Multi-component deposition
AssigneeUnited Technologies Corporation
InventorsAlexander V. Makhotkin, Igor S. Malashenko, Igor V. Belousov
Life of this patent
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Abstract
Physical vapor deposition is augmented by chemical vapor deposition from one or more organometallic compounds to deposit multi-component materials. The organometallic compounds may be carbonyls. The process may be used to deposit coatings and repair material on superalloy turbine engine parts.
Claims38
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein:
- the part has lost first material from a site;
- and
- the deposition material is deposited to the site so as to replace the lost first material.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compounds, wherein:
- the one or more first components and one or more second components are codeposited on a worn or damaged gas turbine engine part to restore the part.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components;
- actively controlling a temperature of the part to, in turn, control dissociation of the one or more organometallic compounds, the actively controlling comprising irradiating the deposition material deposited on the part via an electron beam to cause electron beam-induced dissociation of the one or more organometallic compounds leaving one or more refractory metals as said one or more second components;
- and
- heat treating the part so as to homogenize the deposited deposition material.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein:
- the one or more organometallic compounds comprise, at least 50% by weight, carbonyls of one or more refractory elements.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein:
- the vaporizing of the one or more first components comprises vaporizing at least one M-Cr—Al—Ti alloy;
- and
- the deposition material consists essentially of a nickel- or cobalt-based superalloy.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein:
- the one or more first components consist in major part of Ti;
- and
- the one or more second components consist essentially of Mo.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein the deposition material consists essentially of:
- at least one of a nickel-or cobalt-based superalloy with 1-20%, by weight, refractory metal addition.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein the deposition material consists essentially of:
- at least one M-Cr—Al—Ti alloy;
- 2-20%, by weight, combined of one or more of W, Mo, Re, Pt, Rh, Ru, Os, Ir, Te, and V;
- and
- 0-0.3%, by weight, C.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound,
- wherein the one or more first components comprise, by weight:
- at least 50% of one or a combination of Ni, Co, and Fe;
- at least 12% Cr;
- at least 60% Al;
- and
- at least 0.5% Ti.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound, wherein:
- the one or more first components are from a single ingot;
- and
- the one or more second components are at least two refractory metal components from at least two different sources of different composition.
A method for depositing a deposition material on a part comprising:
- placing the part in a deposition chamber;
- vaporizing one or more first components for forming the deposition material by electron beam heating;
- and
- vaporizing one or more organometallic compounds for providing one or more second components of the deposition material being codeposited on the part with the first components, wherein:
- the part is a gas turbine engine part.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound, wherein:
- the one or more first components include:
- at least 50%, by weight, Ti;
- and
- the one or more second components consist essentially of:
- one or more refractory metals and up to 0.1%, by weight, C.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound, wherein:
- the one or more first components comprise at least 50%, by weight, Ti;
- and
- the one or more second components consist essentially of Mo.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound, wherein the method is used to deposit deposition material consisting essentially of:
- at least one of a nickel-or cobalt-based superalloy with 1-20%, by weight, refractory metal addition.
A method for codepositing one or more first components and one or more second components comprising:
- electron beam physical vapor deposition of the one or more first components;
- and
- chemical vapor deposition of the one or more second components from an organometallic compound, wherein the method is used to deposit deposition material consisting essentially of:
- at least one M-Cr—Al—Ti alloy;
- 2-20%, by weight, combined of one or more of W, Mo, Re, Pt, Rh, Ru, Os, Ir, Te, and V;
- and 0-0.3%, by weight, C.
Dependencies are inferred from the claim text.