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Preparation method of thin-walled c/sic extension

An extension section and thin-wall technology, which is applied in the field of thin-wall C/SiC extension section preparation, can solve the problems of complex manufacturing process, expensive materials, and poor high-temperature oxidation resistance of niobium alloys, so as to reduce quality, improve engine performance, The effect of reducing the production cost

Active Publication Date: 2022-02-15
湖北三江航天江北机械工程有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Niobium alloys have good atmospheric corrosion resistance and good processing performance. Niobium alloys can maintain high strength at high temperatures, but niobium alloys have poor high-temperature oxidation resistance, expensive materials, and complicated manufacturing processes.

Method used

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  • Preparation method of thin-walled c/sic extension

Examples

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preparation example Construction

[0020] A method for preparing a thin-walled C / SiC extension, comprising the following steps:

[0021] 1) Lay up the carbon fiber cloth one by one, and prepare the extension section preform along the mandrel by sewing; the carbon fiber cloth for sewing is T300B-3K plain weave cloth, the yarn for sewing is carbon fiber T300B-6K, and the sewing distance is 2-4mm / needle;

[0022] 2) Put the prefabricated body of the extension section into the furnace, and carry out the degumming treatment. The degumming treatment temperature is 600-1100°C, the vacuum degree is -70--99KPa, and the time is 5-10h;

[0023] 3) Put the prefabricated body that has been degummed into a vapor deposition furnace for chemical vapor infiltration to 0.8-1.0g / cm 3 , The carbon source gas for chemical vapor deposition is methane or propylene, the purity of methane or propylene is above 99.99%, the deposition temperature is 800-1200°C, the pressure is -0.08-0.09MPa, and the time is 120-240h;

[0024] 4) Prepare...

Embodiment 1

[0033] 1) After laying the carbon fiber cloth T300B-3K plain weave cloth along the mandrel to reach 5mm, connect each layer of carbon fiber cloth into a whole by suturing to form an extension prefabricated body, and the sewing stitch distance is 3mm / needle;

[0034] 2) Put the prefabricated body of the extension section into the furnace, and carry out degumming treatment. The degumming treatment temperature is 800°C, the vacuum degree is -90KPa, and the time is 6h;

[0035] 3) Put the prefabricated body that has been degummed into a vapor deposition furnace for chemical vapor infiltration to 0.8g / cm 3 , the carbon source gas for chemical vapor deposition is methane, the deposition temperature is 1000°C, the pressure is -0.09MPa, and the time is 200h;

[0036] 4) Prepare a mixed solution A with polycarbosilane and divinylbenzene at a mass ratio of 1:0.5, and put the mixed solution A into a vacuum impregnation container A; then put the small end of the extension preform into the...

Embodiment 2

[0044] 1) After laying the carbon fiber cloth T300B-3K plain weave cloth along the mandrel to reach 5mm, connect each layer of carbon fiber cloth into a whole by suturing to form a prefabricated extension section, and the sewing stitch distance is 4mm / needle;

[0045] 2) Put the prefabricated body of the extension section into the furnace, and carry out the degumming treatment. The degumming treatment temperature is 900°C, the vacuum degree is -80KPa, and the time is 8h;

[0046] 3) Put the preform that has been degummed into a vapor deposition furnace for chemical vapor infiltration to 0.9g / cm 3 , the carbon source gas for chemical vapor deposition is methane, the deposition temperature is 1100°C, the pressure is -0.07MPa, and the time is 180h;

[0047] 4) Prepare a mixed solution A with polycarbosilane and divinylbenzene at a mass ratio of 1:0.6, and put the mixed solution A into a vacuum impregnation container A; then put the small end of the extension preform into the vacu...

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Abstract

The invention discloses a method for preparing a thin-walled C / SiC extension section. Carbon fiber cloths are sequentially stacked to prepare an extension section preform, degumming treatment is performed, chemical vapor infiltration is performed, and mixed solution A is sucked into the preform by vacuum impregnation. The small end-injecting the mixed solution B into the extension preform by vacuum impregnation-putting the cured extension preform into the furnace for high temperature treatment-circulating until the added weight of the latter round is less than that of the previous round. 1%. The density of the extended section prepared by the present invention does not exceed 2.0g / cm 3 , while the density of traditional niobium alloy is 8.85g / cm 3 , which can effectively reduce the quality of the extension section and improve the performance of the engine; in addition, the extension section provided by the present invention is compared with the conventional niobium alloy extension section, because SiC and Si‑O‑C materials have good oxidation resistance, and do not need complex oxidation resistance treatment. , the preparation process is simple.

Description

technical field [0001] The invention belongs to the technical field of C / SiC composite ceramics, and in particular relates to a method for preparing a thin-walled C / SiC extension. Background technique [0002] The extension section of the liquid rocket engine is used to increase the area ratio of the nozzle of the engine, which is one of the main measures to improve the specific impulse of the engine. Now widely used refractory metal niobium alloy as the extension material. Niobium alloys have good atmospheric corrosion resistance and good processing performance. Niobium alloys can maintain high strength at high temperatures, but niobium alloys have poor high-temperature oxidation resistance, expensive materials, and complicated manufacturing processes. Contents of the invention [0003] The object of the present invention is to address the deficiencies of the above technologies, and provide a method for preparing a thin-walled C / SiC extension that can effectively reduce ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/80
CPCC04B2235/3826C04B2235/5248C04B2235/483C04B2235/77C04B2235/96
Inventor 陈海昆吴广力金秀秀王芬王宇峰
Owner 湖北三江航天江北机械工程有限公司