- •Главная
- •1.1 Напряжений и концентраторы
- •1.1.3 Концентраторы напряжения
- •1.3 Stress concentration factor
- •1.7 Elastic-plastic stress concentration
- •1.8 Joints: bolts and welds
- •3. Механические свойства конструкционных материалов
- •3.1 Напряженности испытания
- •3.2 Stress - strain diagram
- •3.3 Testing schemes
- •3.4 Strength
- •4 Прочность материалов
- •4.1 Tension and compression
- •4.2 Shear and torsion
- •4.3 Stress-strain state
- •4.4 Bending: force and moment diagrams
- •4.5 Geometrical characteristics of sections
- •4.6 Bending: stress and deformation
- •4.7 Mixed mode loading
- •4.8 Buckling
- •4.9 Statically indeterminate systems
- •4.10 Three-dimensional structures
- •References
- •5. Theory of elasticity
- •5.1 Deformation
- •5.2 Stress
- •5.3 Hooke's law
- •5.4 Plane problems
- •5.5 Torsion
- •5.6 Bending
- •5.7 Polar coordinates
- •5.8 Plates
- •5.9 Shells
- •5.10 Contact stresses
- •6.2 Distribution functions
- •6.3 Structural models of reliability
- •6.4 Limiting state
- •6.5 Dispersion
- •6.6 Durabilty
- •6.7 Design by reliability criterion
- •6.8 Risk
- •6.9 Safety classes
- •6.10 Risk : structural and social
- •References
- •7 Materials science
- •7.1 Crystalline solids
- •7.2 Mechanical properties
- •7.3 Failure
- •7.4 Phase diagrams
- •7.5 Heat treatment of metals and alloys
- •7.6 Corrosion of metals and alloys
- •7.7 Casting
- •7.8 Polymers
- •7.9 Composites
- •7.10 Forming of metals
- •8.2 Mechanical properties
- •8.3 Stress concentration
- •8.4 Defects
- •8.5 Residual Stress
- •8.6 Strength
- •8.7 Fatigue strength
- •8.8 Fracture
- •8.9 Weldability
- •References
- •9 Composites
- •9.1 Structure of composites
- •9.2 Fibers
- •9.3 Rigidity
- •9.4 Strength
- •9.5 Crack resistance
- •9.6 Optimization
- •9.7 Fatigue and temperature effect
- •9.8 Reliability
- •9.9 Joints
- •9.10 Material selection
- •References
- •10 Finite element analysis
- •10.1 Finite element method
- •10.2 Finite elements
- •10.3 Meshing
- •10.4 Boundary conditions
- •10.5 Deformation
- •10.6 Accuracy
- •10.7 Heat transfer analysis
- •10.8 Dynamics
- •10.9 Computational fluid dynamics
- •10.10 Design analysis
- •References
8.5 Residual Stress
Unhomogenous
heating causes local thermal expansion of metals. This is reflected
in residual stress after cooling. Residual stress is a tensile stress
in the center of a weld. Tensile stress in a weld is compensated by
compressive stress in base metal.
Weld
metal is squeezed as it cools. During welding, edges move relative to
each other, mostly perpendicular to the welding direction. Residual
stress results in shrinkage of the structure.
The
choice of welding sequence affects the distortion of the welded
structure. If a welder uses opposite directions, the distortion is
smaller.
If
a weld is below the neutral axis the shape is concave up. If a weld
is over the neutral axis the shape is concave down.
The
angle b is small for small weld depths. The angle is not too large if
the weld depth is equal to the thickness of the plate.
A
similar effect can be observed in a tee-joint. For thin plates the
displacement caused by residual stress is rather large, it decreases
as thickness increases.
Residual
stress is at a maximum for a rigid structure with a large number of
welds and with closed loops. The structures are shown in order of
increasing rigidity.
The
residual stress decreases as annealing temperature increases. There
are annealing procedures that can reduce residual stress to zero.
8.6 Strength
Strength
of a welded joint depends on weld geometry and strength of materials.
The minimum cross section of a weld is considered in strength
calculations. Throat a is at a minimum. Throat is the distance from
the root to the surface of a fillet weld. The throat of a fillet is a
measure of the weld size. Critical force P for a lap joint using a 45
degree filet weld depends on allowable shear stress for the weld
material tallowable.
Bending
stress is small if moment of inertia of the weld cross-section is
large. The moment depends on the cross sectional area and it's
distance from the neutral axis shown in the figure. The second
example is three times stronger than the first.
The
tensile strength of a butt-joint is higher for the case with low
stress concentration. Build-up welds are often produced to increase
wear resistance, not tensile strength.
Spot
resistance welding. The nugget is stronger under shear than in
tension. Strength of nugget increases with thickness.
Contrary
to uniform low-carbon steel plate, it's weld joint can have a brittle
fracture mechanism: smaller critical stress at low temperature.
Usually the temperature of brittle-ductile transition is below zero,
ranging from -100oC
to -40oC.
Annealing increases the ductility of materials and prevents brittle
fracture.
Crack
resistance characteristic - the critical value of stress intensity
factor depends on test temperature. Usually the brittle fracture for
base metal, weld and heat-affected zone are similar, lower limits are
equivalent. The characteristic of ductile fracture (upper limit) is
usually smaller in the welded zone.
Presence
of oxygen in weld material affects the embrittlement of the material.
High oxygen content corresponds to embrittlement (relatively high
transition temperature).
