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Common Classification Parameters

There are a few classification parameters that are common across all the types of weld lines that can be detected by HyperLife Weld Certification.
Parameter Label
Weld Type Weld_Type
Weld Category Weld_Category_<Weld Type>
Evaluation Distance Calculation Method EvalDist Calculation Method
Weld_Type
This parameter is automatically detected by HL-WC. The supported weld types are T, L, B, O, X and M welds. More information about weld types is available in The Weld Evaluation.
Weld_Category
Preset configurations for the classification parameters.
EvalDist Calculation Method
HL-WC allows two ways to calculate the evaluation distance using an automatic method and a manual method. The automatic method calculates the evaluation distance as a function of weld width and shell thickness of the components connected by the weld line. When using the manual method you can specify the distance in model units and HL-WC will use the value as is.
Effective Weld Thickness (Ar)
Ar (resulting weld thickness) is user-defined input. Based on this parameter, there is a provision to reduce the stress values that are captured from FE in specific sheets of the connection according to the formula: Stress (corrected) = Stress (current) * Ar / shell thickness. This applies only to the stress normal to the weld and the shear stress. By default the value of Ar is set for the minimum shell thickness and then you can modify the value accordingly.
Tip: Turn on the Enable Effective Weld Thickness option in Preferences to automatically set all weld lines to Yes in the Points Context. The option is disabled by default.


Figure 1.

Direction Details

Longitudinal Direction
Direction parallel to the axis of the weld.
Transverse Direction
Direction perpendicular to the axis of the weld. There are two directions possible here, one towards the base material and other towards the web material.

Static Assessment

Use Static assessment to check for yielding/plasticity at weld locations. The Static evaluation process is carried out for all the evaluation locations based on the weld type. Von Mises stress component is used for this evaluation process. The maximum stress value across all the selected loadcases is compared against the material yield for any particular element.

Static Utilization = Max Von Mises / Material Yield Strength

The above calculation gives the Static utilization factor.
Restriction: Static assessment is currently supported for Shell welds only.

General Stress Correction Based on Effective Weld Thickness

The stress value correction is carried out as shown in the formula below:
σT,corr=σT·1z·tAr·(1+6·eAr)

Where:

  • σT - Stress value before correction (extraction from element at evaluation location)
  • t - Thickness of the shell at the evaluation location
  • Ar - Effective weld thickness
  • z - Intermittent factor, default = 1
  • e - Eccentricity, default = 0


Figure 2.
Influence on Intermittent Factor ( z )
This factor is used to indicate the partiality of welds. This ratio describes the length of the weld that has actually been welded. Whenever the weld connection at any particular location is not continuous/complete, then you are suggested to modify/reduce this parameter to take into account the reduced weld material. (1 ≥ z ≥ 0)
Influence of Effective Weld Thickness ( a )
This parameter is used to consider the influence of welds which do not cover the same cross section area as indicated by the shell element in the respective evaluation location. It modifies the stress at the evaluation location based on the ratio to the shell thickness. ( a > 0)
a=Ti·Tf
  • Ti - Thickness influence represents the resultant maximum weld thickness. It varies based on the weld type. this parameter is location specific.
  • Tf - Indicates which shell thickness you need for the calculation of effective weld thickness ( a ). Valid options are t and tmin , also location specific. t = thickness of welded shell. tmin = min thickness of all connected shells.
Influence of Eccentricity ( e )
This parameter is used to consider the influence of welds which do not have the same cross section center as indicated by the shell element in the respective evaluation location. It modifies the stress at the evaluation location based on the induced bending stress. If e > 0 the stress is increased. If e < 0 the stress is reduced. If e = 0 there is no influence.
Note: The stress correction does not apply to the longitudinal stress components from the weld coordinate system.
General Stress Correction is activated when the Effective Weld Thickness option is set to yes.
  1. This option is activated in the General options section of the Points tool and is available for all regulations.


    Figure 3.
  2. The default effective thickness calculated in the weld line browser under location details is based on the following tables.
    Table 1.
    Weld Locations Ti Tf Effective Thickness
    T-Weld 3, 4 0.7 tmin 0.7 * tmin
    L-Weld 1, 2, 3, 4 0.7 tmin 0.7 * tmin
    Butt-Weld 1, 2, 3, 4 1.0 tmin 1.0 * tmin
    Overlap 3, 4 0.7 tmin 0.7 * tmin
    M-Weld 3, 4, 7, 8 0.7 tmin 0.7 * tmin
    X-Weld 3, 4, 5, 6, 9, 10 0.7 tmin 0.7 * tmin
    Table 2.
    Weld Locations Ti Tf Effective Thickness
    T-Weld 1, 2, 5, 6 1.0 t 1.0 * t
    Overlap 1, 2, 5, 6 1.0 t 1.0 * t
    X-Weld 1, 2, 5, 6 1.0 t 1.0 * t
    M-Weld 1, 2, 5, 6 1.0 t 1.0 * t
  3. The default calculated effective thickness can also be manually edited.