fea studies for the shell a thin wall region:
DESCRIPTION
FEA Studies for the Shell A Thin Wall Region:. Run #1: Original run having E=193 GPa Run #2: Modify E of shell A by a thickness ratio of 1.18/1.5. The E of shell A become 152 GPa. (Note: The actual model shell thickness is 1.375”) - PowerPoint PPT PresentationTRANSCRIPT
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FEA Studies for the Shell A Thin Wall Region:• Run #1: Original run having E=193 GPa
• Run #2: Modify E of shell A by a thickness ratio of 1.18/1.5. The E of shell A become 152 GPa. (Note: The actual model shell thickness is 1.375”)
• Run #3: E’s of shells B and C are 145 GPa, the value given by the specification. By modifying the thickness ratio of 1.05/1.375 for the shell A, the E of shell A becomes 111 GPa
• Run #4: E of shell is 145 GPa except in the shell A thin wall regions, where E=111 GPa
• Run #5: All shells having E=145 GPa, the value given by the specification.
• Run #6: E of shell is 145 GPa except in the shell A thin wall regions, where E=124 GPa based on thickness ratio of 1.18/1.375.
• Run #7: E of shell is 145 GPa except in the shell A thin wall regions, where E=137 GPa based on thickness ratio of 1.30/1.375
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Stresses in Shell Type A for Run No. 1- E=193 GPa
Stress Plot up to 120MPa
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Stresses in Shell Type A for Run No. 2 - E(A)=152 GPa, E(B&C)=193 GPa
Stress Plot up to 110MPa
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Stresses in Shell Type A for Run No. 3 - E(A)=111 GPa, E(B&C)=145 GPa
Stress Plot up to 110MPa
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Modulus of Elasticity in Shell Type A for Run No. 4, No. 6 and No.7
Right ViewLeft View
In the pink regions, E = 145 GPa
In the brown regions, E=111 GPa
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Stresses in Shell Type A for Run No. 4 - E=145 GPa except E(thin wall region)=111 GPa
Stress Plot up to 120MPa
![Page 7: FEA Studies for the Shell A Thin Wall Region:](https://reader034.vdocuments.us/reader034/viewer/2022052415/5681302f550346895d95c68e/html5/thumbnails/7.jpg)
Stresses in Shell Type A for Run No. 5- E=145 GPa
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Stresses in Shell Type A for Run No. 6 - E=145 GPa except E(thin wall region)=124 GPa
![Page 9: FEA Studies for the Shell A Thin Wall Region:](https://reader034.vdocuments.us/reader034/viewer/2022052415/5681302f550346895d95c68e/html5/thumbnails/9.jpg)
Stresses in Shell Type A for Run No. 7 - E=145 GPa except E(thin wall region)=137 GPa
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Top View
Axial Stresses in Modular Coils for Run No. 1 - E=193 GPa
Coil Type A
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Top View
Axial Stresses in Modular Coils for Run No. 2 - E=(B&C)193 GPa, E(A)=152 GPa
Coil Type A
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Top View
Axial Stresses in Modular Coils for Run No. 3 - E=(B&C)145 GPa, E(A)=111 GPa
Coil Type A
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Axial Stresses in Modular Coils for Run No. 4 - E=145 GPa except E(thin wall region)=111 GPa
Top View
Coil Type A
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Axial Stresses in Modular Coils for Run No. 5 - E=145 GPa
Coil Type A
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Axial Stresses in Modular Coils for Run No. 6 - E=145 GPa except E(thin wall region)=124 GPa
Coil Type A
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Axial Stresses in Modular Coils for Run No. 7 - E=145 GPa except E(thin wall region)=137 GPa
Coil Type A
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Summary:
Shell Type A Coil Type A All Coils
Max. Disp. Max. Seqv. Max. Disp. Max. Sz. Max. Disp. Max. Sz
(mm) (MPa) (mm) (MPa) (mm) (MPa)
Run #1 0.980 168 1.246 239 2.711 239
Run #2 1.184 159 1.451 244 2.816 244
Run #3 1.434 152 1.837 256 3.019 256
Run #4 1.168 161 1.517 248 2.971 248
Run #5 1.170 160 1.513 248 2.934 248
Run #6 1.169 161 1.516 249 2.984 249
Run #7 1.170 161 1.515 248 2.997 248