Crane Welded Joint Types & Fatigue Strength Calculation

GB/T 13331-2013 "Cranes — Welded Structures" is the general standard governing the structural design of welded crane frameworks. It specifies the selection of welded joint types, weld calculation methods, and construction requirements for crane steel structures, and is applicable to the welding design of primary load-bearing structures in overhead, gantry, tower, mobile, and boom cranes.

GB/T 13331-2013 is a dedicated standard for welded joint types in crane structures, defining the classification, configuration, and fatigue strength calculation of welded joints.

GB/T 13331-2013 Crane Welded Structure Standard


Standard Positioning and Structural Design Requirements

GB/T 13331-2013 (originally issued as JB/T 13331-2013 before conversion to a national standard) is the core standard for the structural design of welded crane frameworks. The standard establishes the following fundamental principles for the welding design of crane steel structures: welds should be located in areas of lower stress and kept clear of stress concentration zones. Weld dimensions must be determined by calculation rather than by experience alone; arbitrarily increasing fillet weld leg height is not permitted, as oversized welds lead to greater welding distortion and residual stress. When joining steel plates of different thicknesses, the thicker plate should be tapered on the welding side (transition slope ≤ 1:2.5). The fatigue strength of welds must be verified in accordance with GB/T 3811 Crane Design Standard. The structural design should also account for welding accessibility, ensuring that welding torches and operators can reach the weld positions for proper execution.

Welded Joint Types and Selection

The standard specifies the following joint types for crane welded structures: Butt joints — used for splicing the main girder flange plates and web plates. An I-shaped groove is used for plate thickness ≤ 8 mm, a V-shaped groove (60° groove angle) for thicknesses between 8 mm and 20 mm, and an X-shaped groove (double-sided welding to reduce angular distortion) for thicknesses exceeding 20 mm. T-joints — used for connecting web plates to flange plates (the main welds of the main girder). Partial penetration T-joints are suitable for light duty classification, while full penetration T-joints are required for critical welds rated A5 or above. Corner joints — used for connecting stiffening plates to web plates. Lap joints — to be avoided wherever possible for primary load-bearing members and used only for non-load-carrying components. The strength of butt welds must not be lower than the design value of the base metal strength. The fillet weld leg height must be no less than 4 mm and no greater than 1.2 times the thickness of the thinner plate.

Butt Joint
I/V/X groove selected by plate thickness
T-Joint
Partial/full penetration; full penetration required for A5 and above
Fatigue Verification
Welded joint fatigue per GB/T 3811
Fillet Weld Leg Height
≥4 mm ≤1.2× thinner plate thickness
Stress Concentration
Keep welds clear of high-stress zones
Thick Plate Transition
Taper slope ≤ 1:2.5

Weld Calculation Methods

The standard provides calculation methods for various weld types: Butt welds — for butt welds subjected to axial tension or compression, the strength is calculated as σ = F/A ≤ ft or fc, where F is the applied force, A is the weld cross-sectional area (taken as base metal thickness × weld length, excluding reinforcement), and ft and fc are the design values of tensile and compressive strength of the weld, respectively. Fillet welds in T-joints — fillet welds subjected to shear force are calculated as τ = F/(he × lw) ≤ fv, where he is the effective throat thickness of the fillet weld (= 0.7hf, with hf being the leg height), lw is the effective weld length (actual length minus 2 × hf), and fv is the design shear strength of the fillet weld. The standard also specifies strength check formulas for welds under combined stress (bending + shear + axial force) and fatigue strength verification methods, where the allowable fatigue stress range is determined based on the number of stress cycles.


Welded Joint Type Comparison Table

The comparison table below outlines the core parameter configurations for welded joint types, serving as a reference for design selection and field application.

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← Scroll left / right to view full table →
Joint TypeApplication Areagroovetype testfatigue class
Butt jointFlange plate SpliceX Type/V TypeF1-F2
TProfile Jointflangeand Web plateK Type/Half V TypeF2-F3
Corner jointstiffening plate ConnectionSingle-Sided V TypeF3-F4
Lap jointSecondary StructureNonegrooveF4

FAQ

Q: What is the difference between fatigue verification and static strength check for crane welded structures?
A: A static strength check verifies only whether the weld seam can withstand a single maximum load (using the safety factor method), whereas fatigue verification assesses whether the weld seam will fail under repeated cyclic loading at stress levels well below the static strength limit. Fatigue verification of crane structures is critical—because cranes experience alternating loads (each hoisting cycle constitutes one stress cycle), and stress concentrations at weld seams can significantly reduce fatigue life. Field experience shows that over 90% of crane structural failures originate from fatigue cracks. The fatigue verification procedure: determine the number of stress cycles N based on the crane's Work Duty Classification (A1–A8), establish the fatigue class of the welded joint (e.g., FAT80, FAT100) per GB/T 3811 Crane Design Standard, calculate the permissible fatigue stress range Δσ_R, and ensure that the actual stress range Δσ ≤ Δσ_R.
Q: Should the T-joint between the main girder web plate and flange plate be full penetration or partial penetration? How is this determined?
A: The selection depends on the crane's work duty classification. For cranes rated A1–A4 (light and medium-light duty), the T-joint between the web plate and flange plate may use partial penetration fillet welds, with a leg height of at least 0.7 times the web plate thickness. For cranes rated A5 and above (medium, heavy, and extra-heavy duty), full penetration T-joints are required, achieved by beveling the plates (K-groove or J-groove) and welding from both sides to ensure complete fusion. The fatigue strength of a full penetration joint is approximately 2 to 3 times that of a partial penetration joint. For metallurgical cranes used in lifting and transport of molten metal, full penetration T-joints are mandatory regardless of the work duty classification. In partial penetration joints, the unfused region at the weld root creates a natural crack-like discontinuity that can readily propagate into a through-thickness crack under cyclic loading.
Q: Why should cross-shaped weld seams be avoided in welded structures?
A: A "cross-shaped weld seam" refers to two weld seams intersecting perpendicularly in the same plane, or meeting in different planes in space—for example, where the vertical weld of a stiffening plate crosses the longitudinal weld of the main girder web plate at the same cross-section. Cross-shaped weld intersections present three problems: 1) Residual stresses from the three weld passes accumulate at the intersection point, creating an extremely high multi-axial residual stress field; 2) The metallographic structure at the weld intersection deteriorates due to overlapping heat-affected zones from repeated heating; 3) The intersection creates a sharp geometric notch, with stress concentration coefficients reaching 5–8. Because of these three compounding factors, cross-shaped weld seams are the most typical source of fatigue cracks in crane structures. Design should avoid weld intersections by terminating stiffening plate welds at least 50 mm away from the main girder weld.
Q: Why is tapering required on the thicker plate in butt joints of heavy plates?
A: When butt-joining steel plates of different thicknesses—such as in main girder flange plate splicing—the load transfers from the thicker plate to the thinner one. Without a tapered transition, severe stress concentration occurs at the sudden thickness change, with stress concentration factors potentially reaching 3 to 5. The specific requirements for the taper are as follows: the thicker plate is tapered on one side at a slope of ≤1:2.5 until it matches the thickness of the thinner plate (i.e., 1 mm of thickness is removed for every 2.5 mm of length), after which the butt weld is made. Once tapered, the plates on both sides of the weld seam are of equal thickness, allowing smooth stress transfer and keeping the stress concentration factor within 1.2. This requirement is applicable to butt joints with a thickness difference of ≥4 mm.

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