CN113025799B - Heat treatment method for curved surface flexible plate of large wind tunnel - Google Patents

Heat treatment method for curved surface flexible plate of large wind tunnel Download PDF

Info

Publication number
CN113025799B
CN113025799B CN202110229029.7A CN202110229029A CN113025799B CN 113025799 B CN113025799 B CN 113025799B CN 202110229029 A CN202110229029 A CN 202110229029A CN 113025799 B CN113025799 B CN 113025799B
Authority
CN
China
Prior art keywords
flexible plate
curved surface
temperature
tool
order
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202110229029.7A
Other languages
Chinese (zh)
Other versions
CN113025799A (en
Inventor
马东平
王长军
谢晶
赵宽
何文信
何学斌
梁剑雄
任国柱
洪兴福
周荣田
杨志勇
尉成果
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuhan Shanfu Heavy Machine Tool Co ltd
Central Iron and Steel Research Institute
High Speed Aerodynamics Research Institute of China Aerodynamics Research and Development Center
Original Assignee
Wuhan Shanfu Heavy Machine Tool Co ltd
Central Iron and Steel Research Institute
High Speed Aerodynamics Research Institute of China Aerodynamics Research and Development Center
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuhan Shanfu Heavy Machine Tool Co ltd, Central Iron and Steel Research Institute, High Speed Aerodynamics Research Institute of China Aerodynamics Research and Development Center filed Critical Wuhan Shanfu Heavy Machine Tool Co ltd
Priority to CN202110229029.7A priority Critical patent/CN113025799B/en
Publication of CN113025799A publication Critical patent/CN113025799A/en
Application granted granted Critical
Publication of CN113025799B publication Critical patent/CN113025799B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/78Combined heat-treatments not provided for above
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

The invention discloses a heat treatment method for a curved surface flexible plate of a large wind tunnel. According to the heat treatment method, the flexible plate is fixed on a high-precision curved surface tool with a flow channel at the bottom, the flexible plate is fixed into a combined piece through a door-shaped beam and a set screw, the flexible plate of the combined piece is tightly attached to the tool, the combined piece is subjected to heat treatment for three times successively, the combined piece is disassembled after each heat treatment, the tool is subjected to finish machining and then combined into the combined piece, and the flexible plate is ensured to be tightly attached to the tool for each combined piece. The heat treatment method ensures that the heating and cooling speeds of the upper surface and the lower surface of the flexible plate are consistent during heating and cooling of the flexible plate, ensures the profile precision of the flexible plate, and has good effects of controlling performance and shape.

Description

Heat treatment method for curved surface flexible plate of large wind tunnel
Technical Field
The invention belongs to the technical field of wind tunnel tests, and particularly relates to a heat treatment method for a curved surface flexible plate of a large wind tunnel.
Background
In a conventional high-speed wind tunnel, a flexible plate of a spray pipe section is usually made of alloy steel, and the flexible plate can meet the requirement as a plane plate. The spray pipe section of a certain large wind tunnel needs to develop a large-size thin-wall curved flexible plate to meet the change requirements of different Mach numbers in a low-temperature region. As the operation temperature range of the large wind tunnel is 330K-110K, the large thin-walled curved surface flexible plate is made of 022Cr12Ni10MoTi maraging stainless steel with good impact toughness at low temperature, but the 022Cr12Ni10MoTi maraging stainless steel has higher yield strength and complex heat treatment requirements. The process research in the early stage finds that if the cooling speeds of the upper surface and the lower surface of the large-specification thin-wall curved flexible plate are inconsistent, the mechanical property can not meet the requirement, and warping is easy to occur in the heat treatment process, so that the development of the large-specification thin-wall curved flexible plate faces the double problems of difficult controllability and difficult shape control.
At present, the development of a heat treatment method for a curved flexible plate of a large wind tunnel is urgently needed.
Disclosure of Invention
The invention aims to provide a heat treatment method for a curved surface flexible plate of a large wind tunnel.
The invention relates to a heat treatment method of a large wind tunnel curved surface flexible plate, which is characterized in that the length of the flexible plate treated by the heat treatment method is more than the width and more than the thickness, and a surface thermocouple is arranged on the upper surface of the flexible plate; the tool used by the heat treatment method comprises a curved surface support at the lower part, a curved surface panel covered above the curved surface support and a flow channel rib welded on the surface of the curved surface panel, wherein the curved surface of the curved surface panel is consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate, and the curved surface of the top surface of the flow channel rib is also consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate; the heat treatment method comprises the following steps:
a. covering the flexible plate on the surface of the tool, fixing the flexible plate on the surface of the tool through a plurality of groups of door-shaped beams and set screws from front to back, checking and determining that the lower surface of the flexible plate is completely attached to the top surface of the rib of the tool flow channel, and obtaining a combined piece I;
b. putting the assembly I into a furnace, starting from room temperature, heating to a first-order temperature TL1 at a first-order heating speed delta TL1, preserving heat at the first order HL1, then heating to a high-order temperature TH1 at a high-order heating speed delta TH1, timing after a surface thermocouple of the flexible plate reaches the high-order temperature TH1, preserving heat at the high order HH1, discharging the flexible plate out of the furnace, and cooling the flexible plate to the room temperature by air;
c. removing the door-shaped beam of the assembly I, and performing finish machining on the runner ribs of the tool until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the curved surface flexible plate of the large-scale high-speed wind tunnel;
d. covering the flexible plate on the surface of the tool, fixing the flexible plate on the surface of the tool through a plurality of groups of cross beams and set screws from front to back, checking and determining that the lower surface of the flexible plate is completely attached to the top surface of the runner rib of the tool, and obtaining a combined piece II;
e. putting the assembly II into a furnace, starting from room temperature, heating to an initial-stage temperature TL2 at an initial-stage heating speed delta TL2, preserving heat at the initial stage HL2, then heating to a high-stage temperature TH2 at a high-stage heating speed delta TH2, timing after a surface thermocouple of the flexible plate reaches the high-stage temperature TH2, preserving heat at the high stage HH2, discharging the flexible plate, and cooling to room temperature by water;
f. removing the door-shaped beam of the assembly II, and performing finish machining on the runner ribs of the tool until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the curved surface flexible plate of the large-scale high-speed wind tunnel;
g. covering the flexible plate on the surface of the tool, fixing the flexible plate on the surface of the tool through a plurality of groups of door-shaped beams and set screws from front to back, checking and determining that the lower surface of the flexible plate is completely attached to the top surface of the tool flow channel rib to obtain a combined piece III;
h. and putting the assembly III into a furnace, starting from room temperature, heating to a high-order temperature TH3 at a high-order heating speed Delta TH3, timing after the surface thermocouple of the flexible plate reaches the high-order temperature TH3, keeping the temperature at the high order HH3, taking out of the furnace, and air cooling to room temperature to finish heat treatment.
Furthermore, the material of the flexible plate is 022Cr12Ni10MoTi maraging stainless steel.
Further, the tool is made of 304 stainless steel.
Furthermore, the door-shaped beam and the set screw are made of high-temperature alloy steel.
Further, the initial temperature rise speeds are the same, and Δ TL1= Δ TL2; the primary temperature TL1 is more than TL2; the initial stage heat preservation time HL1= HL2;
the high-order heating speed is the same as Deltath 1= Deltath 2= Deltath 3; the high-order temperature TH1 is more than TH2 and more than TH3, and the high-order heat preservation time HH1 is more than HH2 and more than HH3.
Further, the initial temperature rise speed Δ TL1= Δ TL2=100 ℃/h; primary temperature TL1=850 ℃, TL2=700 ℃; the initial stage heat preservation time HL1= HL2=0.5h;
the high-order heating speed Δ TH1= Δ TH2= Δ TH3=60 ℃/h; high-order temperature TH1=900 ℃, TH2=750 ℃, TH3=500 ℃, high-order incubation time HH1=2.5h, hh2=3h, hh3=4h;
the adopted cooling mode is as follows: the high-order temperature TH1=900 ℃ is air-cooled, the high-order temperature TH2=750 ℃ is water-cooled, and the high-order temperature TH3=500 ℃ is air-cooled.
The portal beam and the set screw adopted in the heat treatment method of the large wind tunnel curved surface flexible plate are made of high-temperature alloy steel, the high-temperature alloy steel has higher strength and rigidity in a high-temperature region, and the portal beam has the advantages of ingenious structure, convenience in disassembly and assembly, high installation precision and suitability for repeated disassembly and assembly.
The tool in the heat treatment method of the large wind tunnel curved surface flexible plate is made of 304 stainless steel, and the expansion coefficients of the 304 stainless steel and 022Cr12Ni10MoTi maraging stainless steel materials of the flexible plate are close to each other, so that the tool is suitable for being assembled into an assembly to be put into a furnace for heat treatment.
According to the heat treatment method for the curved-surface flexible plate of the large wind tunnel, the flexible plate is pressed on the tool by the aid of the door-shaped beam all the time in the heating and cooling processes of the flexible plate, so that the upper surface and the lower surface of the flexible plate are consistent in speed in the heating and cooling processes, the tool is subjected to finish machining after each heat treatment, the flexible plate is ensured to be attached to the tool, and the heat treatment of the flexible plate is completed through three heat treatments.
The heating speed, the heat preservation temperature, the heat preservation time and the cooling mode in the heat treatment method of the large wind tunnel curved surface flexible plate are subjected to numerical simulation calculation and test verification, so that the performance of the flexible plate and the curved surface precision of the flexible plate can be ensured, the heat treatment problem of the stainless steel curved surface flexible plate with the ultra-large specification and high strength of the large wind tunnel is solved, and the good effects of controllability and shape control are achieved.
Drawings
FIG. 1 is a schematic diagram of a flexible plate in a heat treatment method for a curved surface flexible plate of a large wind tunnel according to the present invention;
FIG. 2 is a schematic view of a tooling in the heat treatment method of a large wind tunnel curved flexible plate according to the present invention;
FIG. 3 is a schematic diagram of an assembly in the heat treatment method for a large wind tunnel curved flexible plate according to the present invention.
In the figure, 1 is a flexible plate 2, 3 is a door-shaped beam.
Detailed Description
The present invention will be described in detail below with reference to the accompanying drawings and examples.
Example 1
The flexible plate 1 in this embodiment is a curved thin plate of 022Cr12Ni10MoTi maraging stainless steel with extra large gauge and high strength.
As shown in fig. 1, a flexible plate 1 processed by the heat treatment method for the large wind tunnel curved surface flexible plate of the embodiment has a length of 7000mm, a width of 2800mm and a thickness of only 45mm, and a surface thermocouple is mounted on the upper surface of the flexible plate 1; the tool 2 used in the heat treatment method is shown in figure 2, the tool 2 comprises a curved surface support at the lower part, a curved surface panel covering the curved surface support and a flow channel rib welded on the surface of the curved surface panel, the curved surface of the curved surface panel is consistent with the curved surface of a large-scale high-speed wind tunnel curved surface flexible plate, and the curved surface of the top surface of the flow channel rib is also consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate; the heat treatment method comprises the following steps:
a. covering the flexible plate 1 on the surface of the tool 2, fixing the flexible plate 1 on the surface of the tool 2 through 10 groups of door-shaped beams 3 and set screws from front to back, checking and determining that the lower surface of the flexible plate 1 is completely attached to the top surface of the runner rib of the tool 2, and obtaining an assembly I shown in figure 3;
b. putting the assembly I into a furnace, starting from room temperature, heating to 850 ℃ at a primary temperature rise speed of 100 ℃/h, preserving heat for 0.5h at the primary temperature, then heating to 900 ℃ at a high-order temperature rise speed of 60 ℃/h, timing after a surface thermocouple of the flexible plate 1 reaches the high-order temperature of 900 ℃, and taking out of the furnace and air-cooling to room temperature after 2.5h of high-order heat preservation;
c. removing the door-shaped beam 3 of the assembly I, and performing finish machining on the runner ribs of the tool 2 until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate;
d. covering the flexible plate 1 on the surface of the tool 2, fixing the flexible plate 1 on the surface of the tool 2 through 10 groups of door-shaped beams 3 and set screws from front to back, checking to ensure that the lower surface of the flexible plate 1 is completely attached to the top surface of the runner rib of the tool 2, and obtaining a combined piece II;
e. putting the assembly II into a furnace, starting from room temperature, heating to 700 ℃ at a first-stage heating rate of 100 ℃/h, preserving heat for 0.5h at the first stage, then heating to 750 ℃ at a high-stage heating rate of 60 ℃/h, timing after a surface thermocouple of the flexible plate 1 reaches 750 ℃ at a high-stage temperature, preserving heat for 3h at the high stage, taking out of the furnace, and cooling to room temperature by water;
f. removing the door-shaped beam 3 of the assembly II, and performing finish machining on the runner ribs of the tool 2 until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate;
g. covering the flexible plate 1 on the surface of the tool 2, fixing the flexible plate 1 on the surface of the tool 2 through 10 groups of door-shaped beams 3 and set screws from front to back, checking and determining that the lower surface of the flexible plate 1 is completely attached to the top surface of the runner rib of the tool 2, and obtaining a combined piece III;
h. and putting the assembly III into a furnace, heating the assembly III to a high-order temperature of 500 ℃ from room temperature at a high-order heating speed of 60 ℃/h, timing after a surface thermocouple of the flexible plate 1 reaches the high-order temperature of 500 ℃, keeping the temperature for 4h at the high order, taking the assembly out of the furnace, and cooling the assembly to room temperature to finish heat treatment.
Furthermore, the material of the flexible plate 1 is 022Cr12Ni10MoTi maraging stainless steel.
Further, the tool 2 is made of 304 stainless steel.
Furthermore, the material of the door beam 3 and the set screw is high-temperature alloy steel.
The heat treatment method for the large-scale wind tunnel curved surface flexible plate of the embodiment verifies that the heating speed, the heat preservation temperature, the heat preservation time and the cooling mode of the embodiment can solve the problem of development of the large-scale wind tunnel curved surface flexible plate through numerical simulation calculation and two small-scale flexible plate heat treatment tests, ensures the profile precision of the flexible plate, and has good effects of shape control and shape control.
The embodiments of the present invention are disclosed as the preferred embodiments, but not limited thereto, and those skilled in the art can easily understand the spirit of the present invention and make various extensions and changes without departing from the spirit of the present invention.

Claims (3)

1. The heat treatment method of the large wind tunnel curved surface flexible plate is characterized in that the length of the flexible plate (1) treated by the heat treatment method is larger than the width ≫, and the upper surface of the flexible plate (1) is provided with a surface thermocouple; the tool (2) used in the heat treatment method comprises a curved surface support at the lower part, a curved surface panel covering the curved surface support and a flow channel rib welded on the surface of the curved surface panel, wherein the curved surface of the curved surface panel is consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate, and the curved surface of the top surface of the flow channel rib is also consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate; the flexible plate (1) is made of 022Cr12Ni10MoTi maraging stainless steel; the heat treatment method comprises the following steps:
a. covering the flexible plate (1) on the surface of the tool (2), fixing the flexible plate (1) on the surface of the tool (2) through a plurality of groups of door-shaped beams (3) and set screws from front to back, checking and determining that the lower surface of the flexible plate (1) is completely attached to the top surface of the runner rib of the tool (2), and obtaining a combined part I;
b. putting the assembly I into a furnace, starting from room temperature, heating to a first-order temperature TL1 at a first-order heating speed delta TL1, preserving heat at the first order HL1, then heating to a high-order temperature TH1 at a high-order heating speed delta TH1, timing after a surface thermocouple of the flexible plate (1) reaches the high-order temperature TH1, preserving heat at the high order HH1, discharging the flexible plate out of the furnace, and cooling to room temperature;
c. removing the door-shaped beam (3) of the assembly I, and performing finish machining on the runner ribs of the tool (2) until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate;
d. covering the flexible plate (1) on the surface of the tool (2), fixing the flexible plate (1) on the surface of the tool (2) through a plurality of groups of door-shaped beams (3) and set screws from front to back, checking and determining that the lower surface of the flexible plate (1) is completely attached to the top surface of a runner rib of the tool (2), and obtaining a combined piece II;
e. putting the assembly II into a furnace, starting from room temperature, heating to an initial-stage temperature TL2 at an initial-stage heating speed delta TL2, preserving heat at the initial stage HL2, then heating to a high-stage temperature TH2 at a high-stage heating speed delta TH2, timing after a surface thermocouple of the flexible plate (1) reaches the high-stage temperature TH2, preserving heat at the high stage HH2, discharging the furnace, and cooling to room temperature by water;
f. removing the door-shaped beam (3) of the assembly II, and performing finish machining on the runner ribs of the tool (2) until the curved surfaces of the top surfaces of the runner ribs are consistent with the curved surface of the large-scale high-speed wind tunnel curved surface flexible plate;
g. covering the flexible plate (1) on the surface of the tool (2), fixing the flexible plate (1) on the surface of the tool (2) through a plurality of groups of door-shaped beams (3) and set screws from front to back, checking and determining that the lower surface of the flexible plate (1) is completely attached to the top surface of the runner rib of the tool (2), and obtaining a combined part III;
h. putting the assembly III into a furnace, starting from room temperature, heating to a high-order temperature TH3 at a high-order heating speed delta TH3, timing after a surface thermocouple of the flexible plate (1) reaches the high-order temperature TH3, keeping the temperature of HH3 at a high order, taking out of the furnace, air cooling to room temperature, and finishing heat treatment;
the initial-stage heating speeds are the same, and delta TL1= delta TL2; the primary temperature TL1 is more than TL2; the initial stage heat preservation time HL1= HL2;
the high-order heating speed is the same as Deltath 1= Deltath 2= Deltath 3; the high-order temperature TH1 is more than TH2 and more than TH3, and the high-order heat preservation time HH1 is more than HH2 and more than HH3;
the initial temperature rise speed delta TL1= delta TL2=100 ℃/h; primary temperature TL1=850 ℃, TL2=700 ℃; the initial stage heat preservation time HL1= HL2=0.5h;
the high-order temperature rise speed is delta TH1= delta TH2= delta TH3=60 ℃/h; high-order temperature TH1=900 ℃, TH2=750 ℃, TH3=500 ℃, high-order incubation time HH1=2.5h, hh2=3h, hh3=4h;
the cooling method adopted is as follows: the high-order temperature TH1=900 ℃ is air-cooled, the high-order temperature TH2=750 ℃ is water-cooled, and the high-order temperature TH3=500 ℃ is air-cooled.
2. The heat treatment method of the large wind tunnel curved flexible plate according to claim 1, wherein the tool (2) is made of 304 stainless steel.
3. The heat treatment method of the large wind tunnel curved flexible plate according to claim 1, wherein the material of the door beam (3) and the set screw is high-temperature alloy steel.
CN202110229029.7A 2021-03-02 2021-03-02 Heat treatment method for curved surface flexible plate of large wind tunnel Active CN113025799B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110229029.7A CN113025799B (en) 2021-03-02 2021-03-02 Heat treatment method for curved surface flexible plate of large wind tunnel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110229029.7A CN113025799B (en) 2021-03-02 2021-03-02 Heat treatment method for curved surface flexible plate of large wind tunnel

Publications (2)

Publication Number Publication Date
CN113025799A CN113025799A (en) 2021-06-25
CN113025799B true CN113025799B (en) 2022-10-11

Family

ID=76465322

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110229029.7A Active CN113025799B (en) 2021-03-02 2021-03-02 Heat treatment method for curved surface flexible plate of large wind tunnel

Country Status (1)

Country Link
CN (1) CN113025799B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113375893B (en) * 2021-08-12 2022-06-14 中国空气动力研究与发展中心高速空气动力研究所 Continuous wind tunnel test method adopting reverse Brayton cycle to control temperature
CN117433484A (en) * 2023-12-13 2024-01-23 中国空气动力研究与发展中心设备设计与测试技术研究所 Wide-temperature-range wind tunnel multi-pivot flexible-wall spray pipe molded surface measuring device and measuring method

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE670021A (en) * 1964-09-23 1966-03-23
KR920006529A (en) * 1990-09-21 1992-04-27 이상수 High strength, high toughness, high corrosion resistance stainless maraging steel and manufacturing method
JP2004353058A (en) * 2003-05-30 2004-12-16 Koyo Thermo System Kk Heat treatment oven
JP2005256121A (en) * 2004-03-12 2005-09-22 Jfe Steel Kk Cr-CONTAINING ALLOY HAVING EXCELLENT STRAIN AGING RESISTANCE IN WELD ZONE
CN101210304A (en) * 2006-12-27 2008-07-02 沈阳鼓风机(集团)有限公司 Martensite precipitation hardening stainless steel for compressor impeller and preparation method thereof
CN107974642A (en) * 2017-01-17 2018-05-01 上海落日新材料科技有限公司 A kind of cutter precipitation-hardening stainless steel and its manufacture method
CN108237155A (en) * 2016-12-26 2018-07-03 核工业西南物理研究院 A kind of complex-curved manufacturing method of large size tokamak vacuum room housing
CN108421649A (en) * 2018-02-27 2018-08-21 辽宁科技大学 A kind of rectangle superonic flow nozzzle and its design method
CN110438416A (en) * 2019-09-02 2019-11-12 鞍钢股份有限公司 Method for eliminating surface cracks of ultra-wide high-nitrogen austenitic stainless steel medium plate
CN111118258A (en) * 2020-01-20 2020-05-08 中国科学院金属研究所 Heat treatment method for improving low-temperature impact toughness of 00Cr12Ni10MoTi maraging stainless steel

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6474249B1 (en) * 2000-08-18 2002-11-05 John Bruce Smith Mobile furnace and method of facilitating removal of material from workpieces
US7931758B2 (en) * 2008-07-28 2011-04-26 Ati Properties, Inc. Thermal mechanical treatment of ferrous alloys, and related alloys and articles
US9671199B1 (en) * 2014-05-06 2017-06-06 Premier Body Armor, LLC Armor steel products and method for making same
CN205803568U (en) * 2016-07-29 2016-12-14 攀枝花学院 Butterfly spring sheet timeliness fixture
CN208136280U (en) * 2018-03-01 2018-11-23 珠海市金创科技有限公司 Composite material curved surface aging processing apparatus
CN112247483B (en) * 2020-09-28 2022-03-25 天津航天长征火箭制造有限公司 Spinning method of workpiece with 2195 aluminum-lithium alloy special-shaped cross section structure

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE670021A (en) * 1964-09-23 1966-03-23
KR920006529A (en) * 1990-09-21 1992-04-27 이상수 High strength, high toughness, high corrosion resistance stainless maraging steel and manufacturing method
JP2004353058A (en) * 2003-05-30 2004-12-16 Koyo Thermo System Kk Heat treatment oven
JP2005256121A (en) * 2004-03-12 2005-09-22 Jfe Steel Kk Cr-CONTAINING ALLOY HAVING EXCELLENT STRAIN AGING RESISTANCE IN WELD ZONE
CN101210304A (en) * 2006-12-27 2008-07-02 沈阳鼓风机(集团)有限公司 Martensite precipitation hardening stainless steel for compressor impeller and preparation method thereof
CN108237155A (en) * 2016-12-26 2018-07-03 核工业西南物理研究院 A kind of complex-curved manufacturing method of large size tokamak vacuum room housing
CN107974642A (en) * 2017-01-17 2018-05-01 上海落日新材料科技有限公司 A kind of cutter precipitation-hardening stainless steel and its manufacture method
CN108421649A (en) * 2018-02-27 2018-08-21 辽宁科技大学 A kind of rectangle superonic flow nozzzle and its design method
CN110438416A (en) * 2019-09-02 2019-11-12 鞍钢股份有限公司 Method for eliminating surface cracks of ultra-wide high-nitrogen austenitic stainless steel medium plate
CN111118258A (en) * 2020-01-20 2020-05-08 中国科学院金属研究所 Heat treatment method for improving low-temperature impact toughness of 00Cr12Ni10MoTi maraging stainless steel

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
固溶温度对00Cr12Ni10MoTi马氏体时效不锈钢组织与性能的影响;刘入杰等;《中国金属通报》;20180428(第04期);第65-67页 *
改善00Cr12Ni10MoTi热轧板材屈服强度工艺优化探析;胡进;《特钢技术》;20160625(第02期);第37-40页 *
某低温风洞S03钢弯刀热推弯成形工艺;马东平等;《锻压技术》;20201031;第45卷(第10期);第86-91页 *
某低温风洞用高强不锈钢弯刀小试件生产实践;马东平等;《中国冶金》;20201025;第129-136页 *
热处理工艺对00Cr12Ni10MoTi不锈钢组织与力学性能的影响;陶则旭等;《热处理》;20220630(第6期);第95-97页 *
预处理对低温用高强度钢00Cr12Ni10MoTi力学性能的影响;葛鹏等;《金属热处理》;20130430;第38卷(第4期);第60-63页 *

Also Published As

Publication number Publication date
CN113025799A (en) 2021-06-25

Similar Documents

Publication Publication Date Title
CN113025799B (en) Heat treatment method for curved surface flexible plate of large wind tunnel
AU2018451202B2 (en) Mold for implementing in-mold rapid forming and quenching
CN104070075B (en) A kind of TEMPERATURE FOR HOT STRIP LAMINAR cooling procedure control device and method
US6210630B1 (en) Process for manufacturing a hollow turbomachine blade and a multiple-action furnace press for use in said process
CN211595729U (en) Supercritical nitrogen quenching circulating cooling system for vacuum furnace
CN101623823A (en) Automatic production line for warm/hot forming complete equipment of energy-saving high-strength sheet steel
CN106755821A (en) Heat treatment production analogue means and experimental technique
CN106834634A (en) Quenching experimental device and quenching assay method
CN108994135A (en) A kind of quenching integrated manufacturing process of hot forming
CN103559334B (en) Modeling method and system for temperature field in laminar cooling
CN103658657A (en) Controllable cooling method for metal powder injection forming vacuum degreasing sintering furnace
CN111485185A (en) Aluminum alloy plate compounding-solution quenching integrated hot forming method
CN109985955A (en) A kind of control member evenness of wall thickness isothermal hot deep drawing device and its manufacturing process
CN106987685B (en) A kind of heat treatment process for Cr12MoV steel casting mould types face
CN106755778B (en) A kind of thin-walled long blade vacuum hardening technique
CN106435147A (en) Air quenching method of circular saw web
CN113001127B (en) Method and device for machining skin with active cooling channel
CN104785549A (en) Laminar cooling method under thin-specification steel plate forced cooling condition
CN105112625B (en) A kind of manufacture method of pressurized-water reactor nuclear power plant shielding impeller of pump forging
CN220245912U (en) Substrate glass shaping thickness adjusting device
CN103343184A (en) Notched-bar microstructure-crack initiation method used for chipless fine blanking
Chen et al. Iterative reverse deformation optimization design of castings based on numerical simulation of solidification thermal stress
CN106854691A (en) Steel part Technology for Heating Processing, steel part forging method and annealing device using the Technology for Heating Processing
CN110117710A (en) A kind of cooling velocity forecasting procedure being suitable for RCS sections of continuous annealing unit
CN110238619A (en) A kind of manufacture aluminium alloy wheel hub process flow system

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant