ESDU 76007-1976 轴向载荷下钢制纵向角焊附件与接头的疲劳强度

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1
76007
FATIGUE STRENGTH OF LONGITUDINAL FILLET WELDED ATTACHMENTS AND
JOINTS IN STEELS UNDER AXIAL LOADING
1. NOTATION
Both SI and British units are quoted.
2. NOTES
This Item presents data on the fatigue strength of longitudinal fillet welded attachments and joints between
steel members of the types shown in Sketch 2.1 to 2.4 tested in the as-welded condition. The data are
obtained from specimens welded in the laboratory. The range of sizes of the test specimens is quoted on
the relevant figure.
Provided that the welds are sound and free from major defects, the fatigue strength of longitudinal fillet
welds in the untreated and unmachined condition is independent of the properties of the plate and weld
materials (except in the low cycle fatigue region, that is, when is greater than about 85 per cent of the
material tensile strength, at which the endurance is about cycles). The fatigue strength is also
independent of the applied mean stress. This is because as-welded longitudinal joints contain a system of
highly localised residual stresses in the direction of loading which result from the internal constraints applied
during cooling of the weld, and which are of the order of the material yield strength. Hence, any applied
loading will cause local yielding in the region of the end of the weld run during the first few load cycles.
The actual stress experienced in the critical region will thereafter cycle between the yield strength and the
yield strength less the applied stress range, irrespective of applied mean stress, except in cases of high
compressive mean stress.
throat depth (see Sketch 2.5)min
distance of weld end from end of loaded plates m in
modulus of elasticity of plate material N/m2lbf/in2
length of weld run of loaded plate m in
endurance
load applied to joint N lbf
nominal alternating stress (half range) in loaded plate N/m2lbf/in2
weld leg length (see Sketch 2.5)min
thickness of loaded plate m in
width of loaded plate m in
a
d
E
l
N
P
Sa
s
t
w
2Sa
410
3
×
Issued April 1976
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76007
Sketch 2.1 Non-load-carrying joint
(stiffener type) Sketch 2.2 Non-load-carrying joint
(flange type)
Sketch 2.3 Load-carrying joint
(double strap type)
Sketch 2.4 Load-carrying joint
(egg-box type)
Sketch 2.5 Illustrating the assumed throat
depth of a fillet weld and showing
a type C failure
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76007
Provided the weld run is continuous and without severe ripples or defects, all fatigue failures start at one
or both ends of the weld run. Two modes of failure can be distinguished. The fatigue crack may be initiated
at a small defect in the transition region between the plate and the weld bead, and subsequently propagate
transversely through the plate. Alternatively, a crack in the weld throat may begin at the end of the weld in
the weld bead and propagate to cause failure along the weld bead or turn to run transversely through the
loaded plates. The mode of failure is influenced by the throat area of the weld bead relative to the plate
sizes and by the length of the weld run.
Data for non-load-carrying stiffener type attachments are given in Figure 1. These data are for a wide range
of steels and a wide range of applied stress conditions. Figure 2 shows data for non-load-carrying joints of
the flange type and compares these with the data of Figure 1. Figure 3 shows data for asymmetric joints of
the non-load-carrying stiffener type, for example stiffeners welded on one side of the plate only. Data for
load-carrying joints of these types are given in Figures 4 and 5.
3. NON-LOAD-CARRYING JOINTS
3.1 Stiffener-type Attachments
The data for this type of joint, shown in Sketch 2.1, are given in Figure 1. The data show no positive knee
and can be represented by a straight line when plotted on a log/log basis. The mean line of Figure 1 can be
expressed by the equation * over a wide range of tensile mean stress. All
failures begin in the plate at the ends of the weld run, see Sketch 2.1, and fatigue cracks propagate through
and across the loaded plate perpendicular to the stressing direction. Joints with attachments that have been
welded all round, that is, with transverse end welds, have fatigue strengths that are well within the scatter
of the data but are lower on average than those with only longitudinal welds. The reduced fatigue strength
may be due to an increased stress concentration at the ends of the weld runs.
The distribution of the data about the mean is sensibly Gaussian and statistical analysis has led to the
confidence limits shown on the figure. The inner limits give bounds within which there is 95 per cent
confidence that 95 per cent of the population will occur and the outer limits give bounds within which there
is 99 per cent confidence that 99 per cent of the population will occur.
3.2 Flange-type Attachments
This type of joint is shown in Sketch 2.2. The data, given on Figure 2, indicate that the fatigue strength falls
slightly below that of stiffener-type specimens although remaining within the 99 per cent confidence limits
of Figure 1. The lower fatigue strength is thought to be due to the proximity of the weld ends to the edges
of the loaded plate. The location of failure is through the loaded plate from the weld ends as indicated in
Sketch 2.2.
The dashed line in Figure 2 is the mean line for the data.
3.3 Non-load-carrying Asymmetric Joints
The fatigue strength of asymmetric joints is not necessarily lower than that of symmetric joints and may
even be higher as shown in Figure 3, where the dashed line is a mean line through data relating to
stiffener-type joints with attachments on one side of the plate only. This strengthening effect may not exist
for long stiffeners as it may be due to compression at the ends of the stiffener caused by secondary bending.
*The value of E is taken as 207 000 MN/m2 .
N3.65 10 4
×E/2Sa
()
2.9
=
30 106 lbf/in2
×()
北极星标准文库-高清标准规范分享平台 www.bjxwk.com

标签: #接头 #钢 #载荷

摘要:

本文档详细介绍了ESDU 76007-1976标准,该标准专门针对轴向载荷作用下钢制纵向角焊附件与接头的疲劳强度进行评估与设计。内容涵盖焊接接头的疲劳破坏机理、影响疲劳寿命的关键因素(如焊接几何形状、应力集中、载荷频率与幅值等),以及基于大量实验数据与工程实践总结出的疲劳强度预测方法。该标准适用于钢结构设计、船舶、桥梁、压力容器及重型机械等领域中纵向角焊缝的疲劳分析,为工程师提供了可靠的参考依据,以提升焊接结构在循环载荷下的安全性与耐久性。通过遵循该标准,设计人员能够更准确地评估焊缝疲劳寿命,避

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作者:小气猫 分类:国外协会 价格:18星币 属性:12 页 大小:868.89KB 格式:PDF 时间:2026-01-31

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