Project context
A thin-walled cylindrical asset required lifting from a horizontal position, skewed slightly during rotation, and set down onto temporary supports prior to final installation.
The asset was designed strictly for pressure and operational loads, with no allowance for:
Ovalisation under self-weight
Local bending during skewed lift
Temporary support eccentricities during set-down
Why FEA was essential
Hand calculations could not credibly assess:
Shell ovalisation limits under transient load cases
Buckling interaction with local bending
Strain accumulation during staged operations
Equitus FEA scope
Shell-based nonlinear FEA including:
Geometric nonlinearity
Local imperfections consistent with fabrication tolerances
Simulation of:
Horizontal lift
Skewed rotation
Temporary set-down on discrete supports
Assessment against strain-based acceptance criteria
Outcome
Defined a safe operational envelope for lift and rotation
Demonstrated acceptable ovalisation without permanent deformation
Avoided unnecessary stiffening rings that would have increased mass and cost
Provided Mammoet with quantified confidence, not assumptions
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