleation of nickel crystals every time the current is turned on thereby building up a nickel layer matrix material with a grain size between 10-100 nm and a hardness between 250-400HV around the abrasive grit, the nickel layer matrix material of the overplate layer not building up over the abrasive grit because the abrasive grit is non-conductive and does not attract nickel ions from the plating solution, the electroplated overplate layer is between 0.003-0.004 inches (0.0762-0.102 mm) thick.

2. The method as recited in claim 1 , wherein applying the electroplated strike/flash layer comprises pulse plating for a total time period of 1 to 10 minutes.

3. The method as recited in claim 2 , wherein applying the electroplated overplate layer comprises pulse plating for a total time period of for 3 to 4 hours.

4. The method as recited in claim 1 , wherein applying the electroplated strike/flash layer on the tip of the rotor blade comprises reducing imperfections in the surface of the tip via a plating solution.

5. A method for forming an abrasive surface on a tip of a rotor blade, comprising:
applying an electroplated strike/flash layer on the tip of the rotor blade via a plating solution that contains a matrix material reducing imperfections in the surface of the tip, the electroplated strike/flash layer facilitating bonding of subsequent plating layers, wherein applying the electroplated strike/flash layer comprises pulse plating for a total time period of 1 to 10 minutes, the rotor blade is one of a multiple of rotor blades that extend from an integrally bladed rotor (IBR) workpiece;
applying an electroplated electrolytic base layer on the strike/flash layer;
placing the rotor blade in a first plating bath containing a plating solution and an abrasive grit therein, the first plating bath comprises placing the rotor blade into a basket containing the abrasive grit and submerging the basket in the plating solution, then flowing current through the basket and the abrasive grit, thence the blade tip, the basket comprising a mesh bottom section that permits the plating solution to flow up into the abrasive grit the abrasive grit in contact with the blade tip such that an electroplated tack layer formed thereby tacks the grit on the electroplated electrolytic base layer by pulse plating within the first plating bath with a step wave waveform, the step wave waveform causing codeposition of a nickel layer matrix material and an abrasive grit onto the tip until the abrasive grit is tacked to the electroplated electrolytic base layer; and
placing the tip of the rotor blade in a second plating bath containing a fresh supply of plating solution without an abrasive grit therein forming an electroplated overplate layer on the electroplated tack layer by pulse plating within the second plating bath with a step wave waveform causing nucleation of nickel crystals every time the current is turned on thereby building up a nickel layer matrix material with a grain size between 10-100 nm and a hardness between 250-400HV around the abrasive grit, the nickel layer matrix material of the overplate layer not building up over the abrasive grit because the abrasive grit is non-conductive and does not attract nickel ions from the plating solution, wherein applying the electroplated overplate layer comprises pulse plating for a total time period of for 3 to 4 hours, the resultant electroplated strike/flash layer between about 0.00005-0.001 inches (0.00127-0.0254 mm) thick, the electrolytic base layer is between 0.0001-0.0004 inches (0.00254-0.01016 mm) thick, the electroplated tack layer is 0.002 inches (0.0508 mm) thick, and the electroplated overplate layer between 0.003-0.004 inches (0.0762-0.102 mm) thick.

6. A method for forming an abrasive surface on a tip of a rotor blade, comprising:
applying an electroplated strike/flash layer on the tip of the rotor blade via a plating solution that contains a matrix material, the electroplated strike/flash layer facilitating bonding of subsequent plating layers, the electroplated strike/flash layer between about 0.00005-0.001 inches (0.00127-0.0254 mm) thick, the rotor blade is one of a multiple of rotor blades that extend from an integrally bladed rotor (IBR) workpiece;
applying an electroplated electrolytic base layer on the strike/flash layer, the electrolytic base layer is between 0.0001-0.0004 inches (0.00254-0.01016 mm) thick;
placing the rotor blade in a first plating bath containing a plating solution and an abrasive grit therein wherein placing the rotor blade in the first plating bath comprises rotating a workpiece with the rotor blade so that each blade tip of each rotor blade faces upward at during processing to be tacked with the abrasive grit, the abrasive grit in contact with the blade tip such that the nickel plating forms around the abrasive grit forming an electroplated tack layer on the electroplated electrolytic base layer by pulse plating within the first plating bath with a step wave waveform causing codeposition of a nickel layer matrix material and an abrasive grit onto the tip until the abrasive grit is tacked to the electroplated electrolytic base layer, the electroplated tack layer is 0.002 inches (0.0508 mm) thick, an anode positioned above the blade tip to direct the current down onto the blade tip to tack the abrasive grit and form the tack layer;
using air agitation so that the abrasive grit is circulated through the first bath to cause the abrasive grit to fall down onto each upward facing blade tip;
placing the tip of the rotor blade in a second plating bath containing a fresh supply of plating solution without an abrasive grit therein; and
applying an electroplated overplate layer on the electroplated tack layer by pulse plating within the second plating bath with a step wave waveform causing new nucleation of nickel crystals every time the current is turned on thereby building up a nickel layer matrix material with a grain size between 10-100 n

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Martel Nathan T
• Hanlon Thomas R

Classifications

• C25D5/18 Primary

  Electroplating using modulated, pulsed or reversing current · CPC title

• C25D7/00 Primary

  Electroplating characterised by the article coated · CPC title

• C25D5/623

  Porosity of the layers · CPC title

• C25D5/617

  Crystalline layers · CPC title

• C25D5/14

  two or more layers being of nickel or chromium, e.g. duplex or triplex layers · CPC title