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Co-based alloy

a co-based alloy and alloy technology, applied in the field of co-based alloys, can solve the problems of inferior machinability and hot workability of ni-based alloys, harmful processing, and inferior hot workability of conventional co-based alloys, and achieve the effects of suppressing grain boundary sliding, reducing hot workability, and large

Inactive Publication Date: 2013-08-15
TOHOKU UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The patent text describes a method to improve the hot workability and high-temperature characteristics of a Co-based alloy. By adjusting the composition of the alloy and subjecting it to specific heat treatment processes, a less harmful phase can be generated and a strengthening phase can be precipitated. Additionally, carbide can be precipitated in grain boundaries to further improve the alloy's performance. These improvements make the Co-based alloy more durable and better suited for high-temperature applications.

Problems solved by technology

However, there is a problem that the Ni-based alloy is inferior in machinability and hot workability.
However, there was a problem that a conventional Co-based alloy has a lower high-temperature strength than the Ni-based alloy and is inferior in hot workability to the Ni-based alloy, since a γ′-type intermetallic compound effective for improving the high-temperature strength properties of the Co-based alloy was not known.
However, the Co-based alloy including Al and W may have a second phase precipitate depending on heat treatment conditions, that is harmful to processing.
Thus, hot workability may be significantly decreased.
However, high-temperature strength properties of a conventional alloy are not always sufficient.

Method used

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  • Co-based alloy

Examples

Experimental program
Comparison scheme
Effect test

examples 1 to 27

, Comparative Examples 31 to 52

1. Preparation of Specimens

[0074]Alloys having compositions shown in Tables 1 and 2 were each melted in a vacuum induction furnace to obtain a 50 kg ingot. Each ingot prepared by melting was subjected to homogenizing heat treatment at 1200° C. for 16 hours. Then, the ingot was forged into a rod having a diameter of 16 mm. Solution treatment (ST) was performed for the forged material, under conditions of 1200° C. and followed by air cooling for one hour. Then, two-step aging treatment (AG) was performed under conditions of 900° C. for 24 hours followed by air cooling, and furthermore, under conditions of 800° C. for 24 hours followed by air cooling.

TABLE 1composition (mass %)CNiCoCrWAlBMgZrCaothersExample 10.02047.6Bal12.416.23.7—————Example 20.00448.2Ba12.115.23.9—————Example 30.06046.9Bal12.315.44.1—————Example 40.02040.1Bal11.915.34.2—————Example 50.02142.3Bal12.116.33.5—————Example 60.02051.2Bal12.116.03.4—————Example 70.01652.5Bal12.316.13.6—————Ex...

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Abstract

A Co-based alloy containing not less than 0.001 mass % and less than 0.100 mass % of C, not less than 9.0 mass % and less than 20.0 mass % of Cr, not less than 2.0 mass % and less than 5.0 mass % of Al, not less than 13.0 mass % and less than 20.0 mass % of W, and not less than 39.0 mass % and less than 55.0 mass % of Ni, with the remainder being made up by Co and unavoidable impurities, wherein the contents of Mo, Nb, Ti and Ta which are included in the unavoidable impurities are as follows: Mo<0.010 mass %, Nb<0.010 mass %, Ti<0.010 mass %, and Ta<0.010 mass %.

Description

TECHNICAL FIELD[0001]The present invention relates to a Co-based alloy suitable for various components required to have a high strength in a high-temperature environment, such as for a gas turbine, an aircraft engine, a chemical plant, a vehicle engine and a high-temperature furnace. In particular, it relates to a Co-based suitable for casting.BACKGROUND ART[0002]A Ni-based alloy, a Co-based alloy, an Fe-based alloy or the like have been known as a superalloy used at a high-temperature. The Ni-based alloy is precipitation-strengthened by a γ′ phase having an L12 structure (Ni3(Al, Ti)), and exhibits a reverse temperature dependency where strength increases as a temperature increases. In addition, the Ni-based alloy has excellent high-temperature properties such as heat resistance, corrosion resistance, oxidation resistance and creep resistance. Thus, the Ni-based alloy is used for various purposes which require a high strength in a high-temperature environment. However, there is a p...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): C22F1/10C22C30/00C22C19/05
CPCC22C19/055C22C19/056C22C19/057C22F1/10C22C30/00F05C2201/0463F05D2300/17Y02T50/671F01D5/28Y02T50/60
Inventor SATO, JUNIMANO, SHINYAOSAKI, MOTOTSUGUUETA, SHIGEKIISHIDAOMORI, TOSHIHIRONISHIDA, HIROAKIHAYASHI, MASAHIROSHIOTA, TOMOKI
Owner TOHOKU UNIV
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