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Alloy material for aerospace field and manufacturing method thereof

An alloy material, aerospace technology, applied in the field of alloy material, aerospace, can solve the problem of reducing beryllium, performance can not reach beryllium bronze and other problems

Active Publication Date: 2014-02-05
SUZHOU RICHMOND ADVANCED MATERIAL TECH TRANSFER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the U.S. Occupational Safety and Health Administration called for reducing the use of beryllium, because beryllium has certain toxicity, and once the human body inhales its corresponding amount of dust, it will cause fatal lung diseases
In industrial production, among the existing alloy materials, for example, the yield strength of aluminum bronze is 431MPa, and the yield strength of copper-nickel-tin alloy is 724MPa, and its performance cannot reach the level of beryllium bronze, so it has not been fully accepted by people.

Method used

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  • Alloy material for aerospace field and manufacturing method thereof
  • Alloy material for aerospace field and manufacturing method thereof

Examples

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Effect test

Embodiment 1

[0023] The alloy material used to replace beryllium copper in the aerospace field, the components of the alloy material are composed of 6% nickel, 6% tin, 3% aluminum, 0.1% manganese, 0.02% iron, and 84.88% copper.

[0024] First, make copper-nickel alloy: put electrolytic copper, nickel, and tin in a power frequency electric furnace according to the weight ratio, heat to 900-950 degrees, smelt for 1-1.5 hours, and keep warm to 850 degrees after complete melting, and the holding time is 0.5-1 hour; secondly, manufacture aluminum-tin alloy: put aluminum ingots and tin in a power frequency electric furnace according to the weight ratio, heat to 660-700 degrees, smelt for 1-1.5 hours, and keep warm to 550 degrees after completely melting, The holding time is 0.5-1 hour; after holding the heat for 0.5-1 hour, add the aluminum-tin alloy solution to the copper-nickel alloy, stir it with a graphite rod and then raise the temperature to 1000 degrees; after that, make manganese and iron...

Embodiment 2

[0027] The alloy material used to replace beryllium bronze in the aerospace field, the components of the alloy material are composed of 8% nickel, 7% tin, 5% aluminum, 0.3% manganese, 0.06% iron, and 79.64% copper.

[0028] First, make copper-nickel alloy: put electrolytic copper, nickel, and tin in a power frequency electric furnace according to the weight ratio, heat to 900-950 degrees, smelt for 1-1.5 hours, and keep warm to 850 degrees after complete melting, and the holding time is 0.5-1 hour; secondly, manufacture aluminum-tin alloy: put aluminum ingots and tin in a power frequency electric furnace according to the weight ratio, heat to 660-700 degrees, smelt for 1-1.5 hours, and keep warm to 550 degrees after completely melting, The holding time is 0.5-1 hour; after holding the heat for 0.5-1 hour, add the aluminum-tin alloy solution to the copper-nickel alloy, stir it with a graphite rod and then raise the temperature to 1000 degrees; after that, make manganese and iron...

Embodiment 3

[0031] The alloy material used to replace beryllium copper in the aerospace field, the components of the alloy material are composed of 10% nickel, 9% tin, 6% aluminum, 0.5% manganese, 0.1% iron, and 74.4% copper.

[0032] First, make copper-nickel alloy: put electrolytic copper, nickel, and tin in a power frequency electric furnace according to the weight ratio, heat to 900-950 degrees, smelt for 1-1.5 hours, and keep warm to 850 degrees after complete melting, and the holding time is 0.5-1 hour; secondly, manufacture aluminum-tin alloy: put aluminum ingots and tin in a power frequency electric furnace according to the weight ratio, heat to 660-700 degrees, smelt for 1-1.5 hours, and keep warm to 550 degrees after completely melting, The holding time is 0.5-1 hour; after holding the heat for 0.5-1 hour, add the aluminum-tin alloy solution to the copper-nickel alloy, stir it with a graphite rod and then raise the temperature to 1000 degrees; after that, make manganese and iron ...

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Abstract

The invention provides an alloy material for the aerospace field and a manufacturing method thereof. The alloy material comprises the components by weight percent as follows: 6-10% of nickel, 6-9% of tin, 3-6% of aluminum, 0.1-0.5% of manganese, 0.02-0.1% of iron and 74.4-84.88% of copper. According to the invention, the beryllium element of a beryllium-copper alloy is replaced through complete fusion of a copper-nickel alloy material and an aluminum-tin alloy, and excellent properties of the alloy material are realized under the action of a plurality of trace elements; the yield strength of the material is greater than 980 MPa; and as a result, the alloy material provided by the invention completely takes the place of beryllium bronze and achieves the goal of environmental protection and health standards.

Description

technical field [0001] The invention relates to the field of alloy materials, in particular to alloy materials used in the field of aerospace to replace beryllium copper and a manufacturing method thereof. Background technique [0002] Beryllium bronze is made of copper-beryllium alloy. It has superior performance, and its yield strength can be higher than 965MPa. Therefore, it is widely used in high-end product parts such as bushings in the aerospace field. However, the U.S. Occupational Safety and Health Administration called for reducing the use of beryllium, because beryllium has certain toxicity, and once the human body inhales its corresponding amount of dust, it will cause fatal lung diseases. In industrial production, among the existing alloy materials, for example, the yield strength of aluminum bronze is 431MPa, and the yield strength of copper-nickel-tin alloy is 724MPa, and its performance cannot reach the level of beryllium bronze, so it has not been fully accep...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C9/02C22C9/06C22C1/02
Inventor 陆海荣孙飞赵勇
Owner SUZHOU RICHMOND ADVANCED MATERIAL TECH TRANSFER CO LTD
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