GH4169 high-temperature alloy special-cross-section large annular piece liquid forging and rolling composite forming method

A GH4169, liquid die forging technology, applied in metal rolling and other directions, can solve the problems that the comprehensive mechanical properties of metal rings cannot meet the requirements of use, the processing requirements of complex cross-section rings, and the decline of comprehensive mechanical properties of rings. Achieve the effect of shortening preparation time, improving material utilization, improving productivity and economic benefits

Inactive Publication Date: 2012-09-26
SOUTHWEST UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004]1) The process is lengthy, with many procedures and low production efficiency;
[0005]2) The rolled and expanded ring blank needs to be prepared by punching, and the final cross-sectional shape needs to be guaranteed by cutting excess dressing, so the material utilization rate is low;
[0006]3) The machining process cuts off the metal flow line, resulting in a decrease in the comprehensive mechanical properties of the ring;
[0007]4) The preparation process requires repeated heating, resulting in coarse grains, severe surface oxidation, and large energy consumption
[0008]The

Method used

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Examples

Experimental program
Comparison scheme
Effect test

no. 1 example

[0037] The liquid die forging and rolling composite forming method of the GH4169 superalloy large ring with different cross-sections in this embodiment includes the following steps:

[0038] 1) Melting: The triple smelting process of vacuum induction + electroslag remelting + vacuum consumable remelting is adopted. Specifically, the vacuum consumable remelting process adopts double cooling of water and helium, which can effectively reduce the segregation of Nb metal;

[0039] 2) Liquid die forging: After fixing the liquid die forging die on the indirect squeeze casting machine, quantitatively pour the alloy solution obtained in step 1) into the liquid die forging die at a pouring temperature of 1400 °C and a pressurization speed of 40 mm / s, the filling time is 5 s, the specific pressure is 350 MPa, and the pressure is maintained at this pressure for 90 s to obtain a ring billet with a near-end cross-section. The specific pressure refers to the unit pressure that the liquid meta...

no. 2 example

[0063] The liquid die forging and rolling composite forming method of the GH4169 superalloy large ring with different cross-sections in this embodiment includes the following steps:

[0064] 1) Melting: The triple smelting process of vacuum induction + electroslag remelting + vacuum consumable remelting is adopted. Specifically, the vacuum consumable remelting process adopts double cooling of water and helium, which can effectively reduce the segregation of Nb metal;

[0065] 2) Liquid die forging: After fixing the liquid die forging die on the indirect squeeze casting machine, quantitatively pour the alloy solution obtained in step 1) into the liquid die forging die at a pouring temperature of 1350 °C and a pressurization speed of 35 mm / s, the filling time is 1 s, the specific pressure is 400MPa, and the pressure is maintained at this pressure for 35 s to obtain a ring billet with a near-end cross-section. The specific pressure refers to the unit pressure that the liquid meta...

no. 3 example

[0080] The liquid die forging and rolling composite forming method of the GH4169 superalloy large ring with different cross-sections in this embodiment includes the following steps:

[0081] 1) Melting: The triple smelting process of vacuum induction + electroslag remelting + vacuum consumable remelting is adopted. Specifically, the vacuum consumable remelting process adopts double cooling of water and helium, which can effectively reduce the segregation of Nb metal;

[0082] 2) Liquid die forging: After fixing the liquid die forging die on the indirect squeeze casting machine, quantitatively pour the alloy solution obtained in step 1) into the liquid die forging die at a pouring temperature of 1380 °C and a pressurization speed of 38mm / s, the filling time is 6 s, the specific pressure is 370MPa, and the pressure is maintained at this pressure for 50s to obtain a ring blank with a near-end cross-section. The specific pressure refers to the unit pressure that the liquid metal i...

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Abstract

The invention discloses a GH4169 high-temperature alloy special-cross-section large annular piece liquid forging and rolling composite forming method which comprises the following steps: 1) smelting; 2) liquid forging: fixing a liquid forging mold on an indirect squeezing casting machine, pouring an alloy solution in constant volume into the liquid forging mold, wherein the pouring temperature is 1350-1400 DEG C, the pressurization speed is 35-40mm/s, the type filling time is 1-6 seconds, and the specific pressure is 350-400MPa; and keeping the pressure under the pressure for 35-90 seconds, thereby obtaining a near terminal cross section annular blank; 3) homogenizing: cooling the near terminal cross section annular blank to 1150-1160 DEG C, performing heat preservation for 20-30 hours, then rising the temperature to 1180-1190 DEG C, and performing heat preservation for 110-130 hours; 4) residue heat isothermal rolling: reducing the temperature of the near terminal cross section annular blank after homogenization to 1010-1120 DEG C, and carrying out residue heat constant temperature rolling on a radial and axial composite rolling annular machine; 5) heat treatment: performing heat preservation on the annular blank at a temperature of 715-725 DEG C for 8 hours, and then cooling to 615-625 DEG C in a furnace at a speed of 50 DEG C/h, performing heat preservation for 8 hours, and carrying out air cooling; and 6) finishing.

Description

technical field [0001] The invention relates to a short-process processing and forming method for large-diameter metal rings with complex cross-sections, in particular to a liquid die forging and rolling composite forming method for large-scale rings of GH4169 superalloy with different cross-sections. Background technique [0002] The special-shaped large ring parts of aero-engines or gas turbines made of GH4169 superalloy, such as parts such as brakes, have a harsh working environment. The special use environment puts forward almost strict requirements on the dimensional accuracy and comprehensive mechanical properties of the ring parts: on the one hand, the parts are required to have high-precision external dimensions to avoid subsequent machining, which wastes a lot of manpower and material resources and seriously reduces the performance of the ring parts. ; On the other hand, the parts are required to have an excellent organizational state in order to meet the requiremen...

Claims

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Application Information

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IPC IPC(8): B23P15/00B22D18/02B21H1/06
Inventor 李路王放
Owner SOUTHWEST UNIVERSITY
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