JP5403929B2 - レーザショックピーニング処理済み領域内に特徴形状部を機械加工する方法 - Google Patents
レーザショックピーニング処理済み領域内に特徴形状部を機械加工する方法 Download PDFInfo
- Publication number
- JP5403929B2 JP5403929B2 JP2008085235A JP2008085235A JP5403929B2 JP 5403929 B2 JP5403929 B2 JP 5403929B2 JP 2008085235 A JP2008085235 A JP 2008085235A JP 2008085235 A JP2008085235 A JP 2008085235A JP 5403929 B2 JP5403929 B2 JP 5403929B2
- Authority
- JP
- Japan
- Prior art keywords
- laser shock
- article
- shock peening
- laser
- machining
- 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.)
- Expired - Fee Related
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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
- C21D10/00—Modifying the physical properties by methods other than heat treatment or deformation
- C21D10/005—Modifying the physical properties by methods other than heat treatment or deformation by laser shock processing
-
- 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
- Y10T428/31—Surface property or characteristic of web, sheet or block
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Optics & Photonics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laser Beam Processing (AREA)
Description
8 ガスタービンエンジン環状シャフト
9 ドレーン孔
10 レーザショックピーニング処理システム
11 壁
12 物品
14 裸の金属表面
19 給水管
20 水ノズル
21 流水のカーテン
22 前方に延びるアーム
23 後方に延びるアーム
26 軸線
30 タービンディスク組立体
31 発生器
33 発振器
35 光学装置
39 第1の増幅器
41 第2の増幅器
43 ビーム分割器
46 内面
47 前置増幅器
48 外面
54 レーザショックピーニング処理予定表面
55 レーザショックピーニング処理済み表面
56 プレストレスト領域
58 スポット
59 アブレーティブ皮膜
60 外面
62 内面
64 中心線
70 リング
72 スカラップ状エッジ
74 スカラップ
78 円形又は湾曲部分
80 湾曲シャープエッジ
100 光伝送回路
R 曲率半径
Claims (2)
- 物品(12)をレーザショックピーニング処理する方法であって、
前記物品(12)の表面(54)をレーザショックピーニング処理して、該レーザショックピーニング処理によって付与された前記表面(54)から前記物品(12)内に延びる圧縮残留応力を有しかつ該レーザショックピーニング処理によって形成されたレーザショックピーニング処理済み表面(55)から前記物品(12)内に延びる少なくとも1つのプレストレスト領域(56)を形成するステップ
を含み、
前記プレストレスト領域(56)は、前記物品(12)の対向する間隔を置いた面(60、62)間で完全に延びるよう形成され、
前記方法は、さらに、
前記レーザショックピーニング処理後に、前記プレストレスト領域(56)において前記物品(12)を貫通する孔(9)又はスカラップ(74)を含む特徴形状部(9又は74)を機械加工するステップを含み、
前記特徴形状部(9又は74)を機械加工するステップが、前記プレストレスト領域(56)全体を貫通しまた前記物品(12)の間隔を置いた外側及び内面(60、62)間でかつ該外側及び内面を貫通して完全に延びる特徴形状部(9又は74)を機械加工することにより実施される
ことを特徴とする方法。 - 前記レーザショックピーニング処理するステップが、前記対向する間隔を置いた面(60、62)を同時にレーザショックピーニング処理して前記両面間に前記プレストレスト領域(56)を形成する
ことをさらに特徴とする、請求項1記載の方法。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/694,214 | 2007-03-30 | ||
US11/694,214 US20080241546A1 (en) | 2007-03-30 | 2007-03-30 | Machining features in laser shock peened regions |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2008260064A JP2008260064A (ja) | 2008-10-30 |
JP5403929B2 true JP5403929B2 (ja) | 2014-01-29 |
Family
ID=39540628
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008085235A Expired - Fee Related JP5403929B2 (ja) | 2007-03-30 | 2008-03-28 | レーザショックピーニング処理済み領域内に特徴形状部を機械加工する方法 |
Country Status (3)
Country | Link |
---|---|
US (1) | US20080241546A1 (ja) |
EP (1) | EP1978114B1 (ja) |
JP (1) | JP5403929B2 (ja) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922280B1 (fr) * | 2007-10-11 | 2010-02-26 | Airbus France | Procede d'assemblage pour une articulation mecanique resistante a la fatigue |
DE102008044407A1 (de) * | 2008-12-05 | 2010-06-17 | Airbus Deutschland Gmbh | Verfahren zum Vermeiden einer Rissbildung und einer Verlangsamung des Rissfortschritts in metallischen Flugzeugstrukturen mittels Laserschockstrahlen |
DE102012111022A1 (de) | 2012-11-15 | 2014-06-26 | Airbus Operations Gmbh | Verstärktes Fahrzeugstrukturteil, Fahrzeug und Verfahren |
EP2993124B1 (en) | 2014-09-08 | 2019-04-03 | Airbus Operations GmbH | Preventing cracks at bolted or riveted joints of aircraft structural parts |
CN106282532B (zh) * | 2016-08-18 | 2018-01-16 | 江苏大学 | 一种获得金属表层晶粒混合分布的激光冲击强化组合方法 |
CN106467933B (zh) * | 2016-08-29 | 2018-10-09 | 江苏大学 | 一种基于梯度晶粒的激光冲击强化方法 |
CN106319176B (zh) * | 2016-09-13 | 2018-02-27 | 江苏大学 | 一种深冷工作台、深冷激光冲击强化实验系统及其控制方法 |
CN107267742B (zh) * | 2017-05-18 | 2019-08-02 | 江苏大学 | 一种不同厚度小孔构件激光冲击强化方法 |
JP6911653B2 (ja) | 2017-09-04 | 2021-07-28 | トヨタ自動車株式会社 | 部品の製造方法及び部品 |
US11021962B2 (en) * | 2018-08-22 | 2021-06-01 | Raytheon Technologies Corporation | Turbulent air reducer for a gas turbine engine |
US10882158B2 (en) * | 2019-01-29 | 2021-01-05 | General Electric Company | Peening coated internal surfaces of turbomachine components |
CN111485094A (zh) * | 2020-04-23 | 2020-08-04 | 江苏大学 | 一种激光冲击强化金属管内外壁的装置与方法 |
CN112725613B (zh) * | 2020-12-24 | 2021-11-23 | 山东大学 | 一种非单一入射角度不等强度激光冲击加工方法 |
CN113579520B (zh) * | 2021-07-30 | 2022-07-12 | 山东大学 | 一种用于构件连接的高强度小孔的制备方法 |
Family Cites Families (35)
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US3850698A (en) | 1972-06-23 | 1974-11-26 | Ind Materials Ltd | Altering material properties |
US4401477A (en) | 1982-05-17 | 1983-08-30 | Battelle Development Corporation | Laser shock processing |
JPH024915A (ja) * | 1988-06-23 | 1990-01-09 | Mazda Motor Corp | 鋳造部材の製造方法 |
US4937421A (en) | 1989-07-03 | 1990-06-26 | General Electric Company | Laser peening system and method |
DE69020581T4 (de) | 1990-01-11 | 1996-06-13 | Battelle Memorial Institute | Verbesserung von materialeigenschaften. |
JP3036023B2 (ja) * | 1990-08-24 | 2000-04-24 | 日産自動車株式会社 | 軸部材の油穴強化方法 |
DE69431314T2 (de) * | 1993-12-07 | 2003-01-23 | Toyota Motor Co Ltd | Laser-Schock-Behandlungsverfahren unter Verwendung eines lichtabsorbierenden Filmmaterials |
JP3156530B2 (ja) * | 1993-12-07 | 2001-04-16 | トヨタ自動車株式会社 | レーザショック処理方法および装置 |
US5492447A (en) * | 1994-10-06 | 1996-02-20 | General Electric Company | Laser shock peened rotor components for turbomachinery |
US6215097B1 (en) | 1994-12-22 | 2001-04-10 | General Electric Company | On the fly laser shock peening |
US5591009A (en) | 1995-01-17 | 1997-01-07 | General Electric Company | Laser shock peened gas turbine engine fan blade edges |
US5531570A (en) | 1995-03-06 | 1996-07-02 | General Electric Company | Distortion control for laser shock peened gas turbine engine compressor blade edges |
US5584662A (en) * | 1995-03-06 | 1996-12-17 | General Electric Company | Laser shock peening for gas turbine engine vane repair |
US5620307A (en) * | 1995-03-06 | 1997-04-15 | General Electric Company | Laser shock peened gas turbine engine blade tip |
US5525429A (en) * | 1995-03-06 | 1996-06-11 | General Electric Company | Laser shock peening surface enhancement for gas turbine engine high strength rotor alloy repair |
US5735044A (en) * | 1995-12-12 | 1998-04-07 | General Electric Company | Laser shock peening for gas turbine engine weld repair |
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US5674328A (en) | 1996-04-26 | 1997-10-07 | General Electric Company | Dry tape covered laser shock peening |
US5674329A (en) | 1996-04-26 | 1997-10-07 | General Electric Company | Adhesive tape covered laser shock peening |
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US5932120A (en) | 1997-12-18 | 1999-08-03 | General Electric Company | Laser shock peening using low energy laser |
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DE19914826A1 (de) * | 1999-03-31 | 2000-09-14 | Siemens Ag | Verfahren zum Herstellen von Bauteilen für Röntgenröhren |
US6238187B1 (en) * | 1999-10-14 | 2001-05-29 | Lsp Technologies, Inc. | Method using laser shock peening to process airfoil weld repairs pertaining to blade cut and weld techniques |
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US6852179B1 (en) * | 2000-06-09 | 2005-02-08 | Lsp Technologies Inc. | Method of modifying a workpiece following laser shock processing |
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US6657160B2 (en) * | 2001-01-25 | 2003-12-02 | The Regents Of The University Of California | Laser peening of components of thin cross-section |
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US6570126B2 (en) | 2001-08-31 | 2003-05-27 | General Electric Company | Simultaneous offset dual sided laser shock peening using low energy laser beams |
US6570125B2 (en) | 2001-08-31 | 2003-05-27 | General Electric Company | Simultaneous offset dual sided laser shock peening with oblique angle laser beams |
US6875953B2 (en) * | 2002-07-29 | 2005-04-05 | Lsp Technologies, Inc. | Method using laser shock processing to provide improved residual stress profile characteristics |
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-
2007
- 2007-03-30 US US11/694,214 patent/US20080241546A1/en not_active Abandoned
-
2008
- 2008-03-20 EP EP08153123A patent/EP1978114B1/en not_active Expired - Fee Related
- 2008-03-28 JP JP2008085235A patent/JP5403929B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP1978114B1 (en) | 2012-10-03 |
JP2008260064A (ja) | 2008-10-30 |
EP1978114A1 (en) | 2008-10-08 |
US20080241546A1 (en) | 2008-10-02 |
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