CN104220211A - 部件孔处理方法以及具有经过处理的孔的航空航天部件 - Google Patents

部件孔处理方法以及具有经过处理的孔的航空航天部件 Download PDF

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Publication number
CN104220211A
CN104220211A CN201380017792.7A CN201380017792A CN104220211A CN 104220211 A CN104220211 A CN 104220211A CN 201380017792 A CN201380017792 A CN 201380017792A CN 104220211 A CN104220211 A CN 104220211A
Authority
CN
China
Prior art keywords
hole
diameter
component
expanding
expansion process
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
CN201380017792.7A
Other languages
English (en)
Chinese (zh)
Inventor
D.C.斯拉维克
B.H.劳勒斯
R.H.范斯通
G.R.格维德
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN104220211A publication Critical patent/CN104220211A/zh
Pending legal-status Critical Current

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Classifications

    • 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
    • C21D7/00—Modifying the physical properties of iron or steel by deformation
    • C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
    • C21D7/04—Modifying the physical properties of iron or steel by deformation by cold working of the surface
    • C21D7/06—Modifying the physical properties of iron or steel by deformation by cold working of the surface by shot-peening or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P9/00—Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings; Features of such surfaces not otherwise provided for, their treatment being unspecified
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P9/00—Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings; Features of such surfaces not otherwise provided for, their treatment being unspecified
    • B23P9/02—Treating or finishing by applying pressure, e.g. knurling
    • B23P9/025—Treating or finishing by applying pressure, e.g. knurling to inner walls of holes by using axially moving tools
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P9/00—Treating or finishing surfaces mechanically, with or without calibrating, primarily to resist wear or impact, e.g. smoothing or roughening turbine blades or bearings; Features of such surfaces not otherwise provided for, their treatment being unspecified
    • B23P9/04—Treating or finishing by hammering or applying repeated pressure
    • 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
    • C21D7/00—Modifying the physical properties of iron or steel by deformation
    • C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
    • 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
    • C21D7/00—Modifying the physical properties of iron or steel by deformation
    • C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
    • C21D7/04—Modifying the physical properties of iron or steel by deformation by cold working of the surface
    • C21D7/08—Modifying the physical properties of iron or steel by deformation by cold working of the surface by burnishing or the like
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12361—All metal or with adjacent metals having aperture or cut
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Drilling And Boring (AREA)
  • Laser Beam Processing (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
CN201380017792.7A 2012-03-29 2013-03-15 部件孔处理方法以及具有经过处理的孔的航空航天部件 Pending CN104220211A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/434320 2012-03-29
US13/434,320 US20130260168A1 (en) 2012-03-29 2012-03-29 Component hole treatment process and aerospace component with treated holes
PCT/US2013/032099 WO2014007861A1 (en) 2012-03-29 2013-03-15 Component hole treatment process and aerospace component with treated holes

Publications (1)

Publication Number Publication Date
CN104220211A true CN104220211A (zh) 2014-12-17

Family

ID=49235434

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380017792.7A Pending CN104220211A (zh) 2012-03-29 2013-03-15 部件孔处理方法以及具有经过处理的孔的航空航天部件

Country Status (7)

Country Link
US (1) US20130260168A1 (https=)
EP (1) EP2830823A1 (https=)
JP (1) JP2015519208A (https=)
CN (1) CN104220211A (https=)
BR (1) BR112014023177A8 (https=)
CA (1) CA2867859A1 (https=)
WO (1) WO2014007861A1 (https=)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104607889A (zh) * 2015-01-13 2015-05-13 哈尔滨飞机工业集团有限责任公司 一种双曲面成型模工装的制造方法
CN106270783A (zh) * 2016-09-21 2017-01-04 浙江申吉钛业股份有限公司 提高飞行器螺钉孔技术寿命的方法及装置
CN108661720A (zh) * 2017-03-28 2018-10-16 通用电气公司 用于在发动机构件中重新分配残余应力的方法
CN112122488A (zh) * 2019-06-24 2020-12-25 盖瑞特交通一公司 在离心式压缩机轮盘的中心孔的非完整部分上产生压缩残余环向应力区的方法和压缩机轮盘
CN112593072A (zh) * 2020-12-10 2021-04-02 北京航空航天大学 一种紧固孔加工强化方法
CN114599483A (zh) * 2019-10-25 2022-06-07 赛峰直升机发动机公司 用于通孔的冷膨胀的装置

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3036988B1 (fr) * 2015-06-08 2017-06-16 Airbus Operations Sas Outil abrasif pour alesage
JP2018009550A (ja) * 2016-07-15 2018-01-18 川崎重工業株式会社 ガスタービンエンジンの冷却構造およびその製造方法
US10603764B2 (en) 2017-05-26 2020-03-31 General Electric Company Burnishing tool and method of manufacturing the same
FR3081357A1 (fr) * 2018-05-23 2019-11-29 Airbus Operations Outil d’expansion a froid d’un alesage a travers une piece.
US10882158B2 (en) * 2019-01-29 2021-01-05 General Electric Company Peening coated internal surfaces of turbomachine components
CN113579663A (zh) * 2021-09-26 2021-11-02 中国航发北京航空材料研究院 一种提高2124-t851铝合金带孔航空零件疲劳寿命的方法
US11648632B1 (en) * 2021-11-22 2023-05-16 Garrett Transportation I Inc. Treatment process for a centrifugal compressor wheel to extend low-cycle fatigue life
CN118703751B (zh) * 2024-06-05 2026-04-07 清华大学 一种强化装置、结构、车床设备及强化方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR754930A (fr) * 1933-04-28 1933-11-16 Alos Ab Procédé de préparation de morceaux de carton destinés à la confection de boîtes pliantes en carton
CN1905986A (zh) * 2004-01-21 2007-01-31 国立大学法人丰桥技术科学大学 超微细晶体层生成方法、具有利用该超微细晶体层生成方法生成的超微细晶体层的机械部件、制造该机械部件的机械部件制造方法、及纳米晶体层生成方法、具有利用该纳米晶体层生成方法生成的纳米晶体层的机械部件、制造该机械部件的机械部件制造方法
US20080047320A1 (en) * 2006-08-25 2008-02-28 Northrop Grumman Corporation Device and method for sequentially cold working and reaming a hole
US20100287776A1 (en) * 2007-05-09 2010-11-18 Airbus Operations (Societe Par Actions Simplifiee) Method for assembling a part of a metal material and a part of a composite material using a fastener
US20110126943A1 (en) * 2007-08-04 2011-06-02 Mtu Aero Engines Gmbh Method for joining and joined connection of two components made of a metal material

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007055378B4 (de) * 2007-11-19 2017-06-29 Airbus Defence and Space GmbH Verfahren und Vorrichtung zur Randschichtverfestigung von Bohrungen und Bohrungsanordnung mit randschichtverfestigter Bohrung
US10010983B2 (en) * 2008-03-07 2018-07-03 Fatigue Technology, Inc. Expandable member with wave inhibitor and methods of using the same
FR2937654A1 (fr) * 2008-10-28 2010-04-30 Snecma Procede de traitement de pieces metalliques pour en ameliorer la tenue en fatigue
FR2956601B1 (fr) * 2010-02-22 2012-06-01 Snecma Procede et dispositif pour renforcer, par plastification, l'alesage d'un disque de turbomachine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR754930A (fr) * 1933-04-28 1933-11-16 Alos Ab Procédé de préparation de morceaux de carton destinés à la confection de boîtes pliantes en carton
CN1905986A (zh) * 2004-01-21 2007-01-31 国立大学法人丰桥技术科学大学 超微细晶体层生成方法、具有利用该超微细晶体层生成方法生成的超微细晶体层的机械部件、制造该机械部件的机械部件制造方法、及纳米晶体层生成方法、具有利用该纳米晶体层生成方法生成的纳米晶体层的机械部件、制造该机械部件的机械部件制造方法
US20080047320A1 (en) * 2006-08-25 2008-02-28 Northrop Grumman Corporation Device and method for sequentially cold working and reaming a hole
US20100287776A1 (en) * 2007-05-09 2010-11-18 Airbus Operations (Societe Par Actions Simplifiee) Method for assembling a part of a metal material and a part of a composite material using a fastener
US20110126943A1 (en) * 2007-08-04 2011-06-02 Mtu Aero Engines Gmbh Method for joining and joined connection of two components made of a metal material

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104607889A (zh) * 2015-01-13 2015-05-13 哈尔滨飞机工业集团有限责任公司 一种双曲面成型模工装的制造方法
CN106270783A (zh) * 2016-09-21 2017-01-04 浙江申吉钛业股份有限公司 提高飞行器螺钉孔技术寿命的方法及装置
CN108661720A (zh) * 2017-03-28 2018-10-16 通用电气公司 用于在发动机构件中重新分配残余应力的方法
CN112122488A (zh) * 2019-06-24 2020-12-25 盖瑞特交通一公司 在离心式压缩机轮盘的中心孔的非完整部分上产生压缩残余环向应力区的方法和压缩机轮盘
CN114599483A (zh) * 2019-10-25 2022-06-07 赛峰直升机发动机公司 用于通孔的冷膨胀的装置
CN112593072A (zh) * 2020-12-10 2021-04-02 北京航空航天大学 一种紧固孔加工强化方法

Also Published As

Publication number Publication date
CA2867859A1 (en) 2014-01-09
BR112014023177A2 (https=) 2017-06-20
EP2830823A1 (en) 2015-02-04
US20130260168A1 (en) 2013-10-03
WO2014007861A1 (en) 2014-01-09
BR112014023177A8 (pt) 2017-07-25
JP2015519208A (ja) 2015-07-09

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
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Application publication date: 20141217