[go: up one dir, main page]

CN111299575A - A conformal adjustment substrate for laser selective melting and forming of large-sized thin-walled structural parts - Google Patents

A conformal adjustment substrate for laser selective melting and forming of large-sized thin-walled structural parts Download PDF

Info

Publication number
CN111299575A
CN111299575A CN201911270758.6A CN201911270758A CN111299575A CN 111299575 A CN111299575 A CN 111299575A CN 201911270758 A CN201911270758 A CN 201911270758A CN 111299575 A CN111299575 A CN 111299575A
Authority
CN
China
Prior art keywords
substrate
thin
section
forming
walled
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.)
Granted
Application number
CN201911270758.6A
Other languages
Chinese (zh)
Other versions
CN111299575B (en
Inventor
王国庆
何京文
董鹏
梁晓康
严振宇
赵衍华
马丽翠
马芳
周庆军
朱瑞灿
田彩兰
刘天亮
洪媛媛
矫慧
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.)
China Academy of Launch Vehicle Technology CALT
Capital Aerospace Machinery Co Ltd
Original Assignee
China Academy of Launch Vehicle Technology CALT
Capital Aerospace Machinery Co Ltd
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 China Academy of Launch Vehicle Technology CALT, Capital Aerospace Machinery Co Ltd filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201911270758.6A priority Critical patent/CN111299575B/en
Publication of CN111299575A publication Critical patent/CN111299575A/en
Application granted granted Critical
Publication of CN111299575B publication Critical patent/CN111299575B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/30Platforms or substrates
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y30/00Apparatus for additive manufacturing; Details thereof or accessories therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Laser Beam Processing (AREA)
  • Powder Metallurgy (AREA)

Abstract

The utility model provides a follow-up adjustment base plate of laser election district melting shaping jumbo size thin-walled structure, the base plate divides multisection activity base plate, and from the diameter of base plate crescent to the base plate of last section can be nested on adjacent next section base plate, and the thickness of each section of base plate is unanimous, and the base plate is placed in the inside of big breadth thin-walled structure.

Description

一种激光选区熔化成形大尺寸薄壁结构件的随形调节基板A conformal adjustment substrate for laser selective melting and forming of large-sized thin-walled structural parts

技术领域technical field

本发明属于激光选区熔化成形领域,涉及一种大尺寸薄壁结构件的随形调节基板。The invention belongs to the field of laser selective melting and forming, and relates to a shape-compliant adjustment substrate of a large-sized thin-walled structural member.

背景技术Background technique

曲面型薄壁结构件是航天产品的重要构件,小端200mm,大端1200mm,轴高1000mm。螺旋构件密集排列、壁薄、变截面,试件的宽度为5.0mm,焊缝平均宽度达到3.2mm,焊缝面积占产品表面积的60%以上,焊接变形大,目前采用的焊接方式实现试件生产存在困难。Curved thin-walled structural parts are important components of aerospace products, the small end is 200mm, the big end is 1200mm, and the shaft height is 1000mm. The spiral components are densely arranged, with thin walls and variable sections. The width of the test piece is 5.0mm, and the average width of the weld is 3.2mm. The weld area accounts for more than 60% of the surface area of the product, and the welding deformation is large. The current welding method is used to realize the test piece. Production is difficult.

增材制造为结构件制造提供了一种新高效率、高质量、整体优化的制造工艺方案。目前在激光选区熔化成形领域,国内外已经增材制造大量的产品,都是采用非活动式的基板,将基板用螺钉固定在成形腔内,在成形的整个过程中,基板是一直固定,起到试件的支撑作用。刮板将送粉缸的粉末材料铺设置基板,激光对基板上的金属材料进行制造,基板下降一层高度,继续铺粉加工直至试件完成增材制造的整个过程。Additive manufacturing provides a new high-efficiency, high-quality, and overall optimized manufacturing process solution for structural parts manufacturing. At present, in the field of laser selective melting and forming, a large number of products have been additively manufactured at home and abroad, all of which use inactive substrates, and the substrates are fixed in the forming cavity with screws. During the entire forming process, the substrates are always fixed. support to the specimen. The scraper lays the powder material of the powder feeding cylinder on the base plate, and the laser manufactures the metal material on the base plate.

发明内容SUMMARY OF THE INVENTION

本发明所要解决的技术问题是一种大尺寸薄壁结构件的随形调节基板。The technical problem to be solved by the present invention is a conformal adjustment substrate of a large-sized thin-walled structural member.

一种用于激光选区熔化成形大尺寸薄壁结构件的随形调节基板,所述基板分多节活动基板,从上至下基板的直径逐渐增大,并且上一节的基板可以嵌套在相邻下一节基板上,每一节基板的厚度是一致的,基板放置于大幅面薄壁结构件的内部。A conformal adjustment substrate used for laser selective melting and forming of large-sized thin-walled structural parts, the substrate is divided into multi-section movable substrates, the diameter of the substrate gradually increases from top to bottom, and the substrate of the previous section can be nested in On the adjacent next section of the substrate, the thickness of each section of the substrate is the same, and the substrate is placed inside the large-format thin-walled structural member.

所述基板材料根据大幅面薄壁结构件的材料选择,要求基板材料与结构件材料的热物性参数匹配。The substrate material is selected according to the material of the large-format thin-walled structural member, and it is required that the thermal physical parameters of the substrate material and the structural member material be matched.

所述圆形基板最外环的外径薄壁结构件底端外径加40~60mm,第i节活动基板的外径为此处薄壁结构件内径减去5~10mm,每节活动基板的厚度为Δh=H/n,n为活动基板分节的数量H为大幅面薄壁结构的高度。The outer diameter of the outermost ring of the circular substrate is the outer diameter of the bottom end of the thin-walled structural member plus 40 to 60 mm, and the outer diameter of the i-th movable substrate is the inner diameter of the thin-walled structural member here minus 5 to 10 mm. The thickness of Δh=H/n, n is the number of segments of the movable substrate, and H is the height of the large-format thin-walled structure.

将分层调节基板的最外环固定在成形缸上,通过激光选区熔化成形制备第1节薄壁结构件,当成形高度达到Δh时,第1~n节活动基板升高Δh,然后继续成形第2节薄壁结构件,然后继续成形第3节薄壁结构件;重复以上步骤,当成形高度达到H时,第n节活动基板升高Δh的高度,同时成形结束。The outermost ring of the layered adjustment substrate is fixed on the forming cylinder, and the first thin-walled structural parts are prepared by laser selective melting and forming. When the forming height reaches Δh, the first to n movable substrates are raised by Δh, and then continue to be formed. Section 2 thin-walled structural parts, and then continue to form the third section of thin-walled structural parts; repeat the above steps, when the forming height reaches H, the nth movable base plate is raised by the height of Δh, and the forming ends at the same time.

采用大尺寸薄壁结构件的随形调节基板可以取得了良好的成形质量,具有下列优点:解决大幅面薄壁结构件成形缸体的冗余金属粉末过多,成本高, 易导致粉末污染等问题,粉末利用率达到80%。The conformal adjustment substrate using large-sized thin-walled structural parts can achieve good forming quality, and has the following advantages: solving the problem of excessive redundant metal powder in the forming cylinder of large-sized thin-walled structural parts, high cost, and easy to cause powder pollution, etc. Problem, the powder utilization rate reaches 80%.

附图说明Description of drawings

图1为大幅面薄壁结构示意图。Figure 1 is a schematic diagram of a large-format thin-walled structure.

图2为分层调节圆形基板示意图。FIG. 2 is a schematic diagram of a layered adjustment circular substrate.

图3为分层调节基板工作过程示意图。FIG. 3 is a schematic diagram of the working process of the layered adjustment substrate.

具体实施方式Detailed ways

实施例1Example 1

如图1-3所示,以大幅面高温合金薄壁结构件为例,顶端外径D顶端外: 262mm、内径D顶端内:250mm,底端外径D底端外:1158mm、内径D底端内:1146mm、结构件高度H:1000mm。As shown in Figure 1-3, taking a large-format high-temperature alloy thin-walled structure as an example, the outer diameter of the top end D is 262mm, the inner diameter D is 250mm, the outer diameter of the bottom end is D: 1158mm, and the inner diameter D is the bottom. Inner end : 1146mm, structure height H: 1000mm.

(1)基板材料的选择:大幅面薄壁结构件为高温合金材料,选用基板的材料为45号钢;(1) Selection of substrate material: the large-format thin-walled structural parts are high-temperature alloy materials, and the material for the substrate is 45# steel;

(2)基板尺寸的确定:活动基板分节的数量n取为20,每节活动基板的厚度Δh=H/n=1000mm/20=50mm,由大幅面高温合金薄壁结构件底端外径D底端外确定圆形基板最外环的外径d0=D底端外+40mm=1158mm+40mm=1198mm,第 1至第20节活动基板的外径尺寸按照公式di=Di内-6mm进行计算,具体见下表:(2) Determination of substrate size: the number n of movable substrate segments is taken as 20, the thickness of each movable substrate Δh=H/n=1000mm/20=50mm, the outer diameter of the bottom end of the large-format superalloy thin-walled structure is determined by The outer diameter of the outermost ring of the circular base plate is determined from the bottom end of D 0 =D bottom end +40mm=1158mm+40mm=1198mm, the outer diameter of the movable base plate of Sections 1 to 20 is in accordance with the formula d i =D i -6mm for calculation, see the following table for details:

Figure BDA0002314097580000031
Figure BDA0002314097580000031

(3)分层调节基板工作过程:将分层调节基板的最外环固定在成形缸上,通过激光选区熔化成形制备第1节薄壁结构件,当成形高度达到50mm时,第1~20节活动基板升高50mm,然后继续成形第2节薄壁结构件;当成形高度达到2×50mm=100mm时,第2~20节活动基板再次升高50mm,然后继续成形第3节薄壁结构件;重复以上步骤,当成形高度达到1000mm时,第20 节活动基板升高50mm的高度,成形结束。(3) The working process of the layered adjustment substrate: fix the outermost ring of the layered adjustment substrate on the forming cylinder, and prepare the first thin-walled structural parts by laser selective melting and forming. When the forming height reaches 50mm, the first to 20th The movable base plate is raised by 50mm, and then continues to form the second thin-walled structure; when the forming height reaches 2×50mm=100mm, the second to 20th movable base plate is raised again by 50mm, and then continues to form the third thin-walled structure. Repeat the above steps, when the forming height reaches 1000mm, the movable base plate of Section 20 is raised to a height of 50mm, and the forming is completed.

实施例2Example 2

实例2:以大幅面钛合金薄壁结构件为例,顶端外径D顶端外:314mm、内径D顶端内:300mm,底端外径D底端外:1448mm,、内径D底端内: 1434mm、结构件高度H:1200mm。Example 2: Take a large-format titanium alloy thin-walled structure as an example, the outer diameter D of the top end: 314mm, the inner diameter D of the top end: 300mm, the outer diameter of the bottom end D: the outer end of the bottom end: 1448mm, and the inner diameter D of the bottom end: 1434mm , Height H of structural parts: 1200mm.

(1)基板材料的选择:大幅面薄壁结构件为钛合金材料,选用基板的材料为同牌号钛合金;(1) Selection of substrate material: the large-format thin-walled structural parts are made of titanium alloy material, and the material of the substrate selected is the same grade of titanium alloy;

(2)基板尺寸的确定:活动基板分节的数量n取为30,每节活动基板的厚度Δh=H/n=1200mm/30=40mm,由大幅面钛合金薄壁结构件底端外径D底端外确定圆形基板最外环的外径d0=D底端外+40mm=1448mm +40mm=1488mm,第1至第30节活动基板的外径尺寸按照公式di=Di内-7mm 进行计算,具体见下表::(2) Determination of the size of the substrate: the number n of the sub-sections of the movable substrate is taken as 30, the thickness of each movable substrate Δh=H/n=1200mm/30=40mm, the outer diameter of the bottom end of the large-format titanium alloy thin-walled structure is determined by The outer diameter of the outermost ring of the circular base plate is determined from the bottom of D d0 = D bottom end +40mm = 1448mm +40mm = 1488mm, the outer diameter of the movable base plate in Sections 1 to 30 is in accordance with the formula d i = D i in - 7mm for calculation, see the following table for details:

Figure BDA0002314097580000041
Figure BDA0002314097580000041

(3)分层调节基板工作过程:将分层调节基板的最外环固定在成形缸上,通过激光选区熔化成形制备第1节薄壁结构件,当成形高度达到40mm时,第1~30节活动基板升高50mm,然后继续成形第2节薄壁结构件;当成形高度达到2×40mm=80mm时,第2~20节活动基板再次升高40mm,然后继续成形第3节薄壁结构件;重复以上步骤,当成形高度达到1200mm时,第30 节活动基板升高40mm的高度,成形结束。(3) The working process of the layered adjustment substrate: fix the outermost ring of the layered adjustment substrate on the forming cylinder, and prepare the first section of thin-walled structural parts by laser selective melting and forming. When the forming height reaches 40mm, the first to 30th The movable base plate is raised by 50mm, and then continues to form the second thin-walled structure; when the forming height reaches 2×40mm=80mm, the second to 20th movable base plates are raised again by 40mm, and then continue to form the third thin-walled structure. Repeat the above steps, when the forming height reaches 1200mm, the movable base plate of Section 30 is raised to a height of 40mm, and the forming is completed.

Claims (4)

1. The shape-following adjusting substrate for the large-size thin-wall structural member formed by selective laser melting is characterized in that the substrate is a multi-section nested movable substrate, the diameter of the substrate is gradually reduced from bottom to top, the substrate in the previous section can be nested on the substrate in the next adjacent section, the thickness of each section of substrate is consistent, and the substrate is placed in the large-size thin-wall structural member.
2. The substrate of claim 1, wherein the substrate material is selected according to the material of the large-format thin-walled structure, and the substrate material is required to be a material having good compatibility with the material of the structure.
3. The substrate according to claim 1, wherein the outer diameter of the bottom end of the outer diameter thin-walled structure of the outermost ring of the circular substrate is added with 40-60 mm, the outer diameter of the i-th section of the movable substrate is subtracted from the inner diameter of the thin-walled structure at the position, the thickness of each section of the movable substrate is Δ H ═ H/n, and n is the height of the large-width thin-walled structure, which is the number of sections of the movable substrate, H.
4. The use method of the substrate as claimed in claim 1, fixing the outermost ring of the layered adjustment substrate on a forming cylinder, preparing the 1 st section of thin-walled structural member by selective laser melting forming, when the forming height reaches Δ h, raising the 1 st to nth sections of movable substrates by Δ h, then continuing to form the 2 nd section of thin-walled structural member, and then continuing to form the 3 rd section of thin-walled structural member; and repeating the steps, when the forming height reaches H, raising the height of the nth section of movable substrate by delta H, and finishing forming.
CN201911270758.6A 2019-12-12 2019-12-12 Shape-following adjusting substrate for selective laser melting and forming large-size thin-wall structural member Active CN111299575B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911270758.6A CN111299575B (en) 2019-12-12 2019-12-12 Shape-following adjusting substrate for selective laser melting and forming large-size thin-wall structural member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911270758.6A CN111299575B (en) 2019-12-12 2019-12-12 Shape-following adjusting substrate for selective laser melting and forming large-size thin-wall structural member

Publications (2)

Publication Number Publication Date
CN111299575A true CN111299575A (en) 2020-06-19
CN111299575B CN111299575B (en) 2022-03-18

Family

ID=71158059

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911270758.6A Active CN111299575B (en) 2019-12-12 2019-12-12 Shape-following adjusting substrate for selective laser melting and forming large-size thin-wall structural member

Country Status (1)

Country Link
CN (1) CN111299575B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113927048A (en) * 2021-09-16 2022-01-14 首都航天机械有限公司 Selective powder laying device for selective laser melting and forming of large thin-walled part

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104668563A (en) * 2015-02-13 2015-06-03 华中科技大学 High-energy beam additive manufacturing method and equipment with high powder raw material utilization rate
CN106282517A (en) * 2016-08-31 2017-01-04 共享铸钢有限公司 The heat treatment deformation frock of Thin Wall Cylinder Blocks foundry goods and heat treatment shove charge method thereof
CN106312066A (en) * 2016-09-29 2017-01-11 首都航天机械公司 Combined base plate for selective laser melting additive manufacturing
CN106541133A (en) * 2015-09-22 2017-03-29 首都航天机械公司 A kind of method of in-situ preparation auxiliary support structure
CN106702372A (en) * 2015-11-13 2017-05-24 首都航天机械公司 Selective laser melting and forming method of titanium alloy asymmetric protection shield
CN107008904A (en) * 2017-05-18 2017-08-04 山东三迪时空三维科技有限公司 A kind of selective laser fusing dedicated variable shaping volume type device
CN108145161A (en) * 2017-12-04 2018-06-12 首都航天机械公司 A kind of auxiliary support structure for inhibiting thin-wall construction deformation
CN108372298A (en) * 2017-01-04 2018-08-07 中国航空工业集团公司北京航空制造工程研究所 A kind of profile-followed supporting deformation control method of selective laser fusing forming thin-walled parts
EP3492244A1 (en) * 2016-06-29 2019-06-05 VELO3D, Inc. Three-dimensional printing system and method for three-dimensional printing
WO2019166166A1 (en) * 2018-02-28 2019-09-06 Audi Ag Removal of the support structures from components produced by 3d printing

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104668563A (en) * 2015-02-13 2015-06-03 华中科技大学 High-energy beam additive manufacturing method and equipment with high powder raw material utilization rate
CN106541133A (en) * 2015-09-22 2017-03-29 首都航天机械公司 A kind of method of in-situ preparation auxiliary support structure
CN106702372A (en) * 2015-11-13 2017-05-24 首都航天机械公司 Selective laser melting and forming method of titanium alloy asymmetric protection shield
EP3492244A1 (en) * 2016-06-29 2019-06-05 VELO3D, Inc. Three-dimensional printing system and method for three-dimensional printing
CN106282517A (en) * 2016-08-31 2017-01-04 共享铸钢有限公司 The heat treatment deformation frock of Thin Wall Cylinder Blocks foundry goods and heat treatment shove charge method thereof
CN106312066A (en) * 2016-09-29 2017-01-11 首都航天机械公司 Combined base plate for selective laser melting additive manufacturing
CN108372298A (en) * 2017-01-04 2018-08-07 中国航空工业集团公司北京航空制造工程研究所 A kind of profile-followed supporting deformation control method of selective laser fusing forming thin-walled parts
CN107008904A (en) * 2017-05-18 2017-08-04 山东三迪时空三维科技有限公司 A kind of selective laser fusing dedicated variable shaping volume type device
CN108145161A (en) * 2017-12-04 2018-06-12 首都航天机械公司 A kind of auxiliary support structure for inhibiting thin-wall construction deformation
WO2019166166A1 (en) * 2018-02-28 2019-09-06 Audi Ag Removal of the support structures from components produced by 3d printing

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
李艳军等: "Ti2AlNb合金电子束熔透焊的数值模拟 ", 《稀有金属材料与工程》 *
董鹏等: "铝合金激光选区熔化成形技术研究现状 ", 《应用激光》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113927048A (en) * 2021-09-16 2022-01-14 首都航天机械有限公司 Selective powder laying device for selective laser melting and forming of large thin-walled part

Also Published As

Publication number Publication date
CN111299575B (en) 2022-03-18

Similar Documents

Publication Publication Date Title
US10737311B1 (en) Integrated method for forming and performance control of NiAl alloy thin-walled tubular parts
CN111168407B (en) Integrated manufacturing method of high temperature resistant thin-walled components using metal foil tape laying and blanking
CN102085555B (en) Roll forming method of TC25 titanium alloy thin-walled ring forging
CN106825859B (en) A kind of multi-layer double arc additive manufacturing method for aluminum alloy structural parts
CN102861788B (en) Hot shaping method of large-specification titanium plate
MX2010006654A (en) Method for producing highly mechanically demanded pieces and specially tools from low cost ceramics or polymers, like concrete, by casting the desired shape and then coating with a metallic or high property ceramic layer.
CN109778126A (en) A kind of preparation method of high-densit Ultra-fine Grained large scale molybdenum target material
CN103949646A (en) Preparation method for Nb-Si base ultra-temperature alloy turbine vane
CN111151753B (en) Method for manufacturing shear deformation type phase change crack resistance by laser additive manufacturing
CN107457469B (en) Self-compression electric arc additive manufacturing method for carbon steel structural part
CN111299575A (en) A conformal adjustment substrate for laser selective melting and forming of large-sized thin-walled structural parts
CN108620588A (en) A kind of laser metal 3D printing method of the aperiodicity layer with effect
CN109772890A (en) A kind of Ultra-fine Grained milling method of large scale high temperature alloy bar
CN106513453A (en) Amorphous alloy hot extrusion device and method
CN112916704A (en) Thin-wall curved surface die-free spinning forming method based on aluminum alloy welded jointed board
CN113732310B (en) Method for preparing complex thin-walled components by laser metal deposition and follow-up rolling
CN105252003B (en) Additive manufacturing method for aircraft wing spar components
CN116079342B (en) A method for manufacturing a high uniformity and high grain size welded titanium cylinder for cathode roller
CN103212572A (en) Method for rolling magnesium alloy plate
CN108746375A (en) A method of material is increased based on electric arc and prepares hot stamping die insert with laser melting coating
CN110976522A (en) Composite roll collar of kocks rolling mill and manufacturing method
CN109396204B (en) Plate batch modular lateral extrusion forming device and method
JP3233854U (en) Pretreatment equipment and pretreatment method for structural steel
CN104399839A (en) Continuous roll forming process and device for stainless steel corrugated plate of heat exchanger
CN111468726A (en) A manufacturing method of channel member based on selective laser melting and electrolytic machining

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