CN106623927A - Nuclear power fuel assembly tube socket laser additional material forming manufacturing method - Google Patents

Nuclear power fuel assembly tube socket laser additional material forming manufacturing method Download PDF

Info

Publication number
CN106623927A
CN106623927A CN201611144773.2A CN201611144773A CN106623927A CN 106623927 A CN106623927 A CN 106623927A CN 201611144773 A CN201611144773 A CN 201611144773A CN 106623927 A CN106623927 A CN 106623927A
Authority
CN
China
Prior art keywords
nuclear power
laser
power fuel
manufacture method
fuel component
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.)
Pending
Application number
CN201611144773.2A
Other languages
Chinese (zh)
Inventor
马渊
杨松涛
刘文涛
罗峰
康泰峰
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 North Nuclear Fuel Co Ltd
Original Assignee
China North Nuclear Fuel 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 North Nuclear Fuel Co Ltd filed Critical China North Nuclear Fuel Co Ltd
Priority to CN201611144773.2A priority Critical patent/CN106623927A/en
Publication of CN106623927A publication Critical patent/CN106623927A/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20—Direct sintering or melting
    • B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30—Process control
    • B22F10/36—Process control of energy beam parameters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30—Process control
    • B22F10/36—Process control of energy beam parameters
    • B22F10/366—Scanning parameters, e.g. hatch distance or scanning strategy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60—Treatment of workpieces or articles after build-up
    • B22F10/64—Treatment of workpieces or articles after build-up by thermal means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/60—Treatment of workpieces or articles after build-up
    • B22F10/66—Treatment of workpieces or articles after build-up by mechanical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE 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
    • B33Y10/00—Processes of additive manufacturing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE 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
    • B33Y80/00—Products made by additive manufacturing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30—Process control
    • B22F10/32—Process control of the atmosphere, e.g. composition or pressure in a building chamber
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24—After-treatment of workpieces or articles
    • B22F2003/248—Thermal after-treatment
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00—Technologies related to metal processing
    • Y02P10/25—Process efficiency

Landscapes

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

Abstract

The invention provides a nuclear power fuel assembly tube socket laser additional material forming manufacturing method. The method comprises the steps that 1, three-dimensional model design is performed on tube socket drawing paper to obtain a three-dimensional entity model; 2, support adding processing is performed on the suspended position of the obtained model; 3, layering slicing is performed on the model according to the certain thickness; laser powder, laser scanning speed and laser scanning interval parameters of an inner part of each layer of slices are designed; 4, the parameter data obtained in the step 3 is guided into laser selective melting forming equipment, base material leveling and gas washing operation are performed, and parts are started to be manufactured; 5, after the parts are manufactured, thermal treatment is performed on the parts, and internal stress of the parts is removed; 6, linear cutting is adopted for separating the parts from the base material. The pressurized water reactor nuclear power fuel assembly tube socket is rapidly repaired, and integral forming of the tube socket is achieved; the manufacturing period is equal to or shorter than 120 h, the tensile strength is 30% or more higher than that of a tube socket manufactured through a traditional technology, and the material utilization rate is larger than 99.0%.

Description

Nuclear power fuel component base laser gain material moulding manufacture method
Technical field
The invention belongs to nuclear power fuel component manufacturing technology field, and in particular to a kind of compressed water reactor nuclear power fuel assembly The laser gain material moulding manufacture method of seat.
Background technology
Base is one of vitals of compressed water reactor nuclear power fuel assembly, and traditional handicraft has 2 kinds, and one using rolling block base Material, directly carries out machining preparation, and two carry out split shaping using the method for hot investment casting, are then processed again, two kinds The operation of processing method is numerous and diverse, and difficulty is larger.Simultaneously also there is utilization rate of raw materials low, the process exploitation cycle in conventional machining process Long the problems such as.
The preparation of base is carried out using laser gain material forming technique, conventional machining process complex procedures and material can be solved The low problem of yield, realizes that base is integrally formed in preparation process, simplifies preparation technology, it is ensured that the integrality of part, Preparation efficiency, and its utilization rate of raw materials are improve up to more than 99%.
The content of the invention
It is an object of the invention to provide a kind of nuclear power fuel component base laser gain material moulding manufacture method, it passes through to swash Light increasing material manufacturing method, quickly prepares compressed water reactor nuclear power fuel assembly base, realizes being integrally formed for base.
Realize the technical scheme of the object of the invention：A kind of nuclear power fuel component base laser gain material moulding manufacture method, should Method comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；
Step 2) to step 1) gained model overhead positions carry out plus support process；
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；Part in per layer of section of design Laser power, laser scanning speed and laser scanning spacing parameter；
Step 4) by step 3) parameters obtained data import in the melt-forming equipment of selective laser, carry out base material leveling, wash Gas operate, start to prepare part, according to step 3) parameter in the certain thickness spherical powder of substrate surface place Min layers, swashed Light is sintered；
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；
Step 6) part is carried out using wire cutting separate with base material.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 3) in, point Thickness degree is 0.04mm～0.06mm.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 3) in, swash Luminous power is 220W～260W, laser scanning speed 900mm/s～1100mm/s and laser scanning spacing 0.11mm～0.15mm.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 4) in, adopt Spherical powder is 304L stainless steel spherical powders, 20～60 μm of granularity.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 4) in, base Material adopts 304L stainless steels.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 4) in, wash Gas operation is that the indoor oxygen content of shaping is adjusted to into below 1000ppm.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 4) in, base Material leveling is referred to, it is ensured that opposing parallel between powdering scraper and molded substrate.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 5) in, heat It is 1050 DEG C～1200 DEG C to process holding temperature, and heating rate≤10 DEG C/min, protective atmosphere is argon gas.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 2) in, hang Empty position refers to base from bottom to top successively in forming process, portion not phase between previous layer cross section and latter layer cross section Region of the coincidence size more than 2mm.
A kind of nuclear power fuel component base laser gain material moulding manufacture method as above, its described step 1) in, three Dimension module is designed with software for Pro/E, UG or Solidwork.
Effect of the invention is that：The present invention quickly prepares compressed water reactor nuclear power fuel stack by laser gain material manufacture method Part base, realizes being integrally formed for base.Obtained base of the invention, its manufacturing cycle is≤120h, and its tensile strength is than passing It is high by more than 30% that system technique prepares base, and stock utilization is more than 99.0%.
Description of the drawings
Fig. 1 is the base material object photo that laser gain material is molded manufacture.
Specific embodiment
Below in conjunction with the accompanying drawings with specific embodiment to a kind of nuclear power fuel component base laser gain material of the present invention into Type manufacture method is further described.
Embodiment 1
A kind of nuclear power fuel component base laser gain material moulding manufacture method of the present invention, it comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；Threedimensional model is designed with Software is Pro/E.
Step 2) to step 1) overhead positions of gained model carry out 45 ° of solid supports and process；Overhead positions refer to base From bottom to top successively in forming process, the portion size that do not coincide between previous layer cross section and latter layer cross section is more than The region of 2mm.
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；Part in per layer of section of design Laser power, laser scanning speed and laser scanning spacing parameter；Wherein, lift height is 0.05mm, laser power be 255W, Laser scanning speed 960mm/s and laser scanning spacing 0.11mm.
Step 4) by step 3) parameters obtained data are imported in the melt-forming equipment of selective laser；
Base material leveling is carried out first, it is ensured that opposing parallel between powdering scraper and molded substrate, until powdering scraper and base Gap is≤0.05mm between material, then carries out scrubbing operations, and gas washing is carried out to being molded interior using argon gas, when shaping indoor oxygen Content for≤1000ppm when, unlatching equipment carries out part preparation；According to step 3) parameter it is necessarily thick in substrate surface place Min layers The spherical powder of degree, is carried out laser sintered；Base material adopts 304L stainless steel spherical powders using 304L stainless steels, spherical powder, 40～50 μm of granularity.
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；With 10 DEG C/heating rate of min is warming up to 1100 DEG C, is incubated 1h, is then shut off heating along with the furnace cooling, protective atmosphere is argon gas in stove.
Step 6) part is carried out using wire cutting separate with base material.
The base that test is prepared by above-mentioned process, as shown in figure 1, its manufacturing cycle is 108h, dimensional accuracy is full Sufficient base use requirement, its tensile strength is 676MPa, and stock utilization is 99.1%.
Embodiment 2
A kind of nuclear power fuel component base laser gain material moulding manufacture method of the present invention, it comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；Threedimensional model is designed with Software is UG.
Step 2) to step 1) gained model overhead positions carry out plus support process；Overhead positions refer to base from lower and On successively in forming process, portion does not coincide area of the size more than 2mm between previous layer cross section and latter layer cross section Domain.
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；Part in per layer of section of design Laser power, laser scanning speed and laser scanning spacing parameter；Lift height is 0.04mmmm, and laser power is 220W, swashs Optical scanning speed 900mm/s and laser scanning spacing 0.11mm.
Step 4) by step 3) parameters obtained data import in the melt-forming equipment of selective laser, carry out base material leveling, wash Gas is operated；Start to prepare part, according to step 3) parameter in the certain thickness spherical powder of substrate surface place Min layers, swashed Light is sintered；
Base material leveling is referred to, it is ensured that opposing parallel between powdering scraper and molded substrate.
Scrubbing operations are that the indoor oxygen content of shaping is adjusted to into below 1000ppm.
Base material adopts 304L stainless steel spherical powders, 20～30 μm of granularity using 304L stainless steels, spherical powder.
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；Heat treatment Holding temperature is 1050 DEG C, and heating rate≤10 DEG C/min are incubated 2h, and protective atmosphere is argon gas.
Step 6) part is carried out using wire cutting separate with base material.
Embodiment 3
A kind of nuclear power fuel component base laser gain material moulding manufacture method of the present invention, it comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；Threedimensional model is designed with Software is Solidwork.
Step 2) to step 1) gained model overhead positions carry out plus support process；Overhead positions refer to base from lower and On successively in forming process, portion does not coincide area of the size more than 2mm between previous layer cross section and latter layer cross section Domain.
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；Part in per layer of section of design Laser power, laser scanning speed and laser scanning spacing parameter；Lift height is 0.06mm, and laser power is 260W, laser Sweep speed 1100mm/s and laser scanning spacing 0.15mm.
Step 4) by step 3) parameters obtained data import in the melt-forming equipment of selective laser, carry out base material leveling, wash Gas is operated；Start to prepare part, according to step 3) parameter in the certain thickness spherical powder of substrate surface place Min layers, swashed Light is sintered；
Base material leveling is referred to, it is ensured that opposing parallel between powdering scraper and molded substrate.
Scrubbing operations are that the indoor oxygen content of shaping is adjusted to into below 1000ppm.
Base material adopts 304L stainless steel spherical powders, 50～60 μm of granularity using 304L stainless steels, spherical powder.
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；Heat treatment Holding temperature is 1200 DEG C, and heating rate≤10 DEG C/min are incubated 0.5h, and protective atmosphere is argon gas.
Step 6) part is carried out using wire cutting separate with base material.
Embodiment 4
A kind of nuclear power fuel component base laser gain material moulding manufacture method of the present invention, it comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；Threedimensional model is designed with Software is Pro/E.
Step 2) to step 1) overhead positions of gained model carry out 45 ° of solid supports and process；Overhead positions refer to base From bottom to top successively in forming process, the portion size that do not coincide between previous layer cross section and latter layer cross section is more than The region of 2mm.
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；Part in per layer of section of design Laser power, laser scanning speed and laser scanning spacing parameter；Wherein, lift height is 0.05mm, laser power be 250W, Laser scanning speed 1000mm/s and laser scanning spacing 0.12mm.
Step 4) by step 3) parameters obtained data are imported in the melt-forming equipment of selective laser；
Base material leveling is carried out first, it is ensured that opposing parallel between powdering scraper and molded substrate, until powdering scraper and base Gap is≤0.05mm between material, then carries out scrubbing operations, and gas washing is carried out to being molded interior using argon gas, when shaping indoor oxygen Content for≤1000ppm when, unlatching equipment carries out part preparation；Base material adopts 304L not using 304L stainless steels, spherical powder Rust steel ball shape powder, 20～60 μm of granularity.
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；With 8 DEG C/ The heating rate of min is warming up to 1200 DEG C, is incubated 1h, is then shut off heating along with the furnace cooling, and protective atmosphere is argon gas in stove.
Step 6) part is carried out using wire cutting separate with base material.
The base that test is prepared by above-mentioned process, dimensional accuracy meets base use requirement, and stock utilization is 99%.
Embodiments of the invention are explained in detail above, above-mentioned embodiment is only most highly preferred embodiment of the invention, But the present invention is not limited to above-described embodiment, in the ken that those of ordinary skill in the art possess, can with Various changes can be made on the premise of without departing from present inventive concept.

Claims (10)

1. a kind of nuclear power fuel component base laser gain material moulding manufacture method, it is characterised in that：The method comprises the steps：
Step 1) base drawing is carried out into threedimensional model design, it is designed to three-dimensional entity model；
Step 2) to step 1) gained model overhead positions carry out plus support process；
Step 3) by step 2) gained model carries out hierarchy slicing according to certain thickness；The laser of part in per layer of section of design Power, laser scanning speed and laser scanning spacing parameter；
Step 4) by step 3) parameters obtained data are imported in the melt-forming equipment of selective laser, carry out base material leveling, gas washing behaviour Make, start to prepare part, according to step 3) parameter in the certain thickness spherical powder of substrate surface place Min layers, carry out laser burning Knot；
Step 5) in step 4) prepare part after the completion of, part is heat-treated, remove inside parts stress；
Step 6) part is carried out using wire cutting separate with base material.
2. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 3) in, lift height is 0.04mm～0.06mm.
3. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 3) in, laser power is 220W～260W, laser scanning speed 900mm/s～1100mm/s and laser scanning spacing 0.11mm～0.15mm.
4. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 4) in, the spherical powder for adopting is 304L stainless steel spherical powders, 20～60 μm of granularity.
5. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 4) in, base material adopts 304L stainless steels.
6. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 4) in, scrubbing operations are that the indoor oxygen content of shaping is adjusted to into below 1000ppm.
7. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 4) in, base material leveling is referred to, it is ensured that opposing parallel between powdering scraper and molded substrate.
8. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 5) in, heat treatment holding temperature is 1050 DEG C～1200 DEG C, and heating rate≤10 DEG C/min, protective atmosphere is argon Gas.
9. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, it is characterised in that： The step 2) in, overhead positions refer to base from bottom to top successively in forming process, portion previous layer cross section with it is rear Region of the size that do not coincide between one layer cross section more than 2mm.
10. a kind of nuclear power fuel component base laser gain material moulding manufacture method according to claim 1, its feature exists In：The step 1) in, threedimensional model is designed with software for Pro/E, UG or Solidwork.
CN201611144773.2A 2016-12-13 2016-12-13 Nuclear power fuel assembly tube socket laser additional material forming manufacturing method Pending CN106623927A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611144773.2A CN106623927A (en) 2016-12-13 2016-12-13 Nuclear power fuel assembly tube socket laser additional material forming manufacturing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611144773.2A CN106623927A (en) 2016-12-13 2016-12-13 Nuclear power fuel assembly tube socket laser additional material forming manufacturing method

Publications (1)

Publication Number Publication Date
CN106623927A true CN106623927A (en) 2017-05-10

Family

ID=58825462

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611144773.2A Pending CN106623927A (en) 2016-12-13 2016-12-13 Nuclear power fuel assembly tube socket laser additional material forming manufacturing method

Country Status (1)

Country Link
CN (1) CN106623927A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109360671A (en) * 2018-10-24 2019-02-19 中国科学院上海应用物理研究所 A kind of preparation method of fuel element
CN110756800A (en) * 2018-07-26 2020-02-07 中国商用飞机有限责任公司 Additive manufacturing method
CN112828308A (en) * 2020-12-31 2021-05-25 中核北方核燃料元件有限公司 Zirconium alloy framework laser additive manufacturing method
CN112846228A (en) * 2020-12-31 2021-05-28 中核建中核燃料元件有限公司 Selective laser melting forming method for supporting-free local lower tube seat of nuclear fuel assembly
CN113000839A (en) * 2019-12-20 2021-06-22 中核北方核燃料元件有限公司 Method for 3D printing of key parts of fuel elements of 6061 aluminum alloy test reactor
CN113000840A (en) * 2019-12-20 2021-06-22 中核北方核燃料元件有限公司 Zirconium alloy framework laser additive manufacturing method
EP4094881A1 (en) * 2021-05-07 2022-11-30 Transportation IP Holdings, LLC A body and method for locating machining features in additively manufactured parts

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104259459A (en) * 2014-09-29 2015-01-07 飞而康快速制造科技有限责任公司 Method for producing titanium alloy artware by adopting selective laser melting
CN105033255A (en) * 2015-07-31 2015-11-11 南京航空航天大学 Method for directly obtaining martensite die steel through laser 3D printing technology
JP2016527390A (en) * 2013-06-11 2016-09-08 レニショウ パブリック リミテッド カンパニーＲｅｎｉｓｈａｗ Ｐｕｂｌｉｃ Ｌｉｍｉｔｅｄ Ｃｏｍｐａｎｙ Additive manufacturing apparatus and method
CN106077643A (en) * 2016-07-26 2016-11-09 西安航天发动机厂 A kind of integral manufacturing method of S 04/S 08 high strength stainless steel three-dimensional closed impeller

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016527390A (en) * 2013-06-11 2016-09-08 レニショウ パブリック リミテッド カンパニーＲｅｎｉｓｈａｗ Ｐｕｂｌｉｃ Ｌｉｍｉｔｅｄ Ｃｏｍｐａｎｙ Additive manufacturing apparatus and method
CN104259459A (en) * 2014-09-29 2015-01-07 飞而康快速制造科技有限责任公司 Method for producing titanium alloy artware by adopting selective laser melting
CN105033255A (en) * 2015-07-31 2015-11-11 南京航空航天大学 Method for directly obtaining martensite die steel through laser 3D printing technology
CN106077643A (en) * 2016-07-26 2016-11-09 西安航天发动机厂 A kind of integral manufacturing method of S 04/S 08 high strength stainless steel three-dimensional closed impeller

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110756800A (en) * 2018-07-26 2020-02-07 中国商用飞机有限责任公司 Additive manufacturing method
CN110756800B (en) * 2018-07-26 2022-02-01 中国商用飞机有限责任公司 Additive manufacturing method
CN109360671A (en) * 2018-10-24 2019-02-19 中国科学院上海应用物理研究所 A kind of preparation method of fuel element
CN109360671B (en) * 2018-10-24 2020-05-08 中国科学院上海应用物理研究所 Preparation method of fuel element
CN113000839A (en) * 2019-12-20 2021-06-22 中核北方核燃料元件有限公司 Method for 3D printing of key parts of fuel elements of 6061 aluminum alloy test reactor
CN113000840A (en) * 2019-12-20 2021-06-22 中核北方核燃料元件有限公司 Zirconium alloy framework laser additive manufacturing method
CN112828308A (en) * 2020-12-31 2021-05-25 中核北方核燃料元件有限公司 Zirconium alloy framework laser additive manufacturing method
CN112846228A (en) * 2020-12-31 2021-05-28 中核建中核燃料元件有限公司 Selective laser melting forming method for supporting-free local lower tube seat of nuclear fuel assembly
EP4094881A1 (en) * 2021-05-07 2022-11-30 Transportation IP Holdings, LLC A body and method for locating machining features in additively manufactured parts
US12097560B2 (en) 2021-05-07 2024-09-24 Transportation Ip Holdings, Llc Body and method for locating machining features in additively manufactured parts

Similar Documents

Publication Publication Date Title
CN106623927A (en) Nuclear power fuel assembly tube socket laser additional material forming manufacturing method
CN102941343B (en) Quick manufacturing method of titanium-aluminum alloy composite part
CN104084584B (en) For the Laser Scanning of high temperature alloy structural member rapid shaping
CN107971491B (en) Method for eliminating microcracks of nickel-based superalloy parts manufactured by selective electron beam melting and material increase
CN109365811B (en) Method for forming zinc alloy product by selective laser melting technology
CN102126023B (en) Powder hot isostatic pressing (HIP) forming method for titanium (Ti) alloy blisk
CN103949639A (en) Method for preparing Nb-Si based superhigh-temperature alloy by SLM (selective laser melting) technology
CN109807329B (en) Method for 3D printing of brake disc of high-speed rail by high-power laser selective melting
CN103949640B (en) A kind of electron beam RP technique is prepared the method for Nb-Si based ultra-high temperature alloy
CN103949646B (en) A kind of preparation method of Nb-Si based ultra-high temperature alloy turbine blade
CN112008079B (en) Method for improving mechanical property of 3D printing nickel-based superalloy through in-situ heat treatment
CN103495729B (en) The laser solid forming method of large scale titanium aluminium base alloy
CN107138924B (en) A kind of bimetallic dual-property titanium alloy integral blade disk manufacturing method
CN105562694A (en) Hot isostatic pressing three-control method suitable for additive manufacturing parts
CN105397086B (en) A kind of titanium alloy hollow blade laser accurate manufacturing process
CN108555295A (en) A kind of laser solid forming method of high-entropy alloy component
CN105252001B (en) A kind of laser forming manufacturing process of titanium alloy integrated impeller blade
CN108788148A (en) The method of H13 steel mold of the selective laser fusing manufacture with conformal cooling system
CN104174842A (en) Alternating magnetic field based metal wire additive-manufacturing equipment and method
CN107138726A (en) A kind of guide vane preparation method with dot matrix cooling structure
CN105386037A (en) Method for forming functional graded part through selective laser melting
CN104707931A (en) Manufacturing method for large high-temperature alloy disk-type die forging parts
CN107855522A (en) A kind of laser gain material manufacture method of porous micro-channel structure
CN102228947A (en) Finish rolling forming technique of numerical control ring rolling machine of internal long neck special-shaped wind power flange
CN109365826A (en) The compound increasing material manufacturing process of dissimilar material thrust chamber

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20170510

RJ01 Rejection of invention patent application after publication