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14 UV-irradiation UV-cationic cure UV-cationic cure UV-cationic cure Thermal cationic Reaction heat cure Thermal cationic Cation Reaction heat cure Cation (a) UV-curing of surface is (b) Chain-curing continues (c) All resin are cured by trigger of chain-curing. toward depth direction. chain-curing, even (Thermal cations are generated.) non-irradiation part. Cure Reaction Front Closed Mold Driving Energy Input UV, IR and so on (Energy-ray) ray) Heat CF Fabric + UV curable resin
15 Stiffness (Elastic Modulus) Splice Section (Bearing Strength) Flange (Tensile/Compressive Modulus) Web (Shear Modulus) Mechanical Properties Tensile Strength (MPa) Modulus (GPa) Compressive Strength (MPa) Modulus (GPa) Bearing Strength (MPa) CAI * Strength (MPa) *Energy level:6.7j/mm Results
16 Loading Point Support Point
17 Flange Web H18 Tg Tg J/mm
18 I I I R 1 2 (a) Optical loss measurement FBG sensor Strain measurement I F Resin I T FBG Refractive index measurement (c) FBG (b) 2 (d) FBG 2nd n d
19 30mm 30mm 30mm Fiber1 Fiber2 Fiber3 30mm FBG Resin Cure direction Thermocouple 1 Thermocouple 2 Thermocouple 3 2mm Temperature O R1 C O R2 R1 C O H O 0 R1 Time (sec.) O C R2 R1 O C O H O R1 C O R2 Temperature Strain Strain (%)
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23 3.5 mm 250 mm 250 mm
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26 Strain Probe Frequency Intensity 430 Distance 460
27 X=0.18 m X=0.32 m #3 bolt X=-0.42 m 25mm #6 bolt 150mm X=-0.28 m
![Strain [με] 2000](/docs-images/91/107223756/images/28-0.jpg "1500 1000 500 0-500")
28 Strain [με] Position [m] #3 #6
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30 Coupon specimen Double lap shear type 25 mm in width 250 mm in length Structure element type test article Skin with a hat-type stringer 300 mm in width 1000 mm in length Sub-component type test article wing box structure 2000 mm in chord 4000 mm in span 800 mm in thickness
31 Stringer Stringer / / Rib
32 / mm , , , ,000,0000 A-scan Voltage [mv] [mv] Voltage [mv] Voltage / mv Voltage / mv Voltage / mv L Time [µsec] L Time / sec. Step Step Time [µsec] Time / sec. L Step Time [µsec] Time / sec.
33 Health monitoring system FBG sensors
34 HRAGS () FBG 300 SW 18ch MEMS ASE C ASE HRAGS () FBG 300
35 1m 2m
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38 PC DAQ FBG3 AWG FBG4 FBG2 FBG1 ASE mm
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40 CFRP 1800mm500mm 16PLY FBG4 9
41 STRINGER FBG2 FBG1 FBG3 FBG4 VIEW FROM STRINGER SIDE
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43 MgRE Mg Ar mm Al 1.3 H15 H16 H17 H18 H19 H20
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50 0.2 No. (MPa) (MPa) (GPa) Z12a Z12b Z12c Z14a Z14b Z14c ()
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52 2 RS 1000kN
53 RS Mg 97 Zn 1 Y 2 Al RS Mg 97 Zn 1 Y 2 (at%) 1200mm (g/m 3 )
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67 :DAU (Data Acquisition Unit) :DEU (Data Evaluation Unit) :Outline of optical fiber
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14 FEM [1] 1992 [3] 1(a)(b) 1(c) [2] 2 ( 財 ) 日本海事協会 36 平成 14 年度 ClassNK 研究発表会
![14 FEM [1] 1992 [3] 1(a)(b) 1(c) [2] 2 ( 財 ) 日本海事協会 36 平成 14 年度 ClassNK 研究発表会](/thumbs/92/109274181.jpg "14 FEM [1] 1992 [3] 1(a)(b) 1(c) [2] 2 ( 財 ) 日本海事協会 36 平成 14 年度 ClassNK 研究発表会")
1. 1(1) 1(2)[1] 1992 [2] 1992 [3] 100 100 比率 (%) 80 60 40 変形腐食亀裂 相対損傷数 80 60 40 変形腐食亀裂 20 20 0 0 5 10 15 20 25 船齢 ( 年 ) 0 0 5 10 15 20 25 船齢 ( 年 ) (1) Ratio of Each Damage (2) Number of Damage Fig.1 Relation
75 unit: mm Fig. Structure of model three-phase stacked transformer cores (a) Alternate-lap joint (b) Step-lap joint 3 4)
3 * 35 (3), 7 Analysis of Local Magnetic Properties and Acoustic Noise in Three-Phase Stacked Transformer Core Model Masayoshi Ishida Kenichi Sadahiro Seiji Okabe 3.7 T 5 Hz..4 3 Synopsis: Methods of local
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008 stress behavior at the joint of stringer to cross beam of the steel railway bridge 1115117 1..FEM FEM 3. 4. ABSTRACT 1. BackgroundPurpose The occurrence of fatigue crack is reported in the joint of
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Preparation of Functional Nonwoven Fabric KAMIKO Utilizing Wasted Tea Leaves Tetsuya Takahashi 1, Wakako Kasai 2, and Tetsuo Kondo 2 1 Faculty of Education, Shimane University, 1060, Nishikawatsu-cho,
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27.2.9 TOF-SIMS SIMS TOF-SIMS SIMS Mass Spectrometer ABCDE + ABC+ DE + Primary Ions: 1 12 ions/cm 2 Molecular Fragmentation Region ABCDE ABCDE 1 15 atoms/cm 2 Molecular Desorption Region Why TOF-SIMS?
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Continuous Cooling Transformation Diagrams for Welding of Mn-Si Type 2H Steels. Harujiro Sekiguchi and Michio Inagaki Synopsis: The authors performed
Continuous Cooling Transformation Diagrams for Welding of Mn-Si Type 2H Steels. Harujiro Sekiguchi and Michio Inagaki Synopsis: The authors performed a series of researches on continuous cooling transformation
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19 σ = P/A o σ B Maximum tensile strength σ % 0.2% proof stress σ EL Elastic limit Work hardening coefficient failure necking σ PL Proportional
19 σ = P/A o σ B Maximum tensile strength σ 0. 0.% 0.% proof stress σ EL Elastic limit Work hardening coefficient failure necking σ PL Proportional limit ε p = 0.% ε e = σ 0. /E plastic strain ε = ε e
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PowerPoint プレゼンテーション
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研究成果報告書
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軸直角繰返し外力による ねじのゆるみについて ( 元 ) 信州大学工学部 賀勢晋司 2009 年 2 月 24 日 今回の内容 1. ゆるみの種類 ( 全般 ) 2. 巨視的座面滑りによる場合 ゆるみの発生機構 実験と考察 限界座面滑り 3. 微小座面滑りによる場合 ゆるみの発生機構 実験と考察 ゆ
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Graduate School of Education, Hiroshima University 1 1. 2. TG, TG-DTA 3. 4. TG 5. TG-DTA 6. TG 7. TG 8. TG 9. TG-DTA-EGA 2 3 (Thermogravimetry) TG (Derivative TG) DTG (Evolved Gas Detection) EGD (Evolved
A Practical Calculating Method on Spring Characteristics and Stresses of Coiled Wave Springs Hideki TAKAHASHI, Naoko KAWAMURA, Takahiko KUN
35 A Practical Calculating Method on Sring Characteristics and Stresses of Coiled Wave Srings Hideki TAKAHASHI, Naoko KAWAMURA, Takahiko KUNOH Coiled wave srings (CWS) are considered as multile layered
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平成 3 年 1 月 1 日 日本における超高速衝突実験の現状と将来展望 於神戸大学惑星科学研究センター 飛翔体衝突による CFRP の 3 次元変形 挙動の計測 - 材料の静的特性との関連性を求めて - 名古屋大学 大学院工学研究科化学 生物工学専攻 工学研究科附属複合材工学研究センター 1 / 19 話の内容 装置 ( 段式軽ガス加速装置 ) p. 衝突速度 7~18m/s 内部応力と内部歪計測
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Fig. 1 Experimental Apparatus Fig. 2 Typical Ion Distribution in COG-Air Flame Fig. 3 Relation between Steel Temperature and Reduction Time (a) -4furne.ce Fig. I Schematic drawing of cooling chamber Fig.
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Estimation of Photovoltaic Module Temperature Rise Motonobu Yukawa, Member, Masahisa Asaoka, Non-member (Mitsubishi Electric Corp.) Keigi Takahara, Me
Estimation of Photovoltaic Module Temperature Rise Motonobu Yukawa, Member, Masahisa Asaoka, Non-member (Mitsubishi Electric Corp.) Keigi Takahara, Member (Okinawa Electric Power Co.,Inc.) Toshimitsu Ohshiro,
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1 000 Ni-Cr Tribological Characteristics of Ni-Cr Alloy at 1 000 C in Air R&D 1 000 Ni-Cr 1 000 Ni-Cr alloy sliding tests in atmosphere at 1 000 C were carried out and the process in which a glazed oxide