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Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom

a technology of superalloy and nickel-base, which is applied in the field of nickel-base superalloy compositions, can solve the problems of inability to accept off-axial grains and reduce fatigue life, and achieve the effect of reducing the incidence of freckling and superior results

Inactive Publication Date: 2010-02-11
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0005]The present invention provides an alloy composition and method by which the incidence of freckling can be reduced in a unidirectionally-solidified casting having properties similar to unidirectionally-solidified castings produced from the N5 nickel-base superalloy.
[0008]According to a preferred aspect of the invention, the unidirectional crystal structure of the casting is substantially free of freckle defects. As used herein, the characterization of a casting being substantially free of freckles is meant to indicate a total combined length of all freckles of not more than 0.5 inch (about 12 mm). A significant advantage of this invention is that, though the composition of the casting contains the same alloying constituents as N5 and the alloying levels ofthese constituents are within or overlap the broadest ranges disclosed for N5, it has been determined that the employment of particular levels and relative proportions ofthese constituents are able to produce unexpected superior results as compared to the N5 alloy processed under identical conditions. In particular, the reduction in the incidence of freckling is greater than was expected for composition modifications alone, and the result is the absence of freckling that would otherwise be an expected property for N5 under the same processing conditions.

Problems solved by technology

Such defects can reduce fatigue life and act as grain initiators during the solidification process that cause unacceptable off-axial grains.

Method used

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  • Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom
  • Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom
  • Nickel-base superalloy, unidirectional-solidification process therefor, and castings formed therefrom

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Embodiment Construction

[0015]The present invention was the result of an effort to develop a nickel-base alloy having properties similar to the nickel-base alloy commercially known as René N5, but with a chemistry that reduces the tendency for freckling while maintaining the mechanical properties of the alloy, such as high temperature strength (including creep resistance), oxidation resistance, fatigue resistance, castability, and microstructural stability for use in such applications as the hot gas flow path of a gas turbine. As an example, FIG. 1 depicts a first stage bucket 10 for a land-based gas turbine, such as the H and FB class gas turbines used in the power-generating industry and manufactured by the assignee of the invention. The bucket 10 has an airfoil 12 and shank 14, with a dovetail 16 formed on the shank 14 for anchoring the bucket 10 to a turbine disk (not shown). As is common with turbine buckets, the bucket 10 is preferably unidirectionally cast to have a columnar single crystal (SX) or c...

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Abstract

An alloy composition and method by which the incidence of freckling can be reduced in castings produced with properties similar to the René N5 nickel-base superalloy. The casting has a unidirectional crystal structure and a composition consisting of, by weight, 6% to 8% chromium, 6% to 9% cobalt, 0% to 2% molybdenum, 4% to 6% tungsten, 6.4% to 6.9% tantalum, 0% to 2% titanium, 5% to 7% aluminum, 2.7% to 3.0% rhenium, 0.3% to 0.7% haffiium, 0.04% to 0.08% carbon, 0.002% to 0.006% boron, 0% to 0.075% yttrium, 0.002% to 0.004% zirconium, the balance being nickel and incidental impurities.

Description

BACKGROUND OF THE INVENTION[0001]The present invention generally relates to nickel-base superalloy compositions and processes for producing directionally-solidified castings therefrom. More particularly, the invention is directed to a nickel-base superalloy that is castable as single-crystal articles suitable for use as components of gas turbines and other high temperature applications.[0002]Components of gas turbines, such as blades (buckets), vanes (nozzles) and combustor components, are typically formed of nickel, cobalt or iron-base superalloys characterized by desirable mechanical properties at turbine operating temperatures. Because the efficiency of a gas turbine is dependent on its operating temperatures, there is an ongoing effort to develop components, and particularly turbine buckets, nozzles, and combustor components, that are capable of withstanding higher temperatures. As the material requirements for gas turbine components have increased, various processing methods an...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): C22C19/05C22F1/10B22D30/00
CPCB22D27/04C22C19/057B22D27/045
Inventor FENG, GANJIANGHUANG, SHYH-CHINZHENG, JIAN
Owner GENERAL ELECTRIC CO
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