BR112015004764A2 - método de determinar o limiar de não propagação para fissuras por fadiga, e, dispositivo de teste - Google Patents
método de determinar o limiar de não propagação para fissuras por fadiga, e, dispositivo de testeInfo
- Publication number
- BR112015004764A2 BR112015004764A2 BR112015004764A BR112015004764A BR112015004764A2 BR 112015004764 A2 BR112015004764 A2 BR 112015004764A2 BR 112015004764 A BR112015004764 A BR 112015004764A BR 112015004764 A BR112015004764 A BR 112015004764A BR 112015004764 A2 BR112015004764 A2 BR 112015004764A2
- Authority
- BR
- Brazil
- Prior art keywords
- masses
- rigid
- specimen
- crack
- determining
- Prior art date
Links
- 238000012360 testing method Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title abstract 2
- 238000005336 cracking Methods 0.000 title 1
- 125000004122 cyclic group Chemical group 0.000 abstract 4
- 230000005520 electrodynamics Effects 0.000 abstract 1
- 230000001902 propagating effect Effects 0.000 abstract 1
Classifications
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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
- G01N3/32—Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces
-
- 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
-
- 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
-
- 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
- G01M5/0066—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by exciting or detecting vibration or acceleration
-
- 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
- G01M5/0075—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by means of external apparatus, e.g. test benches or portable test systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M7/00—Vibration-testing of structures; Shock-testing of structures
- G01M7/02—Vibration-testing by means of a shake table
- G01M7/027—Specimen mounting arrangements, e.g. table head adapters
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/04—Analysing solids
- G01N29/043—Analysing solids in the interior, e.g. by shear waves
-
- 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
- G01N3/32—Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces
- G01N3/38—Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces generated by electromagnetic means
-
- 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
- G01N2203/0001—Type of application of the stress
- G01N2203/0005—Repeated or cyclic
-
- 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
- G01N2203/0066—Propagation of crack
-
- 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
- G01N2203/0069—Fatigue, creep, strain-stress relations or elastic constants
- G01N2203/0073—Fatigue
-
- 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
- G01N2203/026—Specifications of the specimen
- G01N2203/0262—Shape of the specimen
- G01N2203/027—Specimens with holes or notches
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/02—Indexing codes associated with the analysed material
- G01N2291/025—Change of phase or condition
- G01N2291/0258—Structural degradation, e.g. fatigue of composites, ageing of oils
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/26—Scanned objects
- G01N2291/269—Various geometry objects
- G01N2291/2693—Rotor or turbine parts
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Engineering & Computer Science (AREA)
- Analytical Chemistry (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Health & Medical Sciences (AREA)
- Electromagnetism (AREA)
- Acoustics & Sound (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
1 / 1 resumo âmãtodo de determinar o limiar de não propagaãão para fissuras por fadiga, e, dispositivo de testeâ um mã©todo de alta freqã¼ãªncia para determinar o limiar de nã£o propagaã§ã£o de fissuras por fadiga, em que uma carga cãclica (32, 32a) ã© aplicada a pelo menos um corpo de prova incluindo, em uma ã¡rea de teste (10a), um furo elãptico (12) tendo um entalhe (14) a um ã¡pice, segurado entre duas massas rãgidas (24, 26), duas placas de prã©-tensã£o rãgidas (20, 22) estando dispostas em qualquer lado de dito corpo de prova e sendo preso a cada uma das duas extremidades (20a, 22a; 20b, 22b) da mesma ã s duas massas rãgidas, a freqã¼ãªncia da carga cãclica (32, 32a) sendo escolhida como igual ã freqã¼ãªncia natural da montagem de corpo de prova/massas/placas de prã©-tensã£o de modo a gerar uma fissura por fadiga do entalhe; entã£o, quando ã© observado que a fissura deixou de se propagar, o comprimento final da fissura ã© gravado, e dito limiar de nã£o propagaã§ã£o das fissuras por fadiga ïk da th fissura por fadiga ã© determinado usando uma tabela, a carga cãclica sendo obtida por um vaso de vibrador eletrodinã¢mico presa integralmente por meio colunas rãgidas a uma estrutura apoiando as duas massas rãgidas e incluindo uma haste de impulsã£o para transmitir dita carga cãclica ã montagem de corpo de prova/massas/placas de prã©-tensã£o.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258250 | 2012-09-04 | ||
FR1258250A FR2995080B1 (fr) | 2012-09-04 | 2012-09-04 | Procede de determination en haute frequence du seuil de non-propagation de fissure par fatigue |
PCT/FR2013/052002 WO2014037654A1 (fr) | 2012-09-04 | 2013-08-30 | Procédé de détermination en haute fréquence du seuil de non-propagation de fissure par fatigue |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112015004764A2 true BR112015004764A2 (pt) | 2018-05-22 |
BR112015004764B1 BR112015004764B1 (pt) | 2021-01-12 |
Family
ID=47088985
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015004764-5A BR112015004764B1 (pt) | 2012-09-04 | 2013-08-30 | método de determinar o limiar de não propagação para fissuras por fadiga |
Country Status (11)
Country | Link |
---|---|
US (1) | US9423330B2 (pt) |
EP (1) | EP2893318A1 (pt) |
JP (1) | JP6573828B2 (pt) |
KR (1) | KR102129151B1 (pt) |
CN (1) | CN104704342B (pt) |
BR (1) | BR112015004764B1 (pt) |
CA (1) | CA2884198C (pt) |
FR (1) | FR2995080B1 (pt) |
IN (1) | IN2015DN01774A (pt) |
RU (1) | RU2627939C2 (pt) |
WO (1) | WO2014037654A1 (pt) |
Families Citing this family (21)
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CN105121579B (zh) | 2013-04-15 | 2018-01-26 | 3M创新有限公司 | 包含具有(甲基)丙烯酸酯基团和烯烃基团的交联剂的粘合剂以及方法 |
US10989640B2 (en) | 2015-03-24 | 2021-04-27 | Bell Helicopter Textron Inc. | Method for defining threshold stress curves utilized in fatigue and damage tolerance analysis |
EP3073245B1 (en) * | 2015-03-24 | 2018-09-12 | Bell Helicopter Textron Inc. | System and method for determining direct damage tolerance allowables |
US10732085B2 (en) | 2015-03-24 | 2020-08-04 | Bell Helicopter Textron Inc. | Notch treatment methods for flaw simulation |
US9513200B1 (en) * | 2015-11-04 | 2016-12-06 | Rolls-Royce Corporation | Determination of a threshold crack length |
CN105372119A (zh) * | 2015-12-05 | 2016-03-02 | 西安科技大学 | 能量控制下的振动致裂试验装置 |
CN105973983A (zh) * | 2016-05-09 | 2016-09-28 | 西北工业大学 | 等截面超声扭转疲劳试样设计方法 |
US10746640B2 (en) * | 2017-03-21 | 2020-08-18 | Textron Innovations Inc. | Methods of making a tubular specimen with a predetermined wrinkle defect |
US10744727B2 (en) | 2017-03-21 | 2020-08-18 | Textron Innovations Inc. | Methods of making a specimen with a predetermined wrinkle defect |
US10678969B2 (en) | 2017-04-21 | 2020-06-09 | General Electric Company | Usage based lifing |
CN108362597B (zh) * | 2018-02-05 | 2021-06-15 | 上海航空材料结构检测股份有限公司 | 一种金属擦蚀疲劳试验方法 |
JP7125108B2 (ja) * | 2018-08-27 | 2022-08-24 | 大起産業株式会社 | 初期損傷形成治具及び初期損傷形成方法 |
EP3859302A1 (en) * | 2018-09-27 | 2021-08-04 | Shimadzu Corporation | Material testing machine |
JP7062576B2 (ja) * | 2018-11-19 | 2022-05-06 | 株式会社鷺宮製作所 | 動特性測定装置 |
US10845267B2 (en) * | 2018-12-10 | 2020-11-24 | Efs International S.A. | Fatigue fuse mounting systems and methods |
CN110031204B (zh) * | 2019-05-16 | 2024-03-08 | 昆山丘钛微电子科技有限公司 | 抗疲劳测试治具 |
JP7485564B2 (ja) * | 2019-08-09 | 2024-05-16 | Ntn株式会社 | 算出方法、検査方法および軸受の製造方法 |
CN111929146B (zh) * | 2020-06-18 | 2023-06-13 | 广东石油化工学院 | 一种用于金属材料疲劳裂纹扩展的观测装置 |
US11680869B2 (en) * | 2020-09-03 | 2023-06-20 | University Of South Carolina | Vibration test-cell with axial load and in-situ microscopy |
CN112694008A (zh) * | 2020-12-22 | 2021-04-23 | 中冶建筑研究总院有限公司 | 一种钢吊车梁疲劳破坏的预警方法及装置 |
CN114112130B (zh) * | 2021-09-30 | 2023-04-21 | 河海大学 | 可重复测量裂纹尖端应力强度因子的装置及其方法 |
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-
2012
- 2012-09-04 FR FR1258250A patent/FR2995080B1/fr active Active
-
2013
- 2013-08-30 BR BR112015004764-5A patent/BR112015004764B1/pt not_active IP Right Cessation
- 2013-08-30 JP JP2015529104A patent/JP6573828B2/ja not_active Expired - Fee Related
- 2013-08-30 EP EP13766601.2A patent/EP2893318A1/fr active Pending
- 2013-08-30 CN CN201380046233.9A patent/CN104704342B/zh active Active
- 2013-08-30 US US14/425,999 patent/US9423330B2/en active Active
- 2013-08-30 KR KR1020157006748A patent/KR102129151B1/ko active IP Right Grant
- 2013-08-30 IN IN1774DEN2015 patent/IN2015DN01774A/en unknown
- 2013-08-30 RU RU2015112213A patent/RU2627939C2/ru active
- 2013-08-30 WO PCT/FR2013/052002 patent/WO2014037654A1/fr active Application Filing
- 2013-08-30 CA CA2884198A patent/CA2884198C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CN104704342A (zh) | 2015-06-10 |
JP6573828B2 (ja) | 2019-09-11 |
CN104704342B (zh) | 2017-11-07 |
RU2015112213A (ru) | 2016-10-27 |
CA2884198C (fr) | 2021-06-15 |
US9423330B2 (en) | 2016-08-23 |
JP2015530570A (ja) | 2015-10-15 |
KR20150047523A (ko) | 2015-05-04 |
FR2995080B1 (fr) | 2015-10-23 |
US20150219539A1 (en) | 2015-08-06 |
IN2015DN01774A (pt) | 2015-05-29 |
WO2014037654A1 (fr) | 2014-03-13 |
FR2995080A1 (fr) | 2014-03-07 |
KR102129151B1 (ko) | 2020-07-01 |
EP2893318A1 (fr) | 2015-07-15 |
BR112015004764B1 (pt) | 2021-01-12 |
CA2884198A1 (fr) | 2014-03-13 |
RU2627939C2 (ru) | 2017-08-14 |
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Legal Events
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