Coupled Thermomechanical Analysis of Autofrettaged and Shrink Fitted Compound Cylindrical ShellsSource: Journal of Pressure Vessel Technology:;2014:;volume( 136 ):;issue: 001::page 11204DOI: 10.1115/1.4025115Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this study, different configurations of compound multilayer cylinders subjected to autofrettage and shrinkfit processes and under combined cyclic thermal and pressure loads have been investigated and their fatigue life has been evaluated and compared. Fully coupled thermoelastic analysis is taken into consideration during the calculation of the temperature profile through the wall thickness. Finite element model for the compound twolayer cylinder has been constructed and then validated with previous work in the literature and experimental work. In the experimental work, the temperature has been measured at different locations through the thickness of a twolayer shrinkfitted cylinder (SFC), subjected to internal quasistatic and dynamic thermal loads. Besides, the hoop strain at the outer surface of the cylinder has been measured for the same thermal loads. Using the developed finite element model, the hoop stress distributions through the thickness of different configurations of the compound cylinder have been calculated under different loading conditions, including internal static pressure, internal cyclic thermal loads, and combination of these loads. The mechanical fatigue life has been calculated using ASME codes due to the internal cyclic pressure. Moreover, the stress intensity factor (SIF) has been calculated for these configurations under cyclic thermal loads or cyclic thermomechanical loads, considering thermal accumulation. The stress intensity factors for different configurations have been compared with the critical SIF which is the fracture toughness of the material. The number of stress cycles required until the SIF reaches the critical SIF has been considered as the fatigue life for each configuration. It has been found that for the cases of cyclic thermal loads and combined cyclic pressure and thermal loads, the shrinkfitting of two layers followed by the autofrettage of the assembly is the best configuration to enhance the fatigue life of the twolayer cylinder.
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| contributor author | Abdelsalam, Ossama R. | |
| contributor author | Sedaghati, Ramin | |
| date accessioned | 2017-05-09T01:11:50Z | |
| date available | 2017-05-09T01:11:50Z | |
| date issued | 2014 | |
| identifier issn | 0094-9930 | |
| identifier other | pvt_136_01_011204.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/156095 | |
| description abstract | In this study, different configurations of compound multilayer cylinders subjected to autofrettage and shrinkfit processes and under combined cyclic thermal and pressure loads have been investigated and their fatigue life has been evaluated and compared. Fully coupled thermoelastic analysis is taken into consideration during the calculation of the temperature profile through the wall thickness. Finite element model for the compound twolayer cylinder has been constructed and then validated with previous work in the literature and experimental work. In the experimental work, the temperature has been measured at different locations through the thickness of a twolayer shrinkfitted cylinder (SFC), subjected to internal quasistatic and dynamic thermal loads. Besides, the hoop strain at the outer surface of the cylinder has been measured for the same thermal loads. Using the developed finite element model, the hoop stress distributions through the thickness of different configurations of the compound cylinder have been calculated under different loading conditions, including internal static pressure, internal cyclic thermal loads, and combination of these loads. The mechanical fatigue life has been calculated using ASME codes due to the internal cyclic pressure. Moreover, the stress intensity factor (SIF) has been calculated for these configurations under cyclic thermal loads or cyclic thermomechanical loads, considering thermal accumulation. The stress intensity factors for different configurations have been compared with the critical SIF which is the fracture toughness of the material. The number of stress cycles required until the SIF reaches the critical SIF has been considered as the fatigue life for each configuration. It has been found that for the cases of cyclic thermal loads and combined cyclic pressure and thermal loads, the shrinkfitting of two layers followed by the autofrettage of the assembly is the best configuration to enhance the fatigue life of the twolayer cylinder. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Coupled Thermomechanical Analysis of Autofrettaged and Shrink Fitted Compound Cylindrical Shells | |
| type | Journal Paper | |
| journal volume | 136 | |
| journal issue | 1 | |
| journal title | Journal of Pressure Vessel Technology | |
| identifier doi | 10.1115/1.4025115 | |
| journal fristpage | 11204 | |
| journal lastpage | 11204 | |
| identifier eissn | 1528-8978 | |
| tree | Journal of Pressure Vessel Technology:;2014:;volume( 136 ):;issue: 001 | |
| contenttype | Fulltext |