Loads Part II — Other Loads

Comprehensive coverage of gravity, accidental, seismic, and fatigue loads, plus load combination strategies aligned with API RP 2A and ISO 19902.

1. Gravity Loads (Permanent and Variable)

Dead Load (Permanent Gravity)

Dead load comprises the self-weight of the structure and permanent installations:

Load Case Dead Live Environ. Accidental Seismic In-place storm Pre-service Seismic ELE Fatigue
Figure 1 — Load Combination Matrix (Design Cases)

Dead load is modeled as gravity acting downward at the center of mass of each component. Accurate weight estimates require detailed design and 3D CAD models. Industry practice uses CAD-extracted weights during detailed design phases; preliminary estimates use parametric equations based on deck area and drilling capability.

Live Loads (Variable Gravity)

Live loads represent temporary, operational loads:

Live loads are case-dependent and must be explicitly defined for design scenarios. API RP 2A requires designers to specify maximum mud weight, hydrocarbon inventory, and operational constraints. Load reduction factors for non-coincident live loads are codified in design standards but are typically not applied to critical loads (e.g., full mud weight simultaneous with full lifting operation is rarely credible but is sometimes assumed for conservative design).

2. Buoyancy and Hydrostatic Pressure

Archimedes' Principle

For submerged or partially submerged structures, buoyancy acts upward at the center of buoyancy (centroid of displaced volume):

Buoyancy Force
F_b = ρ_water · g · V_submerged

where:
ρ_water = seawater density (1025 kg/m³)
g = gravitational acceleration (9.81 m/s²)
V_submerged = volume of structure below waterline (m³)

For fixed platforms (jackets, GBS), buoyancy is typically small relative to weight. For floating units (FPSO, Spar, Semi-sub), buoyancy exactly equals weight at equilibrium draft; any overweight causes sinking, and under-buoyancy causes sinking or heel.

Hydrostatic Pressure Distribution

Hydrostatic pressure increases linearly with depth: p(z) = ρ·g·z (gauge pressure, z measured downward from free surface). For closed members (caissons, columns), internal atmospheric pressure may be maintained, creating a net inward pressure. Modern codes require explicit hydrostatic load checks for:

3. Accidental Loads

Dropped Object Impact

A heavy object falling from the deck (pipe, equipment, crane block) impacts a structural member with kinetic energy E_k = 0.5·m·v². The impact is typically modeled as an inelastic collision, converting kinetic energy to local deformation and permanent damage:

Modern platforms employ rigorous "dropped object" prevention programs: all equipment lifted must be tagged, certified, and tracked. Deck layouts minimize objects over critical load paths. Many regulatory authorities now require quantitative risk assessment for dropped objects, estimating frequency and consequence.

Vessel Collision

Floating vessels (supply ships, emergency response vessels) may collide with a platform in fog, storms, or navigation errors. Typical collision scenarios include:

Collision energy is estimated from vessel mass (3,000–20,000 tonnes for supply vessels) and speed (2–5 m/s in operational scenarios, higher in loss-of-control scenarios). Modern designs include:

Explosion and Fire

Explosive atmosphere (gas cloud) and ignition sources can lead to overpressure and thermal loads. API RP 2A Section 5.11 and ISO 19902 Appendix G address explosion-resistant design. Key points:

4. Seismic Loads

Seismic Zones and ISO 19901-2

Offshore platforms in seismic regions (California, Southeast Asia, Mediterranean, etc.) must be designed for earthquake-induced ground motion. ISO 19901-2 classifies regions into seismic zones based on historical activity and probabilistic seismic hazard assessment (PSHA):

Deep-water floating platforms experience reduced seismic loading due to low natural frequencies (long periods > 20 seconds); shallow-water jackets with stiff structures (periods 3–8 seconds) are more excited by typical earthquake spectra (5–20 second period bands).

Equivalent Linear Elastic (ELE) and Acceleration-Led (ALE) Methods

Two primary design approaches:

Modern practice typically uses ELE for routine designs and ALE for risk-critical projects. Both methods require site-specific geotechnical investigation and cone penetrometer (CPT) data to characterize soil profiles.

5. Fatigue Loads and Wave Scatter Diagrams

Cumulative Fatigue Damage

Unlike a single extreme load that must not exceed design capacity, fatigue damage accumulates from cyclic stress over many cycles. Miner's rule estimates total damage:

Miner's Rule (Linear Damage Accumulation)
D = Σ (n_i / N_i)

where:
n_i = actual number of cycles at stress level i
N_i = allowable number of cycles at stress level i (from S-N curve)
Failure occurs when D ≥ 1.0 (typically design for D ≤ 0.3–0.5)

The S-N curve (stress amplitude vs. number of cycles to failure) is empirically derived from fatigue testing of welded steel joints. API RP 2A Table 9-1 provides curves for various weld details and material grades.

Wave Scatter Diagram

A scatter diagram tabulates the frequency of occurrence of sea states (wave height and period pairs) at a given site over a long period (typically 20+ years). Example for Gulf of Mexico:

Hs (m) T ≤ 8s (%) 8s < T ≤ 12s (%) T > 12s (%) Total (%)
0–1 15.2 8.5 1.2 24.9
1–2 12.8 18.3 4.5 35.6
2–3 8.2 15.4 5.2 28.8
3–4 3.1 4.8 2.4 10.3
> 4 0.2 0.1 0.1 0.4

Fatigue analysis uses the scatter diagram to weight the contribution of each sea state to total damage. Sea states with Hs < 2 m, occurring 60% of the time, often contribute 40–60% of total fatigue damage due to frequency. The 100-year extreme (Hs ~ 14–16 m in GoM) contributes negligibly to fatigue.

6. Load Combinations and Safety Philosophy

Design Limit States

Modern codes differentiate between three limit states:

Load Factors and In-Place Load Cases

API RP 2A prescribes load factors for different load types and design scenarios. Example in-place load combination (ULS):

API RP 2A In-Place Load Combination
Demand = 1.0·DL + 1.2·LL + 1.5·WaveLd + 0.75·WindLd + 0.75·CurrentLd

where:
DL = dead load (gravity)
LL = live load (operational)
WaveLd = design wave load (typically 100-year Hs)
WindLd = concurrent wind (typically 20–50 year return period)
CurrentLd = concurrent current (typically 5–10 year return period)

The 1.5 factor on wave load reflects the largest uncertainty in load estimation; wind and current receive lower factors due to lower probability of simultaneous occurrence with design wave. Designers must check all critical members for this combination and select the governing case.

LRFD vs. ASD Philosophy

Load and Resistance Factor Design (LRFD) applies factors on loads and resistances:

LRFD Criterion
γ_L · Q_nominal ≤ φ · R_nominal

where:
γ_L = load factor (> 1, amplifies demand)
φ = resistance factor (< 1, reduces capacity)
Typical: γ_L ≈ 1.5, φ ≈ 0.85

Allowable Stress Design (ASD) applies a single safety factor to permissible stress:

ASD Criterion
f_nominal ≤ F_allowable / SF

where:
f_nominal = calculated stress from nominal (unfactored) loads
F_allowable = yield or buckling stress
SF = safety factor (typically 1.5–2.0)

API RP 2A-WSD uses ASD for in-place analysis; ISO 19902 increasingly emphasizes LRFD. Both approaches, if properly calibrated, yield equivalent safety; choice is often driven by regulatory authority.

7. Dynamic Amplification Factor (DAF)

Wave and wind loads applied quasi-statically overestimate peak stresses compared to true dynamic response. The Dynamic Amplification Factor (DAF) accounts for the structure's inertia and resonance:

Dynamic Amplification Factor
DAF = 1 + (damping_reduction_factor) · (frequency_response_function)

Simplified: DAF ≈ 1.5 to 2.5 for first-mode resonance,
depending on structural damping (typically 2–5% critical damping for offshore platforms)

API RP 2A Table 10-2 provides DAF values; ISO 19902 requires explicit dynamic analysis if the fundamental period exceeds 3 seconds. Very flexible structures (deepwater spars with periods > 20 s) experience minimal DAF because the wave loading frequency (0.05–0.15 Hz) is far below the structural frequency.

Summary: Load Combination and Design Philosophy

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