Method for wire electro-discharge machining a part

Patent metadata

Field	Value
Publication number	US-10189100-B2
Application number	US-18159708-A
Country	US
Kind code	B2
Filing date	Jul 29, 2008
Priority date	Jul 29, 2008
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

A method for machining a part includes wire electro-discharge machining the part, and then selectively reducing a zinc content of the residual recast layer left on a surface of the part, while otherwise leaving the recast layer substantially intact.

First claim

The invention claimed is:

1. A method for machining a part, comprising, in sequence:
wire electro-discharge machining the part using a wire electrode having a zinc component to create a recast layer having an initial composition make-up including a zinc content and at least one other material content in an outer surface thereof as a result of wire electro-discharge machining the part; and
removing at least a portion of the zinc content from the outer surface of the recast layer without substantially altering the remainder of the initial composition make-up of the recast layer by submersing the part in a zinc-removing solution to remove the zinc content that is free within the recast layer and to produce a final composition make-up of the recast layer, the zinc-removing solution dissolving the zinc content that is free for removal from the outer surface and into the zinc-removing solution, the final composition make-up being substantially identical to the initial composition make-up except for the removed zinc content.

2. The method as defined in claim 1 , wherein removing the at least portion of the zinc content from the outer surface of the recast layer comprises removing at least a portion of non-alloyed zinc content from the outer surface of the recast layer.

3. The method as defined in claim 1 , wherein removing the at least portion of the zinc content from the outer surface of the recast layer comprises substantially eliminating the at least portion of the zinc content from the outer surface of the recast layer.

4. The method as defined in claim 1 , wherein removing the at least portion of the zinc content from the outer surface of the recast layer comprises substantially removing the at least portion of the zinc content from the outer surface having a thickness of about 100 nm.

5. The method as defined in claim 1 , wherein removing the at least portion of the zinc content from the outer surface of the recast layer comprises substantially removing the at least portion of the zinc content from the outer surface having a thickness of about 250 nm.

6. The method as defined in claim 1 , wherein the zinc-removing solution is a nitric acid solution.

7. The method as defined in claim 1 , wherein exposing the outer surface of the recast layer to the zinc-removing solution comprises submerging at least the recast layer in the zinc-removing solution.

8. The method as defined in claim 7 , wherein submerging at least the recast layer in the zinc-removing solution comprises submerging at least the recast layer in the zinc-removing solution for 15 minutes.

9. The method as defined in claim 7 , further comprising monitoring a zinc level of the zinc-removing solution, and keeping the outer surface of the recast layer submerged in the zinc-removing solution until the zinc level rate of change drops below a selected threshold.

10. The method as defined in claim 7 , further comprising monitoring a zinc level of the zinc-removing solution, and keeping the outer surface of the recast layer submerged in the zinc-removing solution until the zinc level rises to a selected maximum value.

11. The method as defined in claim 1 , wherein removing the at least portion of the zinc content from the outer surface of the recast layer comprises mechanically removing a portion of the outer surface of the recast layer high in zinc content while leaving a remainder of the recast layer otherwise substantially intact.

12. The method as defined in claim 1 , wherein the part is a turbine disc of a gas turbine engine, and wherein the wire electro-discharge machining step comprises forming a firtree profiled slot within the disc.

13. The method as defined in claim 1 , wherein the part is composed of a nickel based superalloy.

14. The method as defined in claim 1 , wherein the part is composed of a material selected from the group consisting of nickel based superalloys, stainless steels and aluminum alloys.

Assignees

• Ben Salah Nihad
• Bouthillier Alain
• Frederick Michel
• Fournier Jean
• Pratt & Whitney Canada

Inventors

• Ben Salah Nihad
• Bouthillier Alain
• Frederick Michel
• Fournier Jean

Classifications

• Y10T29/49336

  Blade making · CPC title

• B23H1/08

  Working media · CPC title

• B23H1/00 Primary

  Electrical discharge machining, i.e. removing metal with a series of rapidly recurring electrical discharges between an electrode and a workpiece in the presence of a fluid dielectric · CPC title

• B23H9/10

  Working turbine blades or nozzles · CPC title

• C23F1/00

  Etching metallic material by chemical means (manufacture of printing surfaces B41C; manufacture of printed circuits H05K) · CPC title