Spot Weld Fatigue Analysis

Allows for the study of fatigue performance of spot welds in structures.

Currently, only stress-life (SN) based spot weld fatigue analysis is supported. The spot weld location is defined by three attributes, sheet 1, sheet 2, and the nugget.

Implementation

Fatigue analysis for spot welds involves examining the weld at three distinct locations, the sheets and nugget, and is based on a paper by Rupp et al. The cross-sectional forces and moments at the nugget location are determined and used to calculate corresponding stresses at the sheets and the nugget. These stresses are then used to calculate Fatigue Damage using Rainflow counting and the SN approach.

The following sections illustrate how stresses and subsequently damage are calculated at each of the three locations.

Sheet Location (1 or 2)

Radial stresses are calculated at the sheet by considering forces and moments at the nugget. The radial stresses

σ (θ)

are calculated as a function of

θ

for each point in the load-time history as:(1)

σ (θ) = - σ_{\max} (f_{y}) \cos θ - σ_{\max} (f_{z}) \sin θ + σ (f_{x}) + σ_{\max} (m_{y}) \sin θ - σ_{\max} (m_{z}) \cos θ

Where,(2)

σ_{\max} (f_{y}) = \frac{f_{y}}{π D T}

(3)

σ_{\max} (f_{z}) = \frac{f_{z}}{π D T}

$σ (f_{x}) = κ (\frac{1.744 f_{x}}{T^{2}})$ for $f_{x} > 0.0$

σ (f_{x}) = 0.0

for

f_{x} \leq 0.0

(4)

σ_{\max} (m_{y}) = κ (\frac{1.872 m_{y}}{D T^{2}})

(5)

σ_{\max} (m_{z}) = κ (\frac{1.872 m_{z}}{D T^{2}})

Where,

$D$: Diameter of the weld element
$T$: Thickness of the sheet under consideration for damage calculation
$κ$: Calculated as $κ = 0.6 \sqrt{T}$

The equivalent radial stresses are calculated at intervals of $θ$ (Default =18 degrees). The value of $θ$ can be modified by varying the Number of angles field in the spot weld solution settings. Subsequently, Rainflow cycle counting is used to calculate fatigue life and damage at each angle ( $θ$ ). The worst damage value is then picked for output. A similar approach is conducted for the other sheet.

Nugget Location

The absolute maximum principal stresses are calculated using the shear stress and bending stress of the beam element as a function of

θ

for each point in the load-time history as:(6)

τ (θ) = τ_{\max} (f_{y}) \sin θ + τ_{\max} (f_{z}) \cos θ

(7)

σ (θ) = σ (f_{x}) + σ_{\max} (m_{y}) \sin θ - σ_{\max} (m_{z}) \cos θ

Where,(8)

τ_{\max} (f_{y}) = \frac{16 f_{y}}{3 π D^{2}}

(9)

τ_{\max} (f_{z}) = \frac{16 f_{z}}{3 π D^{2}}

$σ (f_{x}) = \frac{4 f_{x}}{π D^{2}}$ for $f_{x} > 0.0$

σ (f_{x}) = 0.0

for

f_{x} \leq 0.0

(10)

σ_{\max} (m_{y}) = \frac{32 m_{y}}{π D^{3}}

(11)

σ_{\max} (m_{z}) = \frac{32 m_{z}}{π D^{3}}

$D$ is the diameter of the weld element.

$T$ is the thickness of the sheet under consideration for damage calculation.

The equivalent maximum absolute principal stresses are calculated for each $θ$ from $τ (θ)$ and $σ (θ)$ . These stresses are used for subsequent fatigue analysis. Rainflow cycle counting is used to calculate fatigue life and damage at each angle ( $θ$ ). The worst damage value is then picked for output.