초록 ▼

A process for coating a part comprises the steps of providing a chamber which is electrically connected as an anode, placing the part to be coated in the chamber, providing a cathode formed from a coating material to be deposited and platinum, and applying a current to the anode and the cathode to d

A process for coating a part comprises the steps of providing a chamber which is electrically connected as an anode, placing the part to be coated in the chamber, providing a cathode formed from a coating material to be deposited and platinum, and applying a current to the anode and the cathode to deposit the coating material and the platinum on the part.

대표청구항 ▼

1. A process for coating a turbine engine component comprising the steps of: providing a chamber which is electrically connected solely as an anode;placing said turbine engine component to be coated in said chamber;providing a cathode formed from a first MCrAlY material to be deposited where M is se

1. A process for coating a turbine engine component comprising the steps of: providing a chamber which is electrically connected solely as an anode;placing said turbine engine component to be coated in said chamber;providing a cathode formed from a first MCrAlY material to be deposited where M is selected from the group consisting of nickel, iron, and cobalt, and from a second material which is from 4.0 to 60 wt% platinum, said providing step including casting an ingot of said first MCrAlY material and electrically connecting said cast ingot as said cathode;applying a current in the range of from 300 to 500 amps from a first power supply to said anode and said cathode and applying a bias to the turbine engine component of −10V to −100V using a second power source to deposit said MCrAlY material and said second material on said turbine engine component;wherein said process comprises electrolytically plating at least one surface of said cast ingot with said second material prior to applying said current, wherein plating includes grading said platinum with a concentration greatest closest to the at least one surface and leanest away from said at least one surface; andwherein a heat treatment of the cast ingot is performed at a temperature in the range of from 1900 degrees Fahrenheit to 2000 degrees Fahrenheit for 3.5 to 5.0 hours to diffuse the platinum into the MCrAlY material. 2. The process according to claim 1, wherein said electrolytic plating step comprises immersing said ingot into a platinum plating solution containing from 17 to 40 grams/liter platinum concentration and applying a current in the range of from 0.2 to 0.6 amps. 3. The process according to claim 2, further comprising maintaining said platinum plating solution at a temperature in the range of from 190 to 200 degrees Fahrenheit. 4. The process according to claim 1, further comprising outgassing any byproduct gases. 5. The process according to claim 4, wherein said outgassing step comprises applying heat at a temperature in the range of from 350 to 400 degrees Fahrenheit for a time in the range of from 2.5 to 4.0 hours. 6. An apparatus for depositing a platinum modified coating on a turbine engine component comprising: a chamber which is electrically connected solely as an anode and in which the turbine engine component to be coated is placed; anda cathode formed from a cast ingot of an MCrAlY material to be deposited onto said turbine engine component where M is a material selected from the group consisting of nickel, iron and cobalt, wherein said cast ingot of said material to be deposited has an electroplated platinum on at least one surface, said electroplated platinum having a graded concentration of platinum greatest closest to the at least one surface and leanest away from the at least one surface;a current in the range of from 300 to 500 amps being applied to the cathode and to the chamber from a first power source to deposit a coating onto said turbine engine component;a bias in the range of from −10V to −100V being applied to said turbine engine component from a second power source during coating of said turbine engine component. 7. An apparatus according to claim 6, further comprising a carrier gas at a pressure in the range of 10-20 microns within the chamber. 8. An apparatus according to claim 7, wherein said carrier gas is argon.