CN118023447A - Guard ring forging and preparation method thereof - Google Patents
Guard ring forging and preparation method thereof Download PDFInfo
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- CN118023447A CN118023447A CN202410183435.8A CN202410183435A CN118023447A CN 118023447 A CN118023447 A CN 118023447A CN 202410183435 A CN202410183435 A CN 202410183435A CN 118023447 A CN118023447 A CN 118023447A
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- 238000005242 forging Methods 0.000 title claims abstract description 128
- 238000002360 preparation method Methods 0.000 title claims abstract description 19
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 67
- 239000010959 steel Substances 0.000 claims abstract description 67
- 238000000034 method Methods 0.000 claims abstract description 19
- 238000003723 Smelting Methods 0.000 claims abstract description 16
- 238000001816 cooling Methods 0.000 claims abstract description 12
- 238000004519 manufacturing process Methods 0.000 claims abstract description 12
- 238000005422 blasting Methods 0.000 claims abstract description 4
- 238000010438 heat treatment Methods 0.000 claims description 31
- 229910052757 nitrogen Inorganic materials 0.000 claims description 22
- 229910001566 austenite Inorganic materials 0.000 claims description 19
- 238000004321 preservation Methods 0.000 claims description 13
- 229910052804 chromium Inorganic materials 0.000 claims description 10
- 229910052759 nickel Inorganic materials 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 238000004080 punching Methods 0.000 claims description 8
- 150000004767 nitrides Chemical class 0.000 claims description 7
- 229910052698 phosphorus Inorganic materials 0.000 claims description 7
- 229910052717 sulfur Inorganic materials 0.000 claims description 7
- 229910052748 manganese Inorganic materials 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 238000007599 discharging Methods 0.000 claims description 5
- 229910052758 niobium Inorganic materials 0.000 claims description 5
- 229910052720 vanadium Inorganic materials 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 229910052802 copper Inorganic materials 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 4
- 238000009792 diffusion process Methods 0.000 claims description 2
- 239000011651 chromium Substances 0.000 description 27
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 24
- 239000000306 component Substances 0.000 description 22
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 19
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 17
- 239000000243 solution Substances 0.000 description 16
- 238000005260 corrosion Methods 0.000 description 15
- 230000007797 corrosion Effects 0.000 description 15
- 229910045601 alloy Inorganic materials 0.000 description 14
- 239000000956 alloy Substances 0.000 description 14
- 230000000052 comparative effect Effects 0.000 description 14
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- 239000011572 manganese Substances 0.000 description 12
- 239000010955 niobium Substances 0.000 description 11
- 238000001556 precipitation Methods 0.000 description 11
- 230000008569 process Effects 0.000 description 11
- 238000005728 strengthening Methods 0.000 description 11
- 239000006104 solid solution Substances 0.000 description 10
- 230000002829 reductive effect Effects 0.000 description 9
- 238000007670 refining Methods 0.000 description 9
- 229910000859 α-Fe Inorganic materials 0.000 description 9
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 8
- 238000000265 homogenisation Methods 0.000 description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 7
- 230000000694 effects Effects 0.000 description 7
- 238000011160 research Methods 0.000 description 7
- 229910001220 stainless steel Inorganic materials 0.000 description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 5
- 238000005266 casting Methods 0.000 description 5
- 239000011159 matrix material Substances 0.000 description 5
- 230000000087 stabilizing effect Effects 0.000 description 5
- 239000010935 stainless steel Substances 0.000 description 5
- 238000005482 strain hardening Methods 0.000 description 5
- 229910052786 argon Inorganic materials 0.000 description 4
- 238000005336 cracking Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 4
- 238000003756 stirring Methods 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 3
- 229910052593 corundum Inorganic materials 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000011056 performance test Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000010079 rubber tapping Methods 0.000 description 3
- 239000002893 slag Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- 229910001845 yogo sapphire Inorganic materials 0.000 description 3
- 229910004261 CaF 2 Inorganic materials 0.000 description 2
- GJPVPJBNBCITNZ-UHFFFAOYSA-N [N].[Mn].[Cr] Chemical compound [N].[Mn].[Cr] GJPVPJBNBCITNZ-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 238000007664 blowing Methods 0.000 description 2
- BQKCOFRVVANBNO-UHFFFAOYSA-N chromium manganese Chemical compound [Cr][Mn][Cr] BQKCOFRVVANBNO-UHFFFAOYSA-N 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- -1 manganese metal nitride Chemical class 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 2
- 229910000742 Microalloyed steel Inorganic materials 0.000 description 1
- 206010070834 Sensitisation Diseases 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 241001062472 Stokellia anisodon Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000008358 core component Substances 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000016507 interphase Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/06—Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
- B21J5/08—Upsetting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/06—Methods for forging, hammering, or pressing; Special equipment or accessories therefor for performing particular operations
- B21J5/10—Piercing billets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K1/00—Making machine elements
- B21K1/76—Making machine elements elements not mentioned in one of the preceding groups
- B21K1/761—Making machine elements elements not mentioned in one of the preceding groups rings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
- B21K29/00—Arrangements for heating or cooling during processing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/40—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for rings; for bearing races
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/04—Making ferrous alloys by melting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
The invention discloses a guard ring forging and a preparation method thereof, belongs to the technical field of guard ring forging manufacture, and solves the problem of insufficient base yield strength of the guard ring forging in the prior art. The preparation method of the guard ring forging comprises the following steps: step 1: smelting an electrode blank and electroslag remelting a steel ingot, and peeling; step 2: homogenizing the steel ingot; step 3: forging and cogging the steel ingot, and blasting air for cooling after forging; step 4: and carrying out solution treatment on the forging stock to obtain the guard ring forging. The guard ring forging prepared by the method has excellent strength after hot forging and solution treatment.
Description
Technical Field
The invention relates to the technical field of manufacturing of guard ring forgings, in particular to a guard ring forgings and a preparation method thereof.
Background
The guard ring forging is a core component of the generator set, belongs to a large thin-wall ring forging, and is characterized in that materials are required to be nonmagnetic at two ends of the generator set, and an austenitic stainless steel forging is usually adopted. Because of the austenitic structure of such steels, the strength cannot be increased by heat treatment, usually by work hardening, which occurs during cold deformation or warm forging, the strength of the material is greatly increased by sacrificing part of the plasticity. In the engineering production process, along with the increasing demand on the size of the forging products, especially the production of large-scale forging, the large-scale equipment, the space field and the special die are needed for cold deformation or warm forging deformation, and the manufacturing period and the production cost are influenced. In order to reduce the deformation amount of the work hardening or to eliminate the need for the work hardening by cold deformation or semi-hot forging, it is an urgent problem to provide a grommet forging that can obtain a high base yield strength (for example, after hot forging or solution treatment).
Disclosure of Invention
In view of the above, the invention aims to provide a guard ring forging and a preparation method thereof, which are used for solving the problem of insufficient basic yield strength of the existing guard ring forging.
The aim of the invention is mainly realized by the following technical scheme:
the invention provides a preparation method of a guard ring forging, which comprises the following steps:
Step 1: smelting an electrode blank and electroslag remelting a steel ingot, and peeling;
Step 2: homogenizing the steel ingot;
step 3: forging and cogging the steel ingot, and blasting air for cooling after forging;
step 4: and carrying out solution treatment on the forging stock to obtain the guard ring forging.
Further, in step2, the homogenization treatment includes the following steps:
S201, heating the steel ingot to 600-650 ℃ for heat preservation, and performing heat preservation according to 1-1.2 h/100 mm;
S202, heating to 800-850 ℃, and carrying out heat preservation according to 1-1.2 h/100 mm;
S203, heating to 1150-1180 ℃, and performing heat preservation according to 2-3 h/100 mm; wherein the temperature rise rate in S202 is smaller than the temperature rise rate in S203.
Further, in S202, the temperature rise rate is 40 ℃/h or less.
Further, in S203, the temperature rise rate is 70 ℃/h or more.
Further, in the step 3, forging cogging is completed through lightly drawing, upsetting and drawing, punching and reaming of the ingot body.
In step 3, the forging temperature of the forging cogging process of the light ingot body drawing, upsetting and drawing is 1150-1180 ℃.
Further, in step 4, the solution treatment includes: and (3) charging the forging stock into a furnace at the furnace temperature of less than or equal to 500 ℃ and rapidly heating to 1080-1100 ℃, preserving heat according to 2-2.5 h/100mm, discharging and cooling with water.
Further, the components of the guard ring forging piece comprise the following components in percentage by mass :C0.08%~0.11%,Si 0.40%~1.2%,Mn 18.5%~21.0%,Cr 18%~19.5%,Ni 0.5%~3%,V0.35%~0.95%,N 0.68%~0.75%,Nb 0.005%~0.03%,Cu≤0.01%,Al
Less than or equal to 0.01 percent, less than or equal to 0.010 percent of P, less than or equal to 0.010 percent of S, and the balance of Fe and unavoidable trace impurities.
The invention also provides a guard ring forging, which is prepared by adopting the preparation method.
Further, the microstructure of the guard ring forging piece is austenite and nitride which is dispersed, the grain size reaches more than 6 levels, and the grains are uniform.
Compared with the prior art, the invention can at least realize one of the following beneficial effects:
a) According to the preparation method of the guard ring forging, smelting, forging and solution treatment are adopted, the steps of homogenization treatment and parameters of each step are accurately controlled, the basic strength of the guard ring forging can be obviously improved by combining with the accurate control of forging technological parameters, the deformation of the guard ring forging for processing and strengthening can be reduced, and even the processing and strengthening can meet the performance use requirements without cold deformation or warm forging deformation, and the manufacturing procedures and cost are reduced.
B) According to the guard ring forging, the solid solution strengthening effect of the alloy is improved by accurately controlling the contents of carbon, silicon, vanadium, niobium and nickel; and through cooperatively controlling manganese and chromium, the epsilon-phase precipitation temperature is controlled by matching with other alloy elements, so that hot forging cracks are reduced; in addition, the solid solubility of nitrogen in the matrix can be improved under normal pressure smelting by adding each alloy element, so that the nitrogen content in normal pressure smelting can reach more than 0.68%; by accurately controlling the content of O, S, P, al, the content of inclusions in the alloy is reduced, the purity of the alloy can be improved, the occurrence probability of hot forging cracks is reduced, and the uniformity of crystal grains and the precipitation and distribution of crystal boundaries are ensured.
C) The components of the guard ring forging are favorable for forming dispersed nitrides in an austenitic structure, and play a role in refining grains and improving the strength of a matrix.
D) The guard ring forging of the present invention is excellent in strength after hot forging and solution treatment, for example, the performance of a forging stock is as follows: the tensile strength σ b is 950MPa or more, for example 956 to 1110MPa; the yield strength sigma 0.2 is more than 690MPa, for example 690-840 MPa; the elongation is more than 35%, such as 35% -46%; the surface shrinkage is more than 60%, for example 60% -69%; the impact energy is 56J or more, for example, 56 to 135J. The properties after solid solution were as follows: the tensile strength sigma b is more than 920MPa, for example, 920-984 MPa; the yield strength sigma 0.2 is more than 620MPa, for example, 620-675 MPa; the elongation is more than 38%, such as 38% -52%; the surface shrinkage is more than 59%, for example, 59% -70%; the impact energy is 70J or more, for example, 70 to 138J.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and drawings.
Drawings
The drawings are only for purposes of illustrating particular embodiments and are not to be construed as limiting the invention, like reference numerals being used to refer to like parts throughout the several views.
FIG. 1 is a grain size of a guard ring forging of example 1 after solution treatment;
FIG. 2 is a microstructure of the guard ring forging of example 1 after solution treatment;
FIG. 3 is a schematic diagram of a heating curve of homogenization treatment in a manufacturing method of a shroud ring forging.
Detailed Description
Preferred embodiments of the present invention are described in detail below with reference to the attached drawing figures, which form a part of the present invention and are used in conjunction with embodiments of the present invention to illustrate the principles of the present invention.
The invention provides a preparation method of a guard ring forging, which comprises the following steps:
Step 1: smelting an electrode blank and electroslag remelting a steel ingot, and peeling;
Step 2: homogenizing the steel ingot;
step 3: forging and cogging the steel ingot, and blasting air for cooling after forging;
step 4: and carrying out solution treatment on the forging stock to obtain the guard ring forging.
Specifically, in the step 1, an arc furnace is adopted to smelt and cast an electrode blank, and then an electroslag remelting smelting mode is adopted to obtain a steel ingot. In the step 1, normal pressure smelting is adopted.
Specifically, in the step 1, the arc furnace smelting and casting electrode blank may include the following steps: refining molten steel in an arc furnace; refining molten steel in a refining ladle, adjusting alloy components, performing VOD operation, blowing nitrogen and stirring, adding manganese metal nitride to adjust N in batches, adjusting N by utilizing Cr metal nitride in the residual insufficient mode, and finally adjusting manganese and chromium by using manganese metal and chromium metal; stirring the components after the components are qualified by argon, wherein the tapping temperature is 1460-1490 ℃; and (5) pouring the electrode blank under the protection of argon.
Specifically, in the step 1, the electroslag remelting may include the following steps: and (3) electroslag remelting a group of electrode blanks in a crystallizer, wherein 20-40% of CaF 2 50%~70%,Al2O3 and 0-20% of CaO are selected for slagging, and the melting speed of the electroslag remelting is 0.8-1.2T/h.
Specifically, in the step 1, the surface of the steel ingot needs to be peeled, and surface cracks and slag skin are removed.
Specifically, in the step 2, the homogenization treatment includes the following steps:
s201, heating the steel ingot to 600-650 ℃, and performing heat preservation according to 1-1.2 h/100 mm;
S202, raising the temperature to 800-850 ℃ at a heating rate below 40 ℃/h for the first time, and performing heat preservation according to 1-1.2 h/100 mm;
s203, heating to 1150-1180 ℃ at a speed of not less than 70 ℃ per hour for the second time, and homogenizing at a speed of 2-3 h/100 mm.
As shown in fig. 3, in step 2, the heating temperature rise curve is exemplified by a steel ingot diameter of 1000 mm.
Specifically, in S202, considering that the low-temperature heat conduction of the high-nitrogen austenitic stainless steel is small, the steel ingot is slowly transferred from the outer surface to the core, and the phenomenon that the temperature difference in the steel ingot is large, internal tensile stress is generated and steel ingot cracking is easily caused due to the fact that the temperature rising rate is too fast is avoided; the temperature rising rate is properly reduced, so that the temperature uniformity of the steel ingot after the first temperature rising can be ensured, and the generation of cracks is avoided, and therefore, the temperature rising rate is controlled to be lower than 40 ℃/h, for example, 30-40 ℃/h.
Specifically, in S203, after the heat preservation at 800-850 ℃ is completed, the internal and external temperatures of the steel ingot are uniform, and the temperature is continuously raised because of good high-temperature plasticity, even if the temperature difference exists between the internal and external temperatures in the temperature raising process, the influence of temperature stress is not worried, and the rapid temperature raising can be performed. In addition, the high-nitrogen austenitic stainless steel can quickly pass through a sensitive temperature range in which brittle phases are separated out, so that the brittle phases in the high-nitrogen austenitic stainless steel are reduced, the plasticity of the stainless steel is improved, and surface cracks or edge cracks generated in the hot working process are reduced. Therefore, the temperature rise rate is 70 ℃ per hour or more, for example, 70 to 100 ℃ per hour.
Specifically, in the step 2, the homogenization treatment is performed at 1150-1180 ℃ for a long time to melt back the harmful phase in the solidification process of the steel ingot, and the alloy elements which are easy to segregate are diffused at high temperature. Therefore, the heat preservation is carried out for homogenization treatment according to the speed of 2 to 3 hours per 100 mm.
Specifically, in the step 3, since cracking and overheating and overburning of the grain boundaries are likely to occur in consideration of the precipitation temperature of the high-temperature hazardous phase δ, the initial forging temperature is controlled to 1150 to 1180 ℃. In addition, the final forging temperature is controlled to 950 ℃ or higher, for example, 960 to 970 ℃ in consideration of precipitation of a low-temperature harmful phase epsilon, poor low-temperature plasticity, deformation resistance to elongation and the like.
Specifically, in the step 3, forging cogging is completed through light drawing, upsetting and drawing, punching and reaming of the ingot body. The forging and cogging process of lightly drawing and upsetting the ingot body is carried out at 1150-1180 ℃ and the forging and cogging process of punching and reaming is carried out at 1100-1150 ℃. The final forging temperature is controlled above 950 ℃.
Specifically, in the step 3, considering that the guard ring forging of the invention has poor high-temperature plasticity, the forging temperature interval is narrow, and the cracking tendency is serious; and carrying out thermal deformation in a mode of multiple times and small deformation. Considering that the deformation is too large, the alloy grain structure has the risk of mixed crystals in a large deformation area and also has the risk of cracking; if the deformation is too small, the alloy is insufficiently deformed, and the purpose of grain breakage and recrystallization cannot be achieved. Therefore, the deformation amount of each upsetting is controlled to be 30-50%, and the deformation amount of each drawing is controlled to be 15-25%. The specific process of hot forging and the pass of deformation can be designed according to the final shape and size of the forging, and will not be described in detail here. After hot forging, air cooling is performed.
Specifically, in the step 4, the solution treatment includes: and (3) charging the forging stock into a furnace at the furnace temperature of less than or equal to 500 ℃ and rapidly heating to 1080-1100 ℃, preserving heat according to 2-2.5 h/100mm, discharging and cooling with water.
Specifically, in the step 4, the heating rate is 70 ℃/h or more.
Specifically, the components of the guard ring forging comprise :C0.08%~0.11%,Si 0.40%~1.2%,Mn 18.5%~21.0%,Cr 18%~19.5%,Ni0.5%~3%,V 0.35%~0.95%,N 0.68%~0.75%,Nb 0.005%~0.03%,Cu≤0.01%,Al≤0.01%,P≤0.010%,S≤0.010%, mass percent of Fe and unavoidable trace impurities as the balance.
The following is a specific description of the action and the selection of the amounts of the components contained in the invention:
N: n has strong solid solution strengthening capability, and the strength of the steel is continuously improved along with the increase of the content of N, but the fracture toughness is not obviously reduced; n is an austenite stabilizing element that inhibits the formation of ferrite and strain-induced martensite in the steel; in addition, N is very advantageous for improving the pitting resistance and the stress corrosion resistance of steel. However, since N is dissolved in austenite under normal pressure and influenced by the alloy components, the present invention ensures that the N content is 0.68% to 0.75% by the ratio of the alloy components.
Cr: cr is one of the most main alloying elements in austenitic stainless steel, cr is added into the high-nitrogen chromium manganese austenitic stainless steel and is dissolved into an iron matrix, so that the electrode potential of the matrix can be effectively improved, a Cr-rich oxide film is formed on the surface under the action of an oxidizing medium, and the anode reaction is prevented, so that the corrosion resistance of the austenitic stainless steel is improved; cr increases the solubility of C and decreases the depletion of Cr, so that it is advantageous to increase the Cr content for the intergranular corrosion resistance of austenitic stainless steel; cr can effectively improve the pitting corrosion resistance and crevice corrosion resistance of steel, and when N exists in the steel at the same time, the effectiveness of Cr is greatly enhanced. The increase in Cr content in austenitic stainless steel can decrease the martensitic transformation temperature (M s), thereby increasing the stability of the austenitic matrix. Therefore, it is difficult to obtain martensite even through cold working and low temperature treatment of the high-chromium austenitic stainless steel. However, the Cr content cannot be too high because Cr is an element that strongly forms/stabilizes ferrite, i.e., can reduce the austenite region. As the Cr content in the steel increases, a ferrite (δ) structure may appear in austenitic stainless steel. In austenitic stainless steels, as the Cr content increases, the propensity for formation of some intermetallic phases (e.g., sigma phases) increases, which also promotes the formation of χ phases if Mo is included in the steel. The precipitation of these intermetallic phases not only significantly reduces the plasticity and toughness of the steel, but also reduces the corrosion resistance of the steel under some conditions. While the stainless steel maintains a fully austenitic structure without delta ferrite formation, the mechanical properties are not significantly affected if the Cr content is only increased. Therefore, the invention is subjected to intensive research and the Cr content is controlled to be 18-19.5%.
Mn: in high nitrogen chromium manganese austenitic stainless steels, the element Mn acts primarily to stabilize austenite and increase the solubility of N. In Ni-saving stainless steel, mn is a very important alloying element and is mainly added to the steel in combination with an element forming austenite. Mn is a weak austenite forming element, but has a strong effect of stabilizing austenite, and Mn itself contributes little to improvement of corrosion resistance of steel. In order to increase the solubility of N, the Mn content is controlled to be 18.5-21.0%.
C: c is an element in the stainless steel which strongly forms, stabilizes and enlarges austenite region, and remarkably improves the strength of the austenitic stainless steel through interstitial solid solution strengthening. C can also improve the stress corrosion resistance of austenitic stainless steel in high concentration chlorides (e.g., 42% MgCl 2 boiling solution). However, C is also sometimes considered a detrimental element in austenitic stainless steel. For example, C may form high chromium M 23C6 type carbides with Cr in the steel, resulting in localized chromium depletion in the steel, degrading the corrosion resistance, particularly intergranular corrosion resistance, of the steel. Therefore, the content of C should be controlled as low as possible in the smelting process of austenitic stainless steel, and the increase of C on the surface of the stainless steel is prevented in the subsequent processes of heat treatment, cold working, heat treatment and the like, so as to avoid the precipitation of Cr carbide. Therefore, through intensive research, the content of C is controlled to be 0.08-0.11%, the strength of austenitic stainless steel is improved, and M 23C6 type carbide can be eliminated through solution treatment.
V: the atomic size of V is equivalent to that of Fe, the solid solubility is large, the addition amount is easy to control, and the V is insensitive to segregation bands. In high nitrogen chromium manganese austenitic stainless steel, V can play a role in nitrogen fixation because V has a strong affinity with nitrogen in the steel, the formation of V (C, N) greatly reduces the content of free N in the steel, and V mainly influences the structure and the performance of the steel by precipitating and separating out V (C, N). Can inhibit austenite recrystallization and prevent grain growth in the hot working process, thereby refining the grains and improving the strength and toughness of the steel. In addition, the strain timeliness of the steel can be effectively avoided. Nitrogen in the steel can enhance the strengthening effect of V. The more the nitrogen content in the steel increases, the more remarkable the V (C, N) precipitation strengthening effect is. At higher temperatures (above 1000 ℃), V (C, N) can dissolve in gamma-Fe, so vanadium is mainly inter-phase precipitation during gamma-alpha transformation and precipitation strengthening in ferrite. Through intensive research, the V content is controlled to be 0.35-0.95%.
Nb: since Nb has a larger atomic size than Fe and a larger diffusion coefficient in austenite, nb tends to be biased at high energy such as grain boundaries and dislocation lines. This produces a strong dragging effect on dislocation climb and grain boundary movement, inhibiting recrystallization nucleation, thereby increasing material recrystallization time. Nb is an austenite stabilizing element, and can form carbon/nitride with elements such as C/N in steel, thereby preventing or reducing the formation of M 23C6 carbide and preventing the generation of sensitization-state intergranular corrosion. The Nb compounds have high complete solid solution temperature, generally above 1100 ℃, and play roles in pinning dislocation and preventing grain boundary migration, and refine austenite grains. Generally, the larger the addition amount, the higher the complete solid solution temperature. Therefore, when the processing technology of Nb microalloyed steel is formulated, the solid solution quantity and precipitation quantity proportion of Nb and the size range of precipitated phase particles are strictly controlled, so that the effect of refining grains is achieved, and the Nb content is controlled to be 0.005% -0.03% by being used as microalloying elements through intensive research.
Si: si is an element that strongly forms ferrite. As the Si content increases, the ferrite content will increase, and the formation of intermetallic phases will also accelerate and increase. But an increase in Si will increase the yield strength. Through intensive research, the Si content is controlled to be 0.40% -1.2%.
Mo: some high-nitrogen chromium manganese austenitic stainless steel also usually contains a small amount of Mo, and the main effect of the Mo is to improve the resistance of the steel to corrosion of reducing medium, pitting corrosion, crevice corrosion and the like. However, mo is an element that forms and stabilizes ferrite and enlarges ferrite regions, and promotes the formation of intermetallic phases, so that plasticity and toughness of steel are lowered. Through intensive research, the addition of Mo element is strictly limited.
Ni: ni is an important alloy element in austenitic stainless steel, and has the main functions of forming and stabilizing austenite, improving the thermodynamic stability of the steel, and simultaneously, ni and Si can also jointly influence the precipitation temperature of high Wen-Fe; nickel and iron can be infinitely dissolved, and nickel enlarges the austenite region of iron and is a main alloy element for forming and stabilizing austenite. Nickel and carbon do not form carbide, nickel can improve the strength of steel, the plasticity and toughness of the steel are not affected, and the corrosion resistance of the steel can be improved. Although the nickel element can be replaced by increasing the N content in the high nitrogen steel, the N is increased to a certain extent by special modes such as pressurization and the like. Through intensive research, the content of Ni element is controlled to be 0.5% -3%.
P, S is used as a harmful element, and in consideration of actual manufacturing cost and technology, the invention is controlled to be less than or equal to 0.010 percent of P, less than or equal to 0.010 percent of S, simultaneously, the Cu content is controlled to be less than or equal to 0.010 percent, the Al content is strictly controlled, alN inclusion formed in high-nitrogen steel is prevented from being easily cracked in hot forging, and the Al content is required to be less than or equal to 0.010 percent.
In order to further improve the comprehensive performance of the guard ring forging, the constituents of the guard ring forging can be :C 0.09%~0.11%,Si 0.50%~1.2%,Mn18.5%~20.0%,Cr 18.5%~19.4%,Ni 0.5%~2.1%,V 0.40%~0.95%,N0.68%~0.75%,Nb 0.01%~0.03%,Cu≤0.006%,Al≤0.008%,P≤0.010%,S≤0.010%, percent by mass and the balance Fe and unavoidable trace impurities.
In order to further improve the comprehensive performance of the guard ring forging, the weight percentage of C in the components of the guard ring forging is as follows: 0.095% -0.11%.
In order to further improve the comprehensive performance of the guard ring forging, the components of the guard ring forging comprise the following Mn in percentage by mass: 18.6 to 19.5 percent.
In order to further improve the comprehensive performance of the guard ring forging, the components of the guard ring forging comprise the following Cr in percentage by mass: 18.7 to 19.2 percent.
In order to further improve the comprehensive performance of the guard ring forging, the components of the guard ring forging comprise the following Ni in percentage by mass: 0.5 to 2.1 percent.
The invention also provides the guard ring forging prepared by the method, the microstructure of the guard ring forging is austenite plus dispersed nitride, the grain size can reach more than 6 levels, for example, 6-9 levels, and the grains are uniform, for example, the grain size difference is less than 0.5 level.
Specifically, the guard ring forging has excellent strength after hot forging and solution treatment, and for example, the forging stock has the following properties: the tensile strength σ b is 950MPa or more, for example 956 to 1110MPa; the yield strength sigma 0.2 is more than 690MPa, for example 690-840 MPa; the elongation is more than 35%, such as 35% -46%; the surface shrinkage is more than 60%, for example 60% -69%; the impact energy is 56J or more, for example, 56 to 135J. The properties after solid solution were as follows: the tensile strength sigma b is more than 920MPa, for example, 920-984 MPa; the yield strength sigma 0.2 is more than 620MPa, for example, 620-675 MPa; the elongation is more than 38%, such as 38% -52%; the surface shrinkage is more than 59%, for example, 59% -70%; the impact energy is 70J or more, for example, 70 to 138J.
Specifically, the base strength of the guard ring forging after solution treatment can meet the use condition that the requirements on partial yield strength and tensile strength are not too high, and cold deformation or half hot forging strengthening is not needed. Even if cold deformation or semi-hot forging strengthening needs to be continued, the deformation rate is relatively small, and the cold deformation or semi-hot forging strengthening process is not described here.
Examples 1 to 4
Embodiments 1-4 of the invention provide a grommet forging and a method of making the same. The chemical composition of the examples is shown in Table 1. The microstructure of the grommet forgings of examples 1-4 is shown in table 2; FIG. 1 is a grain size of a guard ring forging of example 1 after solution treatment; fig. 2 shows the microstructure of the guard ring forging after solution treatment in example 1. The results of the primary performance measurements of the examples are shown in Table 3.
The preparation method of the example 1 comprises the following steps:
Step 1: smelting and casting an electrode blank by adopting an arc furnace, and then smelting 10000kg of steel ingot by adopting electroslag remelting;
The arc furnace smelting and casting electrode blanks can comprise the following steps: refining molten steel in an arc furnace; refining molten steel in a refining ladle, adjusting alloy components, performing VOD operation, blowing nitrogen and stirring, adding manganese metal nitride to adjust N in batches, adjusting N components to 0.7% by utilizing Cr metal nitride, and finally adjusting manganese and chromium by using manganese metal and chromium metal; stirring the components after the components are qualified by argon, wherein the tapping temperature is 1470 ℃; completing casting of the electrode blank under the protection of argon;
The electroslag remelting may include the steps of: electroslag remelting is carried out on a group of electrode blanks in a crystallizer, caF 260%,Al2O3 percent and CaO 20 percent are selected for slagging, and the melting speed of the electroslag remelting is 1T/h;
peeling the surface of the electroslag ingot to remove surface cracks and slag skin;
step 2: homogenizing the steel ingot:
s201, heating the steel ingot to 650 ℃, and preserving heat for 10 hours;
s202, heating to 850 ℃ at 30 ℃/h for the first time, and preserving heat for 10h;
s203, raising the temperature to 1180 ℃ at 80 ℃/h for the second time, and carrying out homogenization treatment at 30 h;
Step 3: forging and cogging the steel ingot, and heating, upsetting, drawing and deforming for many times, wherein the heating temperature is 1180 ℃ and the final forging temperature is 960 ℃; then punching and reaming are carried out, the initial forging temperature of the punching and reaming is 1150 ℃, the wall thickness of the guard ring forging stock after reaming is 240mm, and air cooling is carried out;
step 4: and (3) putting the forging stock into a 450 ℃ kiln, heating at 80 ℃/h, heating to 1080 ℃, preserving heat for 5h, discharging, and cooling with water to obtain the guard ring forging in a solid solution state.
The preparation method of example 2 is substantially the same as that of example 1, except that:
In step 2: homogenizing the steel ingot:
S201, heating the steel ingot to 600 ℃, and preserving heat for 10 hours;
s202, heating to 830 ℃ at 40 ℃/h for the first time, and preserving heat for 8h;
S203, heating to 1180 ℃ at 100 ℃/h for the second time, and carrying out homogenization treatment at 25h by heat preservation.
The preparation method of example 3 is substantially the same as that of example 1, except that:
Step 3: forging and cogging the steel ingot, and heating, upsetting, drawing and deforming for many times, wherein the heating temperature is 1160 ℃ and the final forging temperature is 950 ℃; then punching and reaming are carried out, the initial forging temperature of the punching and reaming is 1130 ℃, the wall thickness of the guard ring forging stock is 180mm after the reaming is finished, and air cooling is carried out;
step 4: and (3) putting the forging stock into a 500 ℃ kiln, heating at 70 ℃/h, heating to 1100 ℃, preserving heat for 4 hours, discharging, and cooling with water to obtain the guard ring forging in a solid solution state.
The preparation method of example 4 is substantially the same as that of example 1, except that:
Step 1: smelting and casting an electrode blank by adopting an arc furnace, and then smelting 7000kg of steel ingot by adopting electroslag remelting; the tapping temperature of the electric arc furnace is 1460 ℃; and the electroslag remelting is carried out by selecting CaF 2 70%,Al2O3 percent and CaO10 percent for slagging, and the melting speed of the electroslag remelting is 1.1T/h.
And (3) peeling the surface of the electroslag ingot to remove surface cracks and slag skin.
TABLE 1 chemical composition, wt%
TABLE 2 microstructure
TABLE 3 Performance test results
The inventors have conducted a number of experimental studies during the course of the study, and now consider some schemes with lower base yield strength as comparative examples.
Comparative example 1
The comparative example provides a grommet forging, the components of which are shown in table 4 below, and the preparation method is the same as that of example 1, and will not be described again here.
Comparative example 2
The comparative example provides a grommet forging, the components of which are shown in table 4 below, and the preparation method is the same as that of example 1, and will not be described again here.
Comparative example 3
The comparative example provides a grommet forging, the components of which are shown in table 4 below, and the preparation method is the same as that of example 1, and will not be described again here.
Comparative example 4
The comparative example provides a grommet forging, the components of which are shown in table 4 below, and the preparation method is the same as that of example 1, and will not be described again here.
The main performance test results of the comparative grommet forgings are shown in table 5.
TABLE 4 chemical composition, wt%
Comparative example | C | Si | Mn | S | P | Cr | Ni | Nb | V | N | Cu | Al |
1 | 0.10 | 0.08 | 20.23 | 0.009 | 0.020 | 19.44 | 0.02 | 0.003 | 0.02 | 0.8 | 0.03 | 0.005 |
2 | 0.078 | 0.074 | 18.86 | 0.008 | 0.020 | 19.45 | 0.02 | 0.003 | 0.005 | 0.68 | 0.008 | 0.008 |
3 | 0.10 | 0.055 | 18 | 0.006 | 0.025 | 18.17 | 0.02 | 0.003 | 0.005 | 0.5 | 0.007 | 0.006 |
4 | 0.11 | 0.45 | 17.5 | 0.002 | 0.012 | 18.7 | 0.17 | 0.003 | 0.005 | 0.58 | 0.06 | 0.002 |
Table 5 comparative example performance test results
The comparative examples and comparative examples show that the grommet forgings of the present invention are excellent in strength after hot forging and solution treatment.
The present invention is not limited to the above-mentioned embodiments, and any changes or substitutions that can be easily understood by those skilled in the art within the technical scope of the present invention are intended to be included in the scope of the present invention.
Claims (10)
1. The preparation method of the guard ring forging is characterized by comprising the following steps of:
Step 1: smelting an electrode blank and electroslag remelting a steel ingot, and peeling;
Step 2: homogenizing the steel ingot;
step 3: forging and cogging the steel ingot, and blasting air for cooling after forging;
step 4: and carrying out solution treatment on the forging stock to obtain the guard ring forging.
2. The method according to claim 1, wherein in the step 2, the homogenizing treatment comprises the steps of:
S201, heating the steel ingot to 600-650 ℃ for heat preservation, and performing heat preservation according to 1-1.2 h/100 mm;
S202, heating to 800-850 ℃, and carrying out heat preservation according to 1-1.2 h/100 mm;
S203, heating to 1150-1180 ℃, and performing heat preservation according to 2-3 h/100 mm; wherein the temperature rise rate in S202 is smaller than the temperature rise rate in S203.
3. The method according to claim 2, wherein in S202, the temperature rise rate is 40 ℃/h or less.
4. The method according to claim 2, wherein in S203, the temperature rise rate is 70 ℃/h or more.
5. The method according to claim 1, wherein in the step 3, forging cogging is performed by lightly drawing, upsetting and drawing, punching, and reaming.
6. The method according to claim 5, wherein in the step 3, the forging temperature for the forging cogging step of the light-drawing, upsetting and drawing of the ingot is 1150 to 1180 ℃.
7. The method according to claim 1, wherein in the step 4, the solution treatment includes: and (3) charging the forging stock into a furnace at the furnace temperature of less than or equal to 500 ℃ and rapidly heating to 1080-1100 ℃, preserving heat according to 2-2.5 h/100mm, discharging and cooling with water.
8. The method of manufacturing of claim 1, wherein the grommet forging comprises the following components in mass percent: 0.08 to 0.11 percent of C, 0.40 to 1.2 percent of Si, and Mn
18.5%~21.0%,Cr 18%~19.5%,Ni 0.5%~3%,V 0.35%~0.95%,N
0.68 To 0.75 percent of Nb 0.005 to 0.03 percent, less than or equal to 0.01 percent of Cu, less than or equal to 0.01 percent of Al, less than or equal to 0.010 percent of P, less than or equal to 0.010 percent of S, and the balance of Fe and unavoidable trace impurities.
9. A grommet forging, characterized in that it is produced by the production method according to any one of claims 1 to 8.
10. The grommet forging of claim 9, wherein the microstructure of the grommet forging is austenite+diffusion nitride.
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