CA3124871C - Method for internal stress regulation in superalloy disk forgings by pre-spinning - Google Patents

Method for internal stress regulation in superalloy disk forgings by pre-spinning Download PDF

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Publication number
CA3124871C
CA3124871C CA3124871A CA3124871A CA3124871C CA 3124871 C CA3124871 C CA 3124871C CA 3124871 A CA3124871 A CA 3124871A CA 3124871 A CA3124871 A CA 3124871A CA 3124871 C CA3124871 C CA 3124871C
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CA
Canada
Prior art keywords
spinning
disk
forgings
disk forgings
internal stress
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
CA3124871A
Other languages
English (en)
French (fr)
Other versions
CA3124871A1 (en
Inventor
Beijiang ZHANG
Wenyun ZHANG
Chenggang Tian
Aihua HUANG
Guodong Zhang
Haijun Xuan
Chuanyong Chen
Shuo Huang
Heyong QIN
Qiang Tian
Ran Duan
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.)
Central Iron and Steel Research Institute
AECC Commercial Aircraft Engine Co Ltd
Gaona Aero Material Co Ltd
Zhejiang Hiro Aviation Technology Co Ltd
Original Assignee
Central Iron and Steel Research Institute
AECC Commercial Aircraft Engine Co Ltd
Gaona Aero Material Co Ltd
Zhejiang Hiro Aviation Technology 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 Central Iron and Steel Research Institute, AECC Commercial Aircraft Engine Co Ltd, Gaona Aero Material Co Ltd, Zhejiang Hiro Aviation Technology Co Ltd filed Critical Central Iron and Steel Research Institute
Publication of CA3124871A1 publication Critical patent/CA3124871A1/en
Application granted granted Critical
Publication of CA3124871C publication Critical patent/CA3124871C/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P25/00Auxiliary treatment of workpieces, before or during machining operations, to facilitate the action of the tool or the attainment of a desired final condition of the work, e.g. relief of internal stress
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/32Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring the deformation in a solid
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/0047Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes measuring forces due to residual stresses
    • 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
    • Y02P10/20Recycling

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Forging (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
CA3124871A 2020-05-19 2021-07-19 Method for internal stress regulation in superalloy disk forgings by pre-spinning Active CA3124871C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202010425506.2 2020-05-19
CN202010425506.2A CN111471944B (zh) 2020-05-19 2020-05-19 通过预旋转调控高温合金毛坯盘锻件的残余应力的方法

Publications (2)

Publication Number Publication Date
CA3124871A1 CA3124871A1 (en) 2021-11-19
CA3124871C true CA3124871C (en) 2023-09-19

Family

ID=71762562

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3124871A Active CA3124871C (en) 2020-05-19 2021-07-19 Method for internal stress regulation in superalloy disk forgings by pre-spinning

Country Status (4)

Country Link
JP (1) JP7356686B2 (ja)
CN (1) CN111471944B (ja)
CA (1) CA3124871C (ja)
RU (1) RU2769339C1 (ja)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112342368A (zh) * 2020-10-16 2021-02-09 中国航发北京航空材料研究院 一种转动法降低变形高温合金盘件残余应力的工艺方法
FR3125335B1 (fr) * 2021-07-19 2023-06-30 Gaona Aero Mat Co Ltd Méthode de réguler les contraintes résiduelles dans les pièces forgées du disque vierge du superalliage par pré-rotation
AU2021206812B1 (en) * 2021-07-20 2022-11-03 Aecc Commercial Aircraft Engine Co., Ltd. Method for Internal Stress Regulation in Superalloy Disk forgings by Pre-spinning
CN114250352B (zh) * 2021-12-22 2023-11-14 北京钢研高纳科技股份有限公司 提高高温合金盘件或环形件服役稳定性的方法及得到的盘件或环形件
CN114214510B (zh) * 2021-12-28 2024-02-06 北京钢研高纳科技股份有限公司 振动时效去除高温合金件内部残余应力的方法及其应用
CN116818555B (zh) * 2023-07-25 2024-02-02 中国航发北京航空材料研究院 镍基高温合金轮盘毛坯预旋转转速的确定方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU733957A1 (ru) * 1977-11-02 1980-05-15 За витель Вибрационна установка дл снижени остаточных напр жений
SU774904A1 (ru) * 1978-11-04 1980-10-30 Завод Сельскохозяйственного Машиностроения "Лиепайсельмаш" Способ сн ти остаточных напр жений в трубных заготовках
US4820356A (en) * 1987-12-24 1989-04-11 United Technologies Corporation Heat treatment for improving fatigue properties of superalloy articles
JP2005060735A (ja) * 2003-08-12 2005-03-10 Nippon Steel Corp 金属の疲労強度向上方法
JP2005305358A (ja) * 2004-04-23 2005-11-04 Japan Science & Technology Agency 高速回転を利用した組成傾斜装置、方法及びその方法で得られた凝縮系薄膜物質
RU2478031C2 (ru) * 2011-05-27 2013-03-27 Альберт Викторович Королев Способ релаксации остаточных напряжений
KR101698338B1 (ko) * 2015-06-30 2017-01-23 한국수력원자력 주식회사 배관 잔류응력 완화장치
CN106702136B (zh) * 2017-01-20 2018-06-05 广西大学 圆柱凸轮激励引发的弯扭耦合共振式残余应力消除装置
CN109145335B (zh) * 2017-06-28 2023-05-30 中国航发贵阳发动机设计研究所 一种通过预旋转提高轮盘低循环疲劳寿命的方法
CN108774667B (zh) * 2018-07-04 2019-11-08 中国工程物理研究院机械制造工艺研究所 一种利用热时效和振动时效协同消除应力的装置及方法
CN110423883B (zh) * 2019-08-08 2020-08-04 北京航空航天大学 一种大型环件旋转离心应力调控方法
CN110408770B (zh) * 2019-08-08 2020-07-10 北京航空航天大学 一种大型环件旋转离心残余应力调控装置
CN110551955B (zh) * 2019-08-23 2020-09-22 中国航发北京航空材料研究院 一种降低gh4169合金大尺寸盘锻件内部残余应力的方法

Also Published As

Publication number Publication date
CN111471944B (zh) 2021-07-23
RU2769339C1 (ru) 2022-03-30
JP7356686B2 (ja) 2023-10-05
CN111471944A (zh) 2020-07-31
CA3124871A1 (en) 2021-11-19
JP2022132667A (ja) 2022-09-09

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