JP2016519303A - タービンエンジンの部品の破断面を分析する方法 - Google Patents
タービンエンジンの部品の破断面を分析する方法 Download PDFInfo
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- 238000000034 method Methods 0.000 title claims abstract description 38
- 239000002245 particle Substances 0.000 claims abstract description 38
- 238000002845 discoloration Methods 0.000 claims abstract description 27
- 229910010038 TiAl Inorganic materials 0.000 claims abstract description 21
- 238000010438 heat treatment Methods 0.000 claims description 21
- 238000003776 cleavage reaction Methods 0.000 claims description 18
- 230000007017 scission Effects 0.000 claims description 18
- 239000000463 material Substances 0.000 claims description 17
- 229910045601 alloy Inorganic materials 0.000 claims description 11
- 239000000956 alloy Substances 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 230000007547 defect Effects 0.000 claims description 6
- 230000000977 initiatory effect Effects 0.000 claims description 4
- 238000003384 imaging method Methods 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 230000001590 oxidative effect Effects 0.000 claims 1
- 238000001878 scanning electron micrograph Methods 0.000 description 14
- 238000004458 analytical method Methods 0.000 description 7
- 229910001092 metal group alloy Inorganic materials 0.000 description 7
- 230000003647 oxidation Effects 0.000 description 7
- 238000007254 oxidation reaction Methods 0.000 description 7
- 238000012545 processing Methods 0.000 description 7
- 238000002474 experimental method Methods 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 230000002250 progressing effect Effects 0.000 description 3
- 230000001174 ascending effect Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000000429 assembly Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 230000000644 propagated effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000005211 surface analysis Methods 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/02—Details
- G01N3/06—Special adaptations of indicating or recording means
- G01N3/068—Special adaptations of indicating or recording means with optical indicating or recording means
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0016—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of aircraft wings or blades
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
- G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/17—Systems in which incident light is modified in accordance with the properties of the material investigated
- G01N21/25—Colour; Spectral properties, i.e. comparison of effect of material on the light at two or more different wavelengths or wavelength bands
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/08—Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
- G01N33/20—Metals
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N33/00—Investigating or analysing materials by specific methods not covered by groups G01N1/00 - G01N31/00
- G01N33/20—Metals
- G01N33/204—Structure thereof, e.g. crystal structure
- G01N33/2045—Defects
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06V—IMAGE OR VIDEO RECOGNITION OR UNDERSTANDING
- G06V20/00—Scenes; Scene-specific elements
- G06V20/60—Type of objects
- G06V20/69—Microscopic objects, e.g. biological cells or cellular parts
- G06V20/698—Matching; Classification
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/26—Electron or ion microscopes; Electron or ion diffraction tubes
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0058—Kind of property studied
- G01N2203/006—Crack, flaws, fracture or rupture
- G01N2203/0062—Crack or flaws
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0058—Kind of property studied
- G01N2203/006—Crack, flaws, fracture or rupture
- G01N2203/0067—Fracture or rupture
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- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/022—Environment of the test
- G01N2203/0222—Temperature
- G01N2203/0226—High temperature; Heating means
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/06—Indicating or recording means; Sensing means
- G01N2203/0641—Indicating or recording means; Sensing means using optical, X-ray, ultraviolet, infrared or similar detectors
- G01N2203/0647—Image analysis
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- Turbine Rotor Nozzle Sealing (AREA)
- Investigating And Analyzing Materials By Characteristic Methods (AREA)
- Sampling And Sample Adjustment (AREA)
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
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Abstract
Description
a)面上に、劈開面の位置および方位を特定して、破断または亀裂の開始領域を特定し、そして前記破断または亀裂の伝播方向を確認するステップ、
b)面を分析して、等軸粒子および/または薄層状粒子を含む領域を検出することにより、破断または亀裂が形成されたときの温度を求めるステップ、および
c)面の熱変色(複数可)を、熱変色カラーチャートのサンプル群の熱変色に基づいて比較するステップであって、前記サンプル群が、部品と同じ材料から作成され、かつ酸化熱処理を所定の温度で、所定の時間長に亘って受けて、破断または亀裂の伝播速度を求める、比較するステップ
のうちの少なくとも1つのステップを含むことを特徴とする。
Claims (10)
- 特にTiAl系合金のような非常に脆い破壊材料からなるタービンエンジンの金属部品(12)の破断面または亀裂面(10)を分析する方法であって、前記面は、破断面または壊れていない亀裂部品の実験室での切開前の亀裂面に対応し、方法は、
a)面上に、劈開面(16)の位置および方位を特定して、破断または亀裂の開始領域(26)を特定し、前記破断または亀裂の伝播方向を確認するステップ、
b)面を分析して、等軸粒子(42)および/または薄層状粒子(44)を含む領域を検出することにより、破断または亀裂が形成されたときの温度を求めるステップ、
c)面の熱変色(複数可)を、熱変色カラーチャート(49)からサンプルのものと比較するステップであって、前記サンプル群が、部品と同じ材料から作成され、かつ酸化熱処理を所定の温度で、所定の時間長に亘って受けて、破断または亀裂の伝播速度を求める、比較するステップ
のうちの少なくとも1つのステップを含み、
ステップa)、b)、およびc)はいずれかの順番で行なわれることを特徴とする、方法。 - ステップa)では更に、亀裂または破断の発生を説明することができる少なくとも1つの形状欠陥または金属欠陥(25)を確認することを特徴とする、請求項1に記載の方法。
- 方法では、ステップa)において、面のビデオ画像で、劈開面(16)の位置および方位を特定して直接突き止めることを特徴とする、請求項1から2のいずれか一項に記載の方法。
- ステップa)およびステップb)のうちの少なくとも一方のステップは、双眼ルーペを使用して、かつ/または走査電子顕微鏡撮像システムを利用して行なわれることを特徴とする、請求項1から3のいずれか一項に記載の方法。
- ステップb)では更に、破断または亀裂が、高温使用時または低温製造時に発生したかどうかについて判断することを特徴とする、請求項1から4のいずれか一項に記載の方法。
- 方法では、ステップb)において、破断または亀裂が、500℃以上または500℃以下で形成されたかどうかについて判断することを特徴とする、請求項1から5のいずれか一項に記載の方法。
- 方法では、ステップb)において、温度を、面上の等軸粒子の密度を推定することにより求めることを特徴とする、請求項1から6のいずれか一項に記載の方法。
- 方法では更に、ステップb)において、面を分析して、延性ディンプルを含む領域を検出することを特徴とする、請求項1から7のいずれか一項に記載の方法。
- ステップc)では、サンプル群が熱処理を受ける前に、切り欠き部(50)を各サンプルに形成し、次にサンプルに応力を加えて、破断または亀裂を前記切り欠き部の領域に発生させることを特徴とする、請求項1から8のいずれか一項に記載の方法。
- ステップc)では更に、部品の表面の熱変色を前述のサンプル群の熱変色と比較して、部品が到達した温度の高さを求めることを特徴とする、請求項1から9のいずれか一項に記載の方法。
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FR1353660A FR3004808B1 (fr) | 2013-04-22 | 2013-04-22 | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
FR1353660 | 2013-04-22 | ||
PCT/FR2014/050880 WO2014174179A1 (fr) | 2013-04-22 | 2014-04-11 | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
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JP2016519303A true JP2016519303A (ja) | 2016-06-30 |
JP6284624B2 JP6284624B2 (ja) | 2018-02-28 |
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US (1) | US9816905B2 (ja) |
EP (1) | EP2989455B1 (ja) |
JP (1) | JP6284624B2 (ja) |
CN (1) | CN105122054B (ja) |
BR (1) | BR112015026627B1 (ja) |
CA (1) | CA2909390C (ja) |
FR (1) | FR3004808B1 (ja) |
RU (1) | RU2668495C2 (ja) |
WO (1) | WO2014174179A1 (ja) |
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FR3004808B1 (fr) * | 2013-04-22 | 2015-04-17 | Snecma | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
CN106814086B (zh) * | 2016-12-07 | 2019-12-27 | 青岛海尔股份有限公司 | 内胆开裂分析方法 |
DE102022108913A1 (de) | 2022-04-12 | 2023-10-12 | ROOCAA UG (haftungsbeschränkt) | Verfahren zum automatischen Klassifizieren eines Schadens |
CN114878374B (zh) * | 2022-07-11 | 2022-09-20 | 天津大学 | 一种用于金属材料短裂纹及长裂纹扩展的表征方法 |
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JPH04282455A (ja) * | 1991-03-11 | 1992-10-07 | Toshiba Corp | 構造部品の保守管理方法およびその保守管理装置 |
JPH08104933A (ja) * | 1994-10-03 | 1996-04-23 | Mitsubishi Heavy Ind Ltd | チタンアルミナイド基複合材料 |
FR3004808B1 (fr) * | 2013-04-22 | 2015-04-17 | Snecma | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
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US5358686A (en) * | 1993-02-17 | 1994-10-25 | Parris Warren M | Titanium alloy containing Al, V, Mo, Fe, and oxygen for plate applications |
JP3459138B2 (ja) * | 1995-04-24 | 2003-10-20 | 日本発条株式会社 | TiAl系金属間化合物接合体およびその製造方法 |
US6970182B1 (en) * | 1999-10-20 | 2005-11-29 | National Instruments Corporation | Image acquisition system and method for acquiring variable sized objects |
FR2892811B1 (fr) * | 2005-10-28 | 2009-04-17 | Commissariat Energie Atomique | Procede et systeme de determination du parcours de propagation d'au moins une fissure a partir d'une ou de surface(s) de rupture creees par cette ou ces fissure(s). |
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- 2014-04-11 JP JP2016508212A patent/JP6284624B2/ja active Active
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- 2014-04-11 WO PCT/FR2014/050880 patent/WO2014174179A1/fr active Application Filing
- 2014-04-11 US US14/785,525 patent/US9816905B2/en active Active
Patent Citations (5)
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JPH04282455A (ja) * | 1991-03-11 | 1992-10-07 | Toshiba Corp | 構造部品の保守管理方法およびその保守管理装置 |
JPH08104933A (ja) * | 1994-10-03 | 1996-04-23 | Mitsubishi Heavy Ind Ltd | チタンアルミナイド基複合材料 |
FR3004808B1 (fr) * | 2013-04-22 | 2015-04-17 | Snecma | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
EP2989455A1 (fr) * | 2013-04-22 | 2016-03-02 | SNECMA Services | Procede d'analyse d'un facies de rupture d'une piece de turbomachine |
US9816905B2 (en) * | 2013-04-22 | 2017-11-14 | Snecma | Method for analysing a fracture face of a part of a turbine engine |
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Title |
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Publication number | Publication date |
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EP2989455B1 (fr) | 2017-01-04 |
CN105122054A (zh) | 2015-12-02 |
RU2668495C2 (ru) | 2018-10-01 |
JP6284624B2 (ja) | 2018-02-28 |
CN105122054B (zh) | 2017-04-19 |
WO2014174179A1 (fr) | 2014-10-30 |
BR112015026627A2 (pt) | 2017-07-25 |
CA2909390C (fr) | 2021-02-23 |
EP2989455A1 (fr) | 2016-03-02 |
FR3004808A1 (fr) | 2014-10-24 |
US20160061699A1 (en) | 2016-03-03 |
BR112015026627B1 (pt) | 2021-01-05 |
RU2015147608A (ru) | 2017-05-26 |
US9816905B2 (en) | 2017-11-14 |
FR3004808B1 (fr) | 2015-04-17 |
RU2015147608A3 (ja) | 2018-03-22 |
CA2909390A1 (fr) | 2014-10-30 |
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