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Preparation method of fiber-reinforced titanium matrix composite precursors

A titanium-based composite material and fiber-reinforced technology, which is applied in metal material coating technology, ion implantation plating, coating, etc., can solve problems that have not yet been discovered, and achieve the goals of avoiding interface pollution, good bonding, and good interface performance Effect

Active Publication Date: 2013-01-09
NORTHWEST INSTITUTE FOR NON-FERROUS METAL RESEARCH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] However, up to now, no information about the preparation of La by magnetron sputtering technology has been found. 2 Zr 2 o 7 Research on the application of barrier layers in the field of fiber-reinforced titanium matrix composite precursors has been reported

Method used

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  • Preparation method of fiber-reinforced titanium matrix composite precursors

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Effect test

Embodiment 1

[0033] The preparation method of the fiber-reinforced titanium matrix composite material precursor of the present embodiment comprises the following steps:

[0034] Step 1. Preparation of SiC_f / La 2 Zr 2 o 7 Silk:

[0035] Step 101. Put lanthanum zirconate with pyrochlore structure, TC4 titanium alloy and silicon carbide fiber together into a multi-target magnetron sputtering apparatus (JGP600 ultra-high vacuum multi-target magnetron sputtering apparatus, developed by Shenyang Scientific Instruments, Chinese Academy of Sciences Center Co., Ltd.) in the sputtering chamber, lanthanum zirconate is used as the sputtering target and silicon carbide fiber is used as the base material;

[0036] Step 102, vacuumize the sputtering chamber to a vacuum degree of 3×10 -5 Pa, and the silicon carbide fiber is heated to 500 ° C, and then argon gas is introduced into the sputtering chamber, and the radio frequency magnetron sputtering treatment is carried out under the conditions of argon...

Embodiment 2

[0042] The preparation method of the fiber-reinforced titanium matrix composite material precursor of the present embodiment comprises the following steps:

[0043] Step 1. Preparation of SiC_f / La 2 Zr 2 o 7 Silk:

[0044] Step 101. Put lanthanum zirconate with pyrochlore structure, TB8 titanium alloy and silicon carbide fiber together into a multi-target magnetron sputtering apparatus (JGP600 ultra-high vacuum multi-target magnetron sputtering apparatus, developed by Shenyang Scientific Instruments, Chinese Academy of Sciences Center Co., Ltd.) in the sputtering chamber, lanthanum zirconate is used as the sputtering target and silicon carbide fiber is used as the base material;

[0045] Step 102, vacuumize the sputtering chamber to a vacuum degree of 4×10 -5 Pa, and the silicon carbide fiber is heated to 510 ° C, and then argon gas is introduced into the sputtering chamber, and radio frequency magnetron sputtering is carried out under the conditions of argon gas pressure ...

Embodiment 3

[0051] The preparation method of the fiber-reinforced titanium matrix composite material precursor of the present embodiment comprises the following steps:

[0052] Step 1. Preparation of SiC_f / La 2 Zr 2 o 7 Silk:

[0053] Step 101, put lanthanum zirconate with pyrochlore structure, Ti600 titanium alloy and silicon carbide fiber together into a multi-target magnetron sputtering apparatus (JGP600 ultra-high vacuum multi-target magnetron sputtering apparatus, developed by Shenyang Scientific Instruments, Chinese Academy of Sciences Center Co., Ltd.) in the sputtering chamber, lanthanum zirconate is used as the sputtering target and silicon carbide fiber is used as the base material;

[0054] Step 102, vacuumize the sputtering chamber to a vacuum degree of 2×10 -5 Pa, and the silicon carbide fiber is heated to 490 ° C, and then argon gas is introduced into the sputtering chamber, and the radio frequency magnetron sputtering treatment is carried out under the conditions of the...

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Abstract

The invention provides a preparation method of fiber-reinforced titanium matrix composite precursors. The preparation method comprises the following steps of: (1) using zirconic acid lanthanum to serve as a sputtering target material, using silicon carbide fibers to serve as a substrate material, conducting magnetron sputtering on the zirconic acid lanthanum to deposit on surfaces of the silicon carbide fibers, and obtaining SiC-f / La2Zr2O7 silks; and (2) using a titanium alloy to serve as the sputtering target material, using the SiC-f / La2Zr2O7 silks to serve as the substrate material, conducting the magnetron sputtering on the titanium alloy to deposit on the surfaces of the SiC-f / La2Zr2O7 silks, and obtaining a fiber-reinforced titanium matrix composite precursor SiC-f / La2Zr2O7 / Ti alloy. The preparation method is simple in preparation process, high in production efficiency and strong in repeatability. The preparation method uses the zirconic acid lanthanum to serve as a separation layer to effectively protect silicon carbide fiber silks, the zirconic acid lanthanum has a good bonding performance with the silicon carbide fiber silks and the titanium alloy, and prepared fiber-reinforced titanium matrix composite precursors are good in high temperature heat stability and have good interface performances.

Description

technical field [0001] The invention belongs to the technical field of composite materials, and in particular relates to a preparation method of a fiber-reinforced titanium-based composite material precursor. Background technique [0002] Fiber-reinforced titanium-based composites have higher specific strength and specific modulus than titanium alloys, good high temperature resistance, creep resistance, and fatigue performance, and can be used in environments higher than 600 ° C. They are considered to be the next generation of high-thrust weight Key materials than aero-engines. At present, the research and development of fiber-reinforced titanium matrix composites in China is far behind the world level in terms of basic research and preparation technology, especially in the development and preparation technology of new high-performance barrier layers. Therefore, there is an urgent need to develop The preparation technology of the precursor of the new barrier layer with hig...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C47/04C22C49/00C23C14/35C23C14/06C23C14/18
Inventor 李磊卢亚锋杨义曾立英王耀
Owner NORTHWEST INSTITUTE FOR NON-FERROUS METAL RESEARCH
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