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A preparation method of aluminum-stainless steel composite pipe for thermal control of space vehicle

A technology for a space vehicle and a stainless steel tube is applied in the field of preparation of an aluminum-stainless steel composite tube for thermal control of a space vehicle, which can solve the problems of influence and the stainless steel tube cannot be deformed greatly, achieves high straightness, and satisfies the mechanical environment adaptability. requirements, the effect of high resistance to mechanical vibration mechanical properties

Active Publication Date: 2018-02-06
GENERAL RESEARCH INSTITUTE FOR NONFERROUS METALS BEIJNG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of this process is that the fixed and constrained aluminum tube and the drawn stainless steel tube cannot produce large deformation, and the large deformation has a great impact on the dimensions and tolerances of the stainless steel tube, such as wall thickness, inner hole roundness, and inner hole coaxiality. have a serious impact

Method used

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  • A preparation method of aluminum-stainless steel composite pipe for thermal control of space vehicle
  • A preparation method of aluminum-stainless steel composite pipe for thermal control of space vehicle
  • A preparation method of aluminum-stainless steel composite pipe for thermal control of space vehicle

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Effect test

Embodiment 1

[0049] A certain specification of lightweight, pressure-resistant, high heat transfer capacity aluminum-stainless steel composite tube is used for the condenser of the thermal control system of a space vehicle.

[0050] Aluminum-stainless steel composite pipe structure: the inner stainless steel pipe 1 is made of 304 austenitic stainless steel, the outer aluminum alloy pipe 5 is 6063, the stress relief metal layer 3 is made of pure silver, and the brazing material is AlSiMg12-2 foil.

[0051] Specifications of aluminum-stainless steel composite pipe: the outer diameter of stainless steel pipe 1 is 6mm, the wall thickness is 0.8mm, the aluminum alloy pipe 5 is a special-shaped cross-section pipe, and the total length of aluminum-stainless steel composite pipe is 270mm.

[0052] 1. Preparation process:

[0053] The preparation process of aluminum-stainless steel composite pipe adopts the process route of hot pressing brazing and 2 times hot isostatic pressing treatment. The main...

Embodiment 2

[0081] The evaporator of a space vehicle thermal control system uses a certain specification of light-weight, pressure-resistant, high-heat-transfer aluminum-stainless steel composite tube.

[0082] Aluminum-stainless steel composite pipe structure: the inner stainless steel pipe 1 is made of 316L austenitic stainless steel, the outer aluminum alloy pipe 5 is 3A21, the stress relief metal layer 3 is made of oxygen-free copper, and the brazing material is ZnAl25 foil.

[0083] Aluminum-stainless steel composite pipe specifications: stainless steel pipe 1 has an outer diameter of 10mm, an internal thread size of M8×0.5mm, aluminum alloy pipe 5 is a special-shaped cross-section pipe, and the total length of aluminum-stainless steel composite pipe is 130mm.

[0084] 1. Preparation process:

[0085] The preparation process of aluminum-stainless steel composite pipe adopts the process route of hot pressing brazing and 2 times hot isostatic pressing treatment. The main steps include ...

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Abstract

The invention belongs to the technical field of a preparation method for a metal composite material and particularly relates to a preparation method for an aluminum-stainless steel composite pipe for thermal control on a spacecraft. According to the method disclosed by the invention, a stress relief metal layer is prepared by adopting a hot isostatic pressing process, and the aluminum-stainless steel composite pipe is prepared by adopting a method of hot-pressing soldering and then hot isostatic pressing treatment. The method disclosed by the invention comprises the following steps: (1) performing modified treatment on the outer surface of a stainless steel pipe; (2) manufacturing the stress relief metal layer; (3) preparing a brazing material; (4) assembling the stainless steel pipe coated with the stress relief layer, an aluminum pipe and the brazing material; (5) performing hot-pressing brazing; (6) performing contour processing and vacuum canning on a brazed part; (7) performing hot isostatic pressing treatment; (8) performing canning removal and contour processing. The aluminum-stainless steel composite pipe manufactured by the method disclosed by the invention has the characteristics of being high in straightness, light, vibration-proof, high in heat-transfer capability and the like, and the thermal environment adaptability and the mechanical vibration mechanics adaptability of the aluminum-stainless steel composite pipe meet the operating requirements of thermal control systems, such as spacecraft flexible heat pipes, single-phase and two-phase liquid heat-transfer loops and expandable thermal radiators.

Description

technical field [0001] The invention belongs to the technical field of preparation methods of metal composite materials, and in particular relates to a preparation method of an aluminum-stainless steel composite pipe for thermal control of space vehicles. Background technique [0002] For the flexible heat pipes, single-phase and two-phase liquid heat transfer circuits, expandable heat radiators and other thermal control systems used in space vehicles, the working medium circulation pipelines and storage containers are made of stainless steel based on considerations of strength and corrosion resistance. material. At the same time, in the area of ​​heat collection (evaporation of heat transfer medium) and heat dissipation (condensation of heat transfer medium), based on the consideration of heat transfer performance and weight, the aluminum material expansion box with light weight, good heat transfer performance and large specific heat capacity is selected in the design. hot...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P15/00
CPCB23K1/00B23K1/20B23K1/206B23K2101/06B23P15/00
Inventor 陆艳杰张小勇苗建印林晨光张红星李新成
Owner GENERAL RESEARCH INSTITUTE FOR NONFERROUS METALS BEIJNG