MX2024010842A - Metodo para fabricar un material conico. - Google Patents

Metodo para fabricar un material conico.

Info

Publication number
MX2024010842A
MX2024010842A MX2024010842A MX2024010842A MX2024010842A MX 2024010842 A MX2024010842 A MX 2024010842A MX 2024010842 A MX2024010842 A MX 2024010842A MX 2024010842 A MX2024010842 A MX 2024010842A MX 2024010842 A MX2024010842 A MX 2024010842A
Authority
MX
Mexico
Prior art keywords
tapered
squeezing
ring material
based superalloy
temperature
Prior art date
Application number
MX2024010842A
Other languages
English (en)
Spanish (es)
Inventor
Takeshi Ikeda
Kazuya Musha
Ryosuke Shioda
Jun OSONE
Original Assignee
Proterial 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 Proterial Ltd filed Critical Proterial Ltd
Publication of MX2024010842A publication Critical patent/MX2024010842A/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/92—Making other particular articles other parts for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D35/00—Combined processes according to or processes combined with methods covered by groups B21D1/00 - B21D31/00
    • B21D35/002—Processes combined with methods covered by groups B21D1/00 - B21D31/00
    • B21D35/005—Processes combined with methods covered by groups B21D1/00 - B21D31/00 characterized by the material of the blank or the workpiece
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02—Stamping using rigid devices or tools
    • B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/02—Stamping using rigid devices or tools
    • B21D22/025—Stamping using rigid devices or tools for tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D41/00—Application of procedures in order to alter the diameter of tube ends
    • B21D41/04—Reducing; Closing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D51/00—Making hollow objects
    • B21D51/02—Making hollow objects characterised by the structure of the objects
    • B21D51/10—Making hollow objects characterised by the structure of the objects conically or cylindrically shaped objects
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K21/00—Making hollow articles not covered by a single preceding sub-group
    • B21K21/12—Shaping end portions of hollow articles
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/40—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for rings; for bearing races
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/172—Copper alloys
    • F05D2300/1723—Nickel-Copper alloy, e.g. Monel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/177—Ni - Si alloys

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Forging (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
MX2024010842A 2022-03-16 2023-02-21 Metodo para fabricar un material conico. MX2024010842A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2022041544 2022-03-16
PCT/JP2023/006262 WO2023176333A1 (ja) 2022-03-16 2023-02-21 テーパーリング素材の製造方法

Publications (1)

Publication Number Publication Date
MX2024010842A true MX2024010842A (es) 2024-09-11

Family

ID=88023378

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2024010842A MX2024010842A (es) 2022-03-16 2023-02-21 Metodo para fabricar un material conico.

Country Status (6)

Country Link
US (1) US20250114839A1 (https=)
EP (1) EP4494776A4 (https=)
JP (1) JP7502727B2 (https=)
CN (1) CN118871223A (https=)
MX (1) MX2024010842A (https=)
WO (1) WO2023176333A1 (https=)

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2357110A (en) * 1941-09-15 1944-08-29 Smith Corp A O Method of making bombshells
JPS635843A (ja) 1986-06-27 1988-01-11 Kawasaki Steel Corp 大型リングの口絞り鍛造方法
JPS63317231A (ja) 1987-06-22 1988-12-26 Kawasaki Steel Corp 鍛造リングの口絞り成形方法
ITVI20050010A1 (it) 2005-01-17 2006-07-18 I M Z Spa Metodo per la fabbricazione di un elemento balistico inerte per esercitazioni ed elemento balistico inerte fabbricato con tale metodo
WO2008106858A1 (fr) * 2007-03-05 2008-09-12 Guizhou Anda Aviation Forging Co., Ltd. Procédé de forgeage quasi-isothermique, à l'air, d'une pièce forgée en forme de disque de superalliages à base de nickel
CN101279349A (zh) * 2008-04-23 2008-10-08 贵州航宇科技发展有限公司 镍基高温合金锥形环锻件的辗轧成形方法
JP5180669B2 (ja) 2008-05-07 2013-04-10 株式会社神戸製鋼所 口絞りシェルの製造方法
FR2935623B1 (fr) * 2008-09-05 2011-12-09 Snecma Procede de fabrication d'une piece thermomecanique de revolution circulaire comportant un substrat porteur a base de titane revetu d'acier ou superalliage, carter de compresseur de turbomachine resistant au feu de titane
CN102513442B (zh) * 2011-11-24 2014-02-05 贵州安大航空锻造有限责任公司 高温合金矩形环轧件热胀形成形为异形环件的方法
JP2014047389A (ja) * 2012-08-31 2014-03-17 Hitachi Ltd 発電用ガスタービン用動翼と、熱処理方法
JP6350919B2 (ja) * 2013-03-21 2018-07-04 日立金属株式会社 リング圧延用素材の製造方法
JP6292761B2 (ja) * 2013-03-28 2018-03-14 日立金属Ｍｍｃスーパーアロイ株式会社 環状成形体の製造方法
FR3017060B1 (fr) * 2014-02-05 2016-08-26 Snecma Outillage de forgeage pour la fabrication d'une couronne laminee de forme, notamment pour la fabrication d'un disque de turbomachine
RU2679677C2 (ru) * 2014-09-01 2019-02-12 Хитачи Металз, Лтд. Способ изготовления кольцевого формованного изделия и кольцевой материал для изготовления такого изделия
JP6686803B2 (ja) * 2016-09-02 2020-04-22 日本製鉄株式会社 口絞り方法及び二相ステンレス鋼管の製造方法
JP7000907B2 (ja) * 2018-02-19 2022-01-19 日本製鉄株式会社 二相ステンレス鋼管の口絞り加工方法及び二相ステンレス鋼管を生産する方法
JP6821147B2 (ja) 2018-09-26 2021-01-27 日立金属株式会社 航空機エンジンケース用Ｎｉ基超耐熱合金及びこれからなる航空機エンジンケース
CN109530607A (zh) * 2018-12-28 2019-03-29 贵州航宇科技发展股份有限公司 一种718plus异形环锻件成形方法
JP7215343B2 (ja) * 2019-06-07 2023-01-31 日本製鉄株式会社 端部が閉塞された管部材の製造方法
CN111112526A (zh) * 2019-12-09 2020-05-08 贵州航宇科技发展股份有限公司 In718合金轴向非对称多法兰机匣环件的制造方法
US11951528B2 (en) * 2020-08-20 2024-04-09 Rolls-Royce Corporation Controlled microstructure for superalloy components
CN112589021B (zh) * 2020-11-17 2023-06-02 贵州航宇科技发展股份有限公司 一种in718合金双法兰高筒机匣环件的制造方法

Also Published As

Publication number Publication date
EP4494776A1 (en) 2025-01-22
JP7502727B2 (ja) 2024-06-19
EP4494776A4 (en) 2026-03-04
CN118871223A (zh) 2024-10-29
JPWO2023176333A1 (https=) 2023-09-21
WO2023176333A1 (ja) 2023-09-21
US20250114839A1 (en) 2025-04-10

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