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Continuous SiC fiber-reinforced refractory metal-based composite material based on nano-multilayer structure and preparation method and application of continuous SiC fiber-reinforced refractory metal-based composite material

A refractory metal, nano-multilayer technology, applied in metal material coating process, coating, ion implantation plating, etc., can solve problems such as excessive molding temperature, interface reaction SiC fiber reinforcement performance degradation, etc., to achieve release Residual stress, abundant optional types, and the effect of suppressing interface reaction

Active Publication Date: 2022-02-25
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the above preparation method uses refractory alloy target sputtering to deposit refractory alloy coating, but due to the high temperature yield strength of refractory alloy, the forming temperature is too high, resulting in severe interfacial reaction and performance degradation of SiC fiber reinforcement

Method used

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  • Continuous SiC fiber-reinforced refractory metal-based composite material based on nano-multilayer structure and preparation method and application of continuous SiC fiber-reinforced refractory metal-based composite material
  • Continuous SiC fiber-reinforced refractory metal-based composite material based on nano-multilayer structure and preparation method and application of continuous SiC fiber-reinforced refractory metal-based composite material
  • Continuous SiC fiber-reinforced refractory metal-based composite material based on nano-multilayer structure and preparation method and application of continuous SiC fiber-reinforced refractory metal-based composite material

Examples

Experimental program
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Effect test

preparation example Construction

[0034] The present invention provides a method for preparing a continuous SiC fiber-reinforced refractory metal matrix composite material based on a nano-multilayer structure described in the above technical solution, comprising the following steps:

[0035] (1) Using a transition metal target, the first magnetron sputtering is carried out on the surface of a continuous SiC fiber with a carbon coating under an inert gas to form a transition metal layer;

[0036] (2) Using a transition metal target, under nitrogen-inert mixed gas, performing second magnetron sputtering on the surface of the transition metal layer to form a transition metal nitride layer to obtain a diffusion barrier unit;

[0037] (3) repeating the preparation operation of the transition metal layer and the transition metal nitride layer on the surface of the diffusion barrier unit to obtain a diffusion barrier coating; the number of repetitions is ≥ 0 times;

[0038] (4) Under an inert gas, using refractory me...

Embodiment 1

[0068] (1) According to figure 1 The multi-magnetron sputtering device shown and figure 2 The preparation process shown prepares continuous SiC fiber-reinforced refractory metal matrix composites based on nano-multilayer structure, and the specific steps are as follows:

[0069] Fix the continuous SiC fiber with carbon coating on the rectangular sample holder, keep the distance between single fibers at 0.2 mm, and put it into the sample chamber of the multi-target magnetron sputtering equipment; put the Ti target, Nb refractory target and The W refractory targets were respectively placed in the multi-target magnetron sputtering equipment, and the distance between each target and the sample was kept at 10 cm.

[0070] (2) Vacuum the multi-magnetron sputtering equipment until the background vacuum is lower than 8×10 -4 Pa, the rotation speed of the sample is 50r / h, argon gas is passed through, and the continuous SiC fiber with carbon coating on the surface is sputtered and cl...

Embodiment 2

[0077] A continuous SiC fiber-reinforced refractory metal matrix composite based on a nano-multilayer structure was prepared according to the method of Example 1, the difference from Example 1 is that:

[0078] In step (6), the deposition current of the refractory metal W is 1.5A, the deposition time is 320 min, and the thickness of the composite Nb / W refractory metal layer is 24 μm.

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Abstract

The invention relates to the technical field of metal-based composite materials, in particular to a continuous SiC fiber-reinforced refractory metal-based composite material based on a nano-multilayer structure and a preparation method and application of the continuous SiC fiber-reinforced refractory metal-based composite material. The transition metal layer is deposited on the surface of the continuous SiC fiber with the carbon coating on the surface, so that the bonding performance of the continuous SiC fiber with the carbon coating on the surface and the subsequently deposited metal nitride layer is effectively improved, and the residual stress is effectively released; and the interface bonding strength of the continuous SiC fiber with the carbon coating on the surface and the nano multi-layer composite refractory metal layer is improved. The nano-multilayer composite refractory metal layer is prepared from the refractory metal elementary substance target materials made of at least two materials, compared with a refractory alloy target material, the temperature of follow-up hot isostatic pressing forming is remarkably reduced, interface reaction and fiber degradation can be inhibited, the selectable types of refractory alloy matrix components are greatly enriched, and the requirements of different application environments on the performance of the composite material can be met and the cost is low.

Description

technical field [0001] The invention relates to the technical field of metal-matrix composite materials, in particular to a continuous SiC fiber-reinforced refractory metal-matrix composite material based on a nano-multilayer structure and its preparation method and application. Background technique [0002] With the development of aerospace technology, the service environment is becoming increasingly harsh. In order to meet the needs of extremely harsh service environments, aerospace vehicles have put forward higher requirements for the temperature resistance of metal matrix composites—excellent mechanical properties in a wide temperature range. performance. The continuous SiC fiber reinforced titanium matrix composite combines the high strength and excellent creep resistance of the reinforcement with the high damage tolerance and machinability of the titanium alloy matrix, which not only greatly improves the mechanical strength of the metal matrix , Creep resistance and f...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C47/04C23C14/35C23C14/18C23C14/06C22C47/14C22C49/10C22C49/14C22C101/14
CPCC22C47/04C23C14/352C23C14/185C23C14/0073C23C14/0641C22C47/14C22C49/10C22C49/14
Inventor 文懋王麒骅齐金磊王龙鹏张侃郑伟涛
Owner JILIN UNIV
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