IP Library Granted Patent US 7,622,150
Granted Patent B2
US 7,622,150 · App. 10/253,750 · Granted Nov 24, 2009

Oxidation resistant coatings for molybdenum silicide-based composite articles

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Quick Facts
Patent No.
US 7,622,150
App. No.
10/253,750
Granted
Nov 24, 2009
Kind
B2
Abstract

An environmentally resistant coating comprising silicon, titanium, chromium, and a balance of niobium and molybdenum for turbine components formed from molybdenum silicide-based composites. The turbine component may further include a thermal barrier coating disposed upon an outer surface of the environmentally resistant coating comprising zirconia, stabilized zirconia, zircon, mullite, and combinations thereof. The molybdenum silicide-based composite turbine component coated with the environmentally resistant coating and thermal barrier coating is resistant to oxidation at temperatures in the range from about 2000° F. to about 2600° F. and to pesting at temperatures in the range from about 1000° F. to about 1800° F.

Claims (13)

1. A method of making a turbine component comprising a molybdenum silicide-based composite and having an environmentally resistant coating disposed on a surface of the molybdenum silicide-based composite, the environmentally resistant coating comprising silicon, titanium, chromium, niobium, and molybdenum, the method comprising the steps of:

a) providing a molybdenum silicide-based composite substrate formed into the turbine component;

b) depositing silicon, chromium, titanium, and niobium on the surface of the molybdenum silicide-based composite using a deposition method selected from the group consisting of ion plasma deposition, vacuum plasma spraying, high velocity oxy-fuel spraying, physical vapor deposition, chemical vapor deposition and dipping the molybdenum silicide-based composite into a slurry comprising silicon, chromium, titanium, and niobium; and

c) heat treating the molybdenum silicide-based composite substrate for at least about one hour at a temperature of at least about 1200° C. to form the environmentally resistant coating on the surface of the turbine component, wherein the step of heat treating follows the step of depositing silicon, chromium, titanium, and niobium on the surface of the molybdenum silicide-based composite.

2. The method of claim 1 , further comprising the step of depositing a thermal barrier coating on an outer surface of the environmentally resistant coating.

3. The method of claim 1 , wherein the environmentally resistant coating comprises between about 43 and 67 atomic percent silicon, between about 2 and about 25 atomic percent titanium, between about 1 and about 25 atomic percent chromium, and a balance of niobium and molybdenum.

4. A method of coating a molybdenum silicide-based composite substrate with an environmentally resistant coating the environmentally resistant coating comprising silicon, titanium, chromium, niobium, and molybdenum, the method comprising the steps of:

a) providing a molybdenum silicide-based composite substrate;

b) depositing silicon, chromium, titanium, and niobium on a surface of the molybdenum silicide-based composite substrate using a deposition method selected from the group consisting of ion plasma deposition, vacuum plasma spraying, high velocity oxy-fuel spraying, physical vapor deposition, chemical vapor deposition and dipping the molybdenum silicide-based composite into a slurry comprising silicon, chromium, titanium, and niobium; and

c) heat treating the molybdenum silicide-based composite substrate for at least about one hour at a temperature of at least about 1200° C. to form the environmentally resistant coating on the surface of the molybdenum silicide-based composite substrate, wherein the step of heat treating follows the step of depositing silicon, chromium, titanium, and niobium on the surface of the molybdenum silicide-based composite.

5. The method of claim 4 , wherein the environmentally resistant coating comprises between about 43 and 67 atomic percent silicon, between about 2 and about 25 atomic percent titanium, between about 1 and about 25 atomic percent chromium, and a balance of niobium and molybdenum.

6. The method of claim 1 , further comprising the step of heat treating the environmentally resistant coating at 1600° C. to consolidate the environmentally resistant coating.

7. The method of claim 4 , further comprising the step of heat treating the environmentally resistant coating at 1600° C. to consolidate the environmentally resistant coating.

Assignments (5)
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE TO GENERAL ELECTRIC COMPANY & CORRECT CORRESPONDENCE STREET ADDRESS TO: 1 RESEARCH CIRCLE PREVIOUSLY RECORDED ON REEL 027518 FRAME 0803. ASSIGNOR(S) HEREBY CONFIRMS THE CLARIFICATION OF OWNERSHIP. Recorded Jan 13, 2012
From: GENERAL ELECTRIC COMPANY
To: GENERAL ELECTRIC COMPANY
Reel/Frame 027531/0149 →
CLARIFICATION OF OWNERSHIP Recorded Jan 11, 2012
From: GENERAL ELECTRIC COMPANY
To: GENEFRAL ELECTRIC COMPANY
Reel/Frame 027518/0803 →
RELEASE OF SECURITY INTEREST Recorded Jun 19, 2009
From: CITIBANK, N.A.
To: SABIC INNOVATIVE PLASTICS IP B.V.
Reel/Frame 022846/0411 →
SECURITY AGREEMENT Recorded Aug 18, 2008
From: SABIC INNOVATIVE PLASTICS IP B.V.
To: CITIBANK, N.A., AS COLLATERAL AGENT
Reel/Frame 021423/0001 →
CONFIRMATORY LICENSE Recorded Dec 4, 2002
From: GENERAL ELECTRIC COMPANY
To: AIR FORCE, UNITED STATES
Reel/Frame 013566/0671 →