Method for Substrate Stabilization of Diffusion Aluminide Coated Nickel-Based Superalloys

a technology of nickel-based superalloys and substrates, which is applied in the direction of solid-state diffusion coatings, transportation and packaging, coatings, etc., can solve the problems of affecting the mechanical properties of articles and the substrate is devoid of the beneficial effects of refractory elements, and achieves the effect of increasing the chemical activity of carbon and quick drying

Inactive Publication Date: 2009-08-06
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The process effectively controls the depth of carburization, preventing the formation of weak SRZ regions and maintaining the mechanical properties of the superalloy, allowing for improved strength and fatigue resistance by forming stable carbides that reduce the availability of refractory elements for TCP phase formation.

Problems solved by technology

The duration of the carburization process itself is controlled to limit the depth of carbide layer formation, since carbide layers that are too thick also can adversely affect the mechanical properties of the article.
Clearly, over-carburization that produces a layer that is too thick results in a substrate that is devoid of the beneficial effects of the refractory elements, as the refractory elements are tied up in the stable carbides.

Method used

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  • Method for Substrate Stabilization of Diffusion Aluminide Coated Nickel-Based Superalloys
  • Method for Substrate Stabilization of Diffusion Aluminide Coated Nickel-Based Superalloys
  • Method for Substrate Stabilization of Diffusion Aluminide Coated Nickel-Based Superalloys

Examples

Experimental program
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Effect test

example 1

[0044]Articles were carburized in a Turbotreater® horizontal vacuum carburizing furnace, Model H3636 AvaC™ Ipsen International Furnace having multiple nozzles for introducing gases. Such a furnace is available from Ipsen International of Rockford, Ill. The furnace has a working zone of 3′×2′×2′ (l×w×h). The furnace utilizes carbon heating elements that do not react with the gases introduced. The working zone was loaded with a plurality of turbine blades, after cleaning, about 10-50. These turbine blades are small commercial engine blades made of refractory-containing superalloy and having a size (overall blade length) of about 1.5″. The blades were maintained under a reducing atmosphere, as hydrogen was introduced into the furnace to a pressure of about 0.150 Torr until the carburizing temperature of 1975° F. was reached. Once at 1975° F., the hydrogen was evacuated from the furnace work zone and acetylene gas was then introduced into the furnace at a flow rate of approximately 100 ...

example 2

[0045]A Turbotreater® horizontal vacuum carburizing furnace Model H3636 AvaC™ Ipsen International Furnace was used, as described in Example 1. 1″ diameter by 0.125″ thick specimen were maintained under a vacuum atmosphere of less than 0.001 Torr until the carburizing temperature of 1975° F. was reached. Once the temperature was stabilized at 1975° F., acetylene gas was introduced into the furnace at a flow rate of about 100 liters per hour to maintain a pressure of about 2 Torr for a time of about 10 minutes. After about 10 minutes of carburization, the acetylene was evacuated from the furnace work zone and argon gas was introduced to allow for rapid cooling of the furnace load below about 1800° F. A zone of submicron carbide particles was formed in the near surface region of the blades, the depth of which was about 74 microns for the samples. A sample was coated with a platinum modified beta nickel-aluminide coating ant then exposed to 2000° F. for about 400 hours. The aluminide co...

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Abstract

An article and method for stabilization of a nickel-based superalloy coated with a diffusion aluminide coating. The region below the aluminide coating is first carburized to form refractory carbides. The article is cleaned and masked as required so that regions that will not have an aluminide coating are not carburized. After placing the article into a furnace and heating in a non-oxidizing atmosphere to a carburizing temperature, a carburizing gas is introduced, and the near surface region is carburized to a depth of about 100 microns. Refractory carbides are formed in this region. When a diffusion aluminide coating is formed on the article, the refractory elements, being present as refractory carbides, are not available to form detrimental TCP phases.

Description

CROSS REFERENCE TO RELATED APPLICATIONS[0001]This application is a divisional of U.S. application Ser. No. 11 / 359,788, filed Feb. 22, 2006, which is incorporated by reference in its entirety and which claims the benefit of U.S. Provisional Application No. 60 / 656,691, filed Feb. 26, 2005.FIELD OF THE INVENTION[0002]The present invention relates to the carburization of nickel-based superalloys, and more particularly, to methods for carburizing nickel-based superalloys that include refractory elements for preventing the formation of secondary reaction zones.BACKGROUND OF THE INVENTION[0003]In a gas turbine engine such as used for aircraft applications, air is drawn into the front of the engine, compressed by a compressor, and mixed with fuel. The compressed mixture is burned in a combustor, and the hot combustion gases flow through a turbine that turns the compressor. The hot gases then flow from the rear of the engine.[0004]The turbine includes stationary turbine vanes that deflect th...

Claims

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Application Information

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Patent Type & AuthorityApplications(United States)
IPC IPC(8): B32B15/04
CPCC23C8/02C23C8/04Y10T428/12576C23C10/48Y02T50/67C23C8/20Y02T50/60
InventorFINK, PAUL J.HAZEL, BRIAN T.GOVERN, CHRISTINEGREENE, JOSEPH M.
OwnerGENERAL ELECTRIC CO