Impact Tensile Behavior of Liquid Packaging Bag(Impact 1)
スポンサーリンク
概要
- 論文の詳細を見る
Since laminate films used for liquid packaging bags are produced by laminating very thin single films, they are easily influenced by ambient temperature; bags often break due to impact load during loading and unloading of packaged products. In this study, impact tensile tests were carried out at relatively low impact tensile speeds between v=0.20 and 1.40 m/s using a rotary impact tensile apparatus developed by us, with ambient temperature varied to six temperatures, i.e., t=0, 10, 20, 30, 40 and 50℃. The results indicate that the impact tensile strength of NY/EVA is negligibly influenced by the impact tensile speed at an ambient temperature of t=50℃, while those of NY/XA and PET/XA are influenced by the impact tensile speed.
- 一般社団法人日本機械学会の論文
- 2001-10-20
著者
-
Shimamoto Akira
Department Of Mechanical Engineering Saitama Institute Of Technology
-
Kamada Yukihiko
Taisei Lamick Co. Ltd.
-
Futase Katsunori
Taisei Lamic Co. Ltd.
-
AOKI Hiroyuki
Taisei Lamick Co., Ltd.
-
Futase Katsunori
Taisei Lamick Co. Ltd.
-
Aoki Hiroyuki
Taisei Lamick Co. Ltd.
-
Shimamoto Akira
Department of Mechanical Engineering, Saitama Institute of Technology
関連論文
- A Method of Measuring Physical Properties from Stress Fringe Values
- Study on the Development of Photoelastic Experimental Composite Material : Development of Orthotropic Material
- The Role of Cyclosporine A and Interleukin-2 in Obliterative Airway Disease in a Rat Tracheal Transplant Model
- A Basic Study of Plastic Strain Freezing by Photoplastic Experiment : Solid-Mechanics, Strength of Materials
- Pulmonary histoplasmosis as an example of imported mycoses in Japan
- OS1(2)-7(OS01W0221) Evaluation of Deformation of Sheets of Recycled Paper with Different Fiber Directions Using Electronic Speckle Pattern Interferometry
- Effect on K_I Reduction in SMA Fiber of TiNi Reinforced Epoxy Matrix Composite(Composite 3)
- Impact Tensile Behavior of Liquid Packaging Bag(Impact 1)
- Axial Multiple Crack Propagation and Crack Kinking Criteria in Pressurized Fuselage
- 113 Active Control for Stress Intensity of Crack-tip under Mixed Mode by Shape Memory TiNi Fiber Epoxy Composite
- Axial Crack Propagation and Crack Kinking Criteria in Pressurized Fuselage
- Axial Multi Crack Propagation and Crack Kinking Criteria in Pressurized Fuselage : An Experimental - Numerical Analysis(Crack Growth)
- Plastic Strain Concentration by means of Photoplasticity at a Circular Hole Edge in a Finite Sheet Subjected to Uniaxial Tension
- Optical Measurement of Principal Strains in Plastic Region