High-temperature alloy mandrel applied to planetary rolling mill for rolling copper and copper alloy and preparation method thereof

A high-temperature alloy and planetary rolling mill technology, applied in metal processing equipment, cores, manufacturing tools, etc., can solve the problems of high hardness and strength of copper alloy, easy sticking of copper on the outer surface of the mandrel, and low heat dissipation efficiency of the mandrel, etc., to achieve Increase heat corrosion resistance, low probability of copper sticking phenomenon, and good comprehensive mechanical properties

Active Publication Date: 2020-12-15
JIANGSU LONGDA SUPERALLOY MATERIAL CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, in the actual production process, the planetary rolling mill has matured the copper tube rolling process, and the mandrel adopts H13 material and domestic Y4 material, which can meet the use requirements.
When rolling copper alloys, the requirements for mandrels are higher, and the more mature ones are used for the rolling of brass tubes, but the service life of the supporting mandrels is still low, while for other copper alloys such as white copper tubes The rolling mandrel of the pipe is more demanding
Mandrels made of materials such as H13 and Y4 generate a lot of heat during the rolling process, and the temperature rises sharply, causing the outer surface of the mandrel to stick to copper. Especially when rolling copper alloys, due to the high rolling temperature, the sticking The copper is extremely serious, and the outer surface of the mandrel needs to be ground every time one is rolled, which seriously affects the production efficiency
And the sticking copper part is the stress point of rolling, and the damage at this stress point is more serious. The main reasons for the serious damage are: (1) The temperature rises rapidly during the copper alloy rolling process, and the hardness and strength of the copper alloy (2) The hardness of the mandrel material at high temperature is low; (3) The fatigue performance at high temperature is poor; (4) The heat dissipation efficiency of the mandrel is low

Method used

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  • High-temperature alloy mandrel applied to planetary rolling mill for rolling copper and copper alloy and preparation method thereof
  • High-temperature alloy mandrel applied to planetary rolling mill for rolling copper and copper alloy and preparation method thereof
  • High-temperature alloy mandrel applied to planetary rolling mill for rolling copper and copper alloy and preparation method thereof

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Experimental program
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Effect test

Embodiment 1

[0028] It includes a sizing belt 1, a guide cone 2, an external thread 3, a cooling hole 4 and an internal thread 5; the front end of the sizing belt 1 is provided with a guide cone 2, and the end is provided with an external thread 3; There are cooling holes 4, and internal threads 5 are arranged along the cooling holes 4.

[0029] The mandrel provided by the invention has a sizing band length of 145-155mm, a circular threaded part of 30-40mm, and a truncated conical guide cone part of 10-20mm, and the cooling hole runs through the whole mandrel such as figure 1 shown. The surface of the mandrel cooling hole is processed with internal threads, which increases the heat dissipation during the rolling process, thereby increasing the service life of the mandrel. In the center of the mandrel sizing zone, the wall thickness of 2-4cm does not process the internal thread.

[0030] The mandrel provided by the invention is used for rolling copper ingots of various copper and copper a...

Embodiment 2

[0032] A method for preparing a high-temperature alloy mandrel applied to a planetary rolling mill for rolling copper and copper alloys, the steps are as follows:

[0033] (1) Vacuum melting: In terms of mass percentage, take Cr 12.7%, Mo 4.5%, Al 6%, Ti 0.75%, Nb 2.3%, the rest is Ni, and add control trace elements B 0.012%, C 0.14%, Zr 0.12%, smelting under vacuum not higher than 5MPa, casting temperature is 1480℃, to prepare superalloy master alloy;

[0034] (2) Investment casting: The master alloy prepared in step (1) is removed from the riser, and the outer surface is ground to remove scale as the secondary melting raw material for investment casting; it is remelted and cast into the mold shell by vacuum induction melting to prepare For blanks close to the size of the mandrel, the mold shell is baked at 850°C and held for 3 hours; the refining temperature is 1510°C, the casting temperature is 1430°C, the melting vacuum is not higher than 5MPa, and the melting time is 30 m...

Embodiment 3

[0039] (1) Vacuum smelting: by weight percentage, take Cr 12.5%, Mo 4.2%, Al 6.2%, Ti 0.8%, Nb 2.2%, the rest is Ni, and the rest is Ni, and add control trace elements B 0.015%, C 0.12%, Zr 0.12%, smelting under vacuum not higher than 5MPa, casting temperature is 1490℃, to prepare superalloy master alloy;

[0040] (2) Investment casting: The master alloy prepared in step (1) is removed from the riser, and the outer surface is ground to remove scale as the secondary melting raw material for investment casting; it is remelted and cast into the mold shell by vacuum induction melting to prepare For billets close to the size of the mandrel, the mold shell baking temperature is 1000°C, and the heat preservation is 3h; the refining temperature is 1530°C, the casting temperature is 1430°C, the melting vacuum degree is not higher than 5MPa, and the melting time is 20min;

[0041] (3) Hot isostatic pressing treatment: hot isostatic pressing treatment is performed on the casting prepared...

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Abstract

The invention relates to a high-temperature alloy core rod applied to planetary rolling mill for rolling copper and copper and a preparation method of the high-temperature alloy core rod, and belongsto the technical field of metal machining. The high-temperature alloy core rod comprises 11.50-14.00% of Cr, 3.80-5.2% of Mo, 5.50-6.50% of Al, 0.50-1.00% of Ti, 1.80-2.80% of Nb and Ta, 0.005-0.020%of B, 0.08-0.20% of C, 0.050-0.20% of Zr, 0-0.50% of Si, 0-0.50% of Mn, 0-0.015% of P, 0-0.015% of S, 0-2.50% of Fe and the balance Ni. In the preparation process, a mother alloy cast ingot is prepared through vacuum induction smelting, vacuum induction remelting is carried out, a high-temperature alloy core rod blank is prepared through investment casting, the blank is subjected to hot isostaticpressure treatment and subsequent heat treatment, then the blank is polished and subjected to finish machining, and finally the core rod is subjected to surface aluminizing treatment to improve the surface hardness and corrosion resistance at high temperature. The high-temperature alloy core rod prepared through the preparation method has relatively high comprehensive mechanical property, long infatigue life and high in high-temperature strength, the service life of a die is obviously prolonged, the preparation process is simple, and the process is short.

Description

technical field [0001] The invention relates to a high-temperature alloy mandrel used for rolling copper and copper alloys in a planetary rolling mill and a preparation method thereof, belonging to the technical field of metal processing. Background technique [0002] The technology of rolling hollow copper and copper alloy ingots in a three-roll planetary rolling mill is a technical method for efficiently preparing copper and copper alloy pipes. Compared with the technology of preparing statistical copper alloy pipes by hot extrusion, the technology of rolling hollow copper ingots by planetary rolling mill has the following advantages: (1) high yield; (2) significantly improved production efficiency; (3) low production cost and energy saving effect Obviously; (4) It can prepare short tubes, long tubes, small and large copper and copper alloy tubes. [0003] However, in the actual production process, the planetary rolling mill has matured the copper tube rolling process, an...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22C1/02C22C19/05B22C9/04C22F1/10C23C10/48
CPCB22C9/04C22C1/023C22C19/056C22F1/10C23C10/48
Inventor 李华兵王颜臣李淑苹
Owner JIANGSU LONGDA SUPERALLOY MATERIAL CO LTD
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