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The elevated container with its front cabin and access stair

Structural FEA of an Elevated Container

NEOM container, supports and access platforms

FINITE ELEMENT ANALYSIS

Structural FEA of an Elevated Container

01 / THE STRUCTURE

An elevated enclosure with a separate front cabin

The model combines a long electrical enclosure with a smaller projecting cabin. The container floor carries the installed equipment, while columns and diagonal bracing transfer loads to the ground connections. The cabin has its own support arrangement, making it important to assess both parts of the assembly

Render of the elevated container on its support frame

The assessed system

Container base frame Wall panels and roof Front cabin and floor Columns and bracing Welds and bolt connections Lifting attachment regions

Original project geometry, with the elevated support frame visible beneath the enclosure

02 / ANALYSIS DEVELOPMENT

Preparing the assembly for structural analysis

The supplied 3D model was developed into an FE assembly in HyperMesh and solved in ANSYS Mechanical APDL. Thin sections were represented using midsurfaces and shell elements. Thick parts used solid elements, and the model connected the structural parts at their intended interfaces

  • FE assembly with the walls, roof, base and supports in separate colours

    Component representation

    The assembly view separates the walls, roof, base and supporting structure so their contribution can be traced through the analysis

  • Transparent view of the internal members and payload connections

    Internal connectivity

    The transparent view reveals internal members and payload connections that are hidden by the exterior panels

03 / MESH & CONNECTIONS

Resolving the floor, panels and load-carrying joints

  • Mesh of the base frame and floor members

    Base-frame mesh

    The floor and equipment-supporting members form a primary load path. Their mesh represents the spans and intersections beneath the enclosure

  • Mesh at the welded member intersections

    Welded interfaces

    Connectivity at welded locations transfers load between intersecting members. The report models these joints as continuous connections

  • Mesh at the column-head connection

    Column-head connection

    The mesh follows the support-to-base interface, where loads enter the elevated steelwork

  • Mesh at the wall-panel corner connections

    Wall-panel connections

    Panel edges, framing and corner interfaces are represented to examine the enclosure response

  • Shell mesh of the roof and its supporting members

    Roof and supporting members

    Shell modelling captures the thin roof sections and the members that support them

Bolts were represented by one-dimensional beam elements. Equipment masses were represented by point masses coupled to their mounting locations. The assessment assumes homogeneous material and ideal joints, and excludes ageing and corrosion effects

04 / PAYLOAD & BOUNDARY CONDITIONS

Applying mass and support conditions to the model

  • Model with the six main-container and four cabin supports

    Installed support arrangement

    The service cases use six main-container supports and four cabin supports. The illustrated restraints establish how reactions develop at the base

  • Equipment point masses coupled to their mountings

    Equipment mass at its mountings

    The model includes two 2,200 kg control panels, air-conditioning units and distribution boards, in addition to the structural mass

Recorded dead-load mass
13,813 kg
Specified wind speed
46 m/s
Model material yield strength
350 MPa

05 / LOADING PROGRAMME

Seven structural loading conditions

Structural loading conditions
CONDITIONAPPLIED LOADINGSUPPORT BASIS
Dead loadStructural self-weight and equipment payloads6 + 4 base supports
Dead + live load5 kN/m² on walkway and 1 kN/m² on roof6 + 4 base supports
Wind, two directionsDead load and wind corresponding to 46 m/s6 + 4 base supports
Seismic, two directionsDead load and equivalent seismic action at 0.1125 g6 + 4 base supports
LiftingSelf-weight and the specified 2.54 kPa walkway loadFour lifting-lug restraints
  • Live load applied to the walkway and roof

    Walkway and roof loading

    The live-load model applies distributed loads to the occupied floor and roof regions

  • Wind pressure on the enclosure in the first orientation

    Wind in one direction

    Pressure acts on the exposed surfaces of the enclosure in the illustrated orientation

  • Wind pressure on the enclosure in the second orientation

    Wind in the other direction

    The second orientation changes the loaded face and the response of the walls and supports

06 / DEAD & LIVE LOAD RESULTS

Checking the equipment-supporting base frame

  • Base-frame deformation contour under dead load

    1.52 mm under dead load

    The original contour reports 1.518 mm maximum base-frame deformation. The assessment uses an 8.88 mm beam-deflection limit

  • Base-frame stress contour with live load

    145.63 MPa with live load

    Adding the specified walkway and roof loading raises the reported base-frame stress from 80.90 MPa to 145.63 MPa

The combined dead- and live-load case produces 3.06 mm base-frame deformation. Reviewing displacement alongside stress shows both the movement of the supporting members and the regions carrying the higher demand Result interpretation: the report excludes singularities and local peaks when stating some assessment stresses. Original contour legends are retained so the displayed solver values remain visible

07 / WIND RESPONSE

Comparing movement in the two wind cases

  • Deformation contour for wind case WL1

    15.45 mm in wind case WL1

    The deformation pattern shows the wall and frame response for the first wind case. The report compares this movement with a 25.5 mm horizontal limit

  • Deformation contour for wind case WL2

    12.47 mm in wind case WL2

    Changing the wind direction changes the displacement pattern. This case is assessed against the same reported horizontal limit

The analysis follows the load beyond the external wall: through the base frame, columns and bracing. Separate support results identify the demand on the main-container and cabin steelwork.

08 / LIFTING ASSESSMENT

A separate support condition for handling

The model combines a long electrical enclosure with a smaller projecting cabin. The container floor carries the installed equipment, while columns and diagonal bracing transfer loads to the ground connections. The cabin has its own support arrangement, making it important to assess both parts of the assembly

Model restrained at the four lifting lugs

Four lifting restraints

The lifting case replaces the installed support condition with restraints at the lifting lugs. This changes how the load is carried through the enclosure and its base frame The model evaluates the defined analysis condition and its associated payload

  • Deformation contour for the lifting case

    2.93 mm reported deformation

    The lifting contour shows the response of the container under the defined lifting condition. The report compares it with an 8.88 mm limit

  • Stress contour at the lifting lug

    Local response at the lifting lug

    The lug plot shows a 544.6 MPa local solver maximum. The report states 150 MPa after excluding peaks, so the local maximum must be distinguished from its assessment value

The base-frame stress for lifting is 206.28 MPa. Local attachment behaviour remains an important part of the review because the handling load enters the structure through a small number of connection regions

09 / SEISMIC ASSESSMENT

Examining the enclosure in two horizontal directions

Equivalent seismic actions were applied longitudinally and transversely using the reported 0.1125 g acceleration component. Component plots allow the wall response to be examined separately from the base frame, roof and supporting columns

  • Wall stress contour for the longitudinal seismic case

    189.63 MPa, longitudinal case

    The wall contour identifies the stress distribution for longitudinal seismic loading. This is the maximum shown by the original component plot

  • Wall stress contour for the transverse seismic case

    206.85 MPa, transverse case

    The transverse case produces a higher maximum in the displayed wall result. This comparison helps identify which loading direction governs this component

10 / SUPPORTS & FOUNDATION INTERFACE

Assessing the columns and bracing

Stress contour of the columns and bracing in wind case WL1

209.57 MPa

Main support stress in WL1 The report identifies this wind case as the highest main-support stress in its summary. The stated yield-to-stress ratio is 1.67 for the model material

Reaction schedules record forces and moments at the six main columns and four cabin columns, with axis definitions for the foundation interface.

These schedules provide inputs for foundation coordination. They do not establish soil capacity or concrete-foundation adequacy

11 / ACCESS PLATFORM ASSESSMENT

Extending the study to the access structures

  • Model of the larger access platform

    Larger access platform

    The separate platform study represents the deck, supporting legs and guardrails. Its loading basis includes self-weight and 5 kN/m² on the platform.

  • Model of the smaller access platform

    Smaller access platform

    A second platform geometry is assessed in the same report, with its own span, supports and component response

  • Deformation contour of the larger platform and guardrail

    Platform deck and guardrail movement

    The report states 6.13 mm on the platform against a 7.22 mm limit. The whole-model contour reaches 17.26 mm at the guardrail, a different location

  • Stress contour of the smaller platform

    81.76 MPa in the smaller platform

    The smaller platform plot shows 81.76 MPa stress. Its separate deformation result is 1.76 mm against a reported 2.72 mm limit

For the larger platform, the report states an assessment stress of 200 MPa after peak exclusions. The original stress contour has a local maximum of 319.89 MPa

12 / SELECTED RESULTS

Component checks used in the assessment

Selected component results
ASSESSMENTREPORTED RESPONSEREFERENCE USED IN REPORT
Base frame, dead load1.52 mm deformation / 80.90 MPa stress8.88 mm deflection limit
Base frame, dead + live3.06 mm deformation / 145.63 MPa stress8.88 mm deflection limit
Wind cases WL1 / WL215.45 mm / 12.47 mm movement25.5 mm horizontal limit
Lifting2.93 mm deformation / 206.28 MPa base stress8.88 mm deflection limit
Main supports, WL1209.57 MPa stress / reported ratio 1.67350 MPa material yield strength

Values are rounded from the detailed plots where available. The source summary records satisfaction of its stated checks, subject to the model assumptions and treatment of local peaks

Outcome

A detailed basis for vessel design review

The ASME Section VIII, Division 2 assessment connected full-vessel response with the behaviour of individual pressure-boundary components. SCL evaluations resolved membrane and bending stresses at critical regions and supported the documented design development The delivered analysis package gave the engineering team a traceable basis for reviewing the propane and butane vessels across the defined operating, test and handling scenarios

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