IP Library Granted Patent US 10,669,865
Granted Patent B2
US 10,669,865 · App. 15/732,374 · Granted Jun 2, 2020

Internal turbine component electroplating

Inventors: Willard N. Kirkendall (Muskegon, MI); Scott A. Meade (Muskegon, MI); Donald R. Clemens (Muskegon, MI)
Assignee: HOWMET CORPORATION
F01D5/286C25D5/022C25D5/08C25D5/48C25D7/00C25D7/04C25D17/004C25D17/10C25D17/12F01D5/186F01D9/02C25D3/50F05D2230/31F05D2300/143F05D2300/1431F05D2300/175F05D2300/177
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Quick Facts
Patent No.
US 10,669,865
App. No.
15/732,374
Granted
Jun 2, 2020
Kind
B2
Abstract

Method and apparatus are provided for electroplating a surface area of an internal wall defining a cooling cavity present in a gas turbine engine component.

Claims (14)

1. Apparatus for electroplating a surface area of an internal wall defining a cooling cavity present in a gas turbine engine component having a first end region with an opening into the cooling cavity and a second end region that is closed, comprising:

a first electrically insulating mask configured for fitting on the first end region of the component where the cooling cavity has a cavity open end to the exterior;

an anode extending through the first mask and the opening into the cooling cavity, the first mask supporting the anode in electrically insulated relationship to the component with the anode extending into the cooling cavity;

a second electrically insulating mask configured for fitting on the second end region exterior to the cooling cavity;

a cathode extending through the first mask to contact the component; and

an electroplating solution supply conduit or passage extending through the first mask adapted to supply electroplating solution to the cooling cavity.

2. The apparatus of claim 1 including a pump flowing a noble-metal containing electroplating solution to the supply conduit or passage and into the cooling cavity.

3. The apparatus of claim 1 wherein the solution includes at least one selected from the group of Pt and Pd to deposit at least one selected from the group of a Pt layer and Pd layer on the surf ace area.

4. The apparatus of claim 1 wherein the anode comprises nickel and the component is made of Ni base superalloy.

5. The apparatus of claim 1 wherein the component comprises a gas turbine engine vane or blade or segment thereof.

6. The apparatus of claim 1 wherein the anode resides on an anode support exterior of the mask so that the anode on the support is positioned in the cooling cavity when the component is disposed on the mask.

7. The apparatus of claim 1 including a tank having the electroplating solution therein and in which the component with the anode therein is submerged.

8. The apparatus of claim 1 wherein the mask comprises rubber.

9. The apparatus of claim 1 wherein the mask comprises a flexible material.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 23, 2019
From: KIRKENDALL, WILLARD N.; MEADE, SCOTT A.; CLEMENS, DONALD R.
To: HOWMET CORPORATION
Reel/Frame 048970/0120 →
Continuity (3)
Division 14121919 · Nov 3, 2014
Provisional Application 61964006 · Dec 20, 2013
Related Publication 20180073374A1 · Mar 15, 2018