Andere Kunden interessierten sich auch für
![Drilling of Carbon Fibre Reinforced Plastic Composites]( "Drilling of Carbon Fibre Reinforced Plastic Composites")
Drilling of Carbon Fibre Reinforced Plastic Composites53,99 €![Découpe au laser CO2 de polymère renforcé de fibres de carbone (CFRP)]( "Découpe au laser CO2 de polymère renforcé de fibres de carbone (CFRP)")
Découpe au laser CO2 de polymère renforcé de fibres de carbone (CFRP)39,99 €![Taglio laser CO2 di polimero rinforzato con fibra di carbonio (CFRP)]( "Taglio laser CO2 di polimero rinforzato con fibra di carbonio (CFRP)")
Taglio laser CO2 di polimero rinforzato con fibra di carbonio (CFRP)39,99 €![Corte a laser de CO2 de polímero reforçado com fibra de carbono (CFRP)]( "Corte a laser de CO2 de polímero reforçado com fibra de carbono (CFRP)")
Corte a laser de CO2 de polímero reforçado com fibra de carbono (CFRP)39,99 €![FEA of Drilling of CFRP Reinforced with Different Percentage of SI3N4]( "FEA of Drilling of CFRP Reinforced with Different Percentage of SI3N4")
FEA of Drilling of CFRP Reinforced with Different Percentage of SI3N426,99 €![Fatigue Damage Modeling of CFRP Strengthened Reinforced Concrete Beams]( "Fatigue Damage Modeling of CFRP Strengthened Reinforced Concrete Beams")
Fatigue Damage Modeling of CFRP Strengthened Reinforced Concrete Beams51,99 €![EFFECT OF TIG WELDING PARAMETERS ON ALUMINUM 5052 PLATE]( "EFFECT OF TIG WELDING PARAMETERS ON ALUMINUM 5052 PLATE")
EFFECT OF TIG WELDING PARAMETERS ON ALUMINUM 5052 PLATE43,99 €
The purpose of research in this book is to cut a 1mm thick Carbon fibre reinforced polymer (CFRP) by using a low power CO2 laser cutting speed (1-2mm/sec) and assist gas pressure (1-2bar). Main objective of this research work is to lower production cost of cutting by using lower laser power. A Composite of Carbon Fibre (carbon fibre + epoxy resin) with initial dimensions of 120mm×100mm×1mm was used as a material for laser cutting. A CO2 laser machine of maximum laser power 150 watt was used for laser cutting. Rectangle cuts of 50mm×40mm were cut through CFRP sheets. Samples size was determined according to response surface methodology (RSM). Factorial design was used to determine number of experiments. According to this design, number of experiment was eight. Experiments were conducted according to this design. Experiments were conducted by changing process parameters (laser power, cutting speed and assist gas pressure) simultaneously. After laser cutting, scanning electron microscope was used to see effect of process parameters on material surface in the form of microstructure. Optimization was done by the use of MINITAB software.
The purpose of research in this book is to cut a 1mm thick Carbon fibre reinforced polymer (CFRP) by using a low power CO2 laser cutting speed (1-2mm/sec) and assist gas pressure (1-2bar). Main objective of this research work is to lower production cost of cutting by using lower laser power. A Composite of Carbon Fibre (carbon fibre + epoxy resin) with initial dimensions of 120mm×100mm×1mm was used as a material for laser cutting. A CO2 laser machine of maximum laser power 150 watt was used for laser cutting. Rectangle cuts of 50mm×40mm were cut through CFRP sheets. Samples size was determined according to response surface methodology (RSM). Factorial design was used to determine number of experiments. According to this design, number of experiment was eight. Experiments were conducted according to this design. Experiments were conducted by changing process parameters (laser power, cutting speed and assist gas pressure) simultaneously. After laser cutting, scanning electron microscope was used to see effect of process parameters on material surface in the form of microstructure. Optimization was done by the use of MINITAB software.
The purpose of research in this book is to cut a 1mm thick Carbon fibre reinforced polymer (CFRP) by using a low power CO2 laser cutting speed (1-2mm/sec) and assist gas pressure (1-2bar). Main objective of this research work is to lower production cost of cutting by using lower laser power. A Composite of Carbon Fibre (carbon fibre + epoxy resin) with initial dimensions of 120mm×100mm×1mm was used as a material for laser cutting. A CO2 laser machine of maximum laser power 150 watt was used for laser cutting. Rectangle cuts of 50mm×40mm were cut through CFRP sheets. Samples size was determined according to response surface methodology (RSM). Factorial design was used to determine number of experiments. According to this design, number of experiment was eight. Experiments were conducted according to this design. Experiments were conducted by changing process parameters (laser power, cutting speed and assist gas pressure) simultaneously. After laser cutting, scanning electron microscope was used to see effect of process parameters on material surface in the form of microstructure. Optimization was done by the use of MINITAB software.