Forging method of nickel-based high-temperature alloy annular part

A technology of nickel-based high-temperature alloy and ring parts, which is applied in the field of metal forging, can solve problems such as difficulty in forging ring rolling, failure to meet design requirements, and narrow ring forging temperature range, so as to reduce rolling deformation resistance and improve product mechanical properties , Improve the effect of forgeability

Active Publication Date: 2018-10-19
豪梅特航空机件(苏州)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Nickel-based superalloy materials are widely used, forging ring rolling is difficult, prone to cracking and mechanical performance test results do not meet the design requirements
The existing forging methods have the following deficiencies: ①Limited by transfer time, preheating temperature, etc., the ring forging temperature range is narrow, and the rolled ring products are severely cracked and lead to scrapping; ②The existing ring rolling technology has no understanding of the ring forging temperature design Comprehensive, adopting the traditional method of gradually cooling down from high-temperature ring rolling to low-temperature ring rolling will affect the transformation of the product structure, resulting in the macroscopic manifestation that the comprehensive room temperature tensile properties of the product cannot meet the design requirements

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0020] A method for forging a nickel-based superalloy ring, comprising the steps of:

[0021] (1) Cutting: cutting and chamfering the nickel-based superalloy material;

[0022] (2) Punching step: use a high-temperature gas furnace to heat the billet to 1026°C, keep it warm for 3 hours, then take the billet out of the high-temperature gas furnace and transport it to the press, and control the transfer time within 30 seconds; Upsetting and punching round holes, the operation time is completed within 180 seconds;

[0023] (3) High-temperature ring forging and rolling steps: evenly smear an insulating coating on the punched ring, and the thickness of the insulating coating is 0.5mm; use a high-temperature gas furnace to heat the punched ring to 1026°C, keep warm for 3 hours, then take out the ring piece from the high-temperature gas furnace and transfer it to the cerclage machine. The transfer time is controlled within 30 seconds; the ring piece is rolled in a straight ring, and ...

Embodiment 2

[0028] A method for forging a nickel-based superalloy ring, comprising the steps of:

[0029] (1) Cutting: cutting and chamfering the nickel-based superalloy material;

[0030] (2) Punching step: use a high-temperature gas furnace to heat the billet to 1040°C, keep it warm for 1.5 hours, then take the billet out of the high-temperature gas furnace and transport it to the press, and control the transfer time within 30 seconds; Upsetting and punching round holes, the operation time is completed within 180 seconds;

[0031] (3) High-temperature ring forging and rolling steps: evenly smear an insulating coating on the punched ring, and the thickness of the insulating coating is 0.5mm; use a high-temperature gas furnace to heat the punched ring to 1040°C, keep warm for 2 hours, then take out the ring piece from the high-temperature gas furnace and transfer it to the cerclage machine. The transfer time is controlled within 30 seconds; the ring piece is rolled in a straight ring, an...

Embodiment 3

[0036] A method for forging a nickel-based superalloy ring, comprising the steps of:

[0037] (1) Cutting: cutting and chamfering the nickel-based superalloy material;

[0038] (2) Punching step: use a high-temperature gas furnace to heat the billet to 1054°C, keep it warm for 3.5 hours, then take the billet out of the high-temperature gas furnace and transport it to the press, and control the transfer time within 30 seconds; Upsetting and punching round holes, the operation time is completed within 180 seconds;

[0039] (3) High-temperature ring forging and rolling steps: apply an insulating coating evenly on the punched ring, the thickness of which is 0.48 mm; use a high-temperature gas furnace to heat the punched ring to 1054°C, keep warm for 2 hours, then take out the ring piece from the high-temperature gas furnace and transfer it to the cerclage machine. The transfer time is controlled within 30 seconds; the ring piece is rolled in a straight ring, and the rolling amoun...

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Abstract

The invention discloses a forging method of a nickel-based high-temperature alloy annular part. The method comprises following steps of discharging, punching, high-temperature ring forging rolling, relative low-temperature ring forging rolling, temperature rising high-temperature ring forging rolling, and low-temperature circle checking shaping. Through the above manner, the surface of the annularpart is coated with a heat preservation coating, in the rolling process, the temperature of the annular part is ensured, meanwhile, rolling deformation resistance can be reduced, forging of the annular part is improved, and the roundness error, the cracking and the like appearing in the forging process can be effectively reduced. The technology processes of high-temperature ring forging-process relative low-temperature rolling-temperature rising high-temperature ring forging-final relative low-temperature circle checking shaping are adopted, the product structure can be effectively convertedand controlled to be optimal, the cross section room temperature stretching property of the forging part meets the design need, the full cross section mechanical property of the part is evenly distributed, the product mechanical property is improved, and the part size precision is ensured.

Description

technical field [0001] The invention relates to the technical field of metal forging, in particular to a method for forging a nickel-based superalloy ring piece. Background technique [0002] Nickel-based superalloy materials are widely used, but forging ring rolling is difficult, prone to cracking and mechanical performance test results do not meet the design requirements. The existing forging methods have the following deficiencies: ①Limited by transfer time, preheating temperature, etc., the ring forging temperature range is narrow, and the rolled ring products are severely cracked and lead to scrapping; ②The existing ring rolling technology has no understanding of the ring forging temperature design Comprehensively, adopting the traditional method of gradually cooling from high-temperature ring rolling to low-temperature ring rolling will affect the transformation of the product structure, resulting in the macroscopic manifestation that the comprehensive room temperature...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21J5/08B21J5/10B21H1/06B21C37/00
CPCB21H1/06B21J5/002B21J5/08B21J5/10
Inventor 陈小杰宋利冰黄震杨超
Owner 豪梅特航空机件(苏州)有限公司
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