Post on 09-Sep-2018
Design of Machine Members-I
Contents: Unsymmetrical welded joints
Axially Loaded Unsymmetrical WeldedSections
Sometimes unsymmetrical sections such as angles,
flange edges are loaded axially as shown in Fig.
proportioned in such a way that the sum of resisting
axis is zero. Consider an angle section as shown in Fig.
Let la = Length of weld at the top,
lb = Length of weld at the bottom,
l = Total length of weld = la + lb
P = Axial load,
a = Distance of top weld from gravity axis,
b = Distance of bottom weld from gravity axis, and
f = Resistance offered by the weld per unit length.
Fig. Axially loaded unsymmetrical welded section
Moment of the top weld about gravity axis
And moment of the bottom weld about gravity axis
Since the sum of the moments of the weld about the gravity axis must be zero, therefore,
We know that l =
From equations (i) and (ii), we have
Lecture Notes – 34
Contents: Unsymmetrical welded joints
Axially Loaded Unsymmetrical WeldedSections
Sometimes unsymmetrical sections such as angles, channels, T-sections etc., welded on the
axially as shown in Fig. In such cases, the lengths of weld
proportioned in such a way that the sum of resisting moments of the welds about the gravity
section as shown in Fig.
= Length of weld at the top,
= Length of weld at the bottom,
= Distance of top weld from gravity axis,
= Distance of bottom weld from gravity axis, and
= Resistance offered by the weld per unit length.
Axially loaded unsymmetrical welded section
gravity axis
= la × f × a
nd moment of the bottom weld about gravity axis
= lb × f × b
Since the sum of the moments of the weld about the gravity axis must be zero, therefore,
la × f × a – lb × f × b = 0
or la × a = lb × b ...(i)
= la + lb ...(ii)
we have
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sections etc., welded on the
In such cases, the lengths of weld should be
moments of the welds about the gravity
Since the sum of the moments of the weld about the gravity axis must be zero, therefore,
Design of Machine Members-I Unit-3Lecture Notes – 34
References:
1. Machine Design - V.Bandari .
2. Machine Design – R.S. Khurmi
3. Design Data hand Book - S MD Jalaludin.
Design of Machine Members-I
Eccentrically Loaded Welded Joints
An eccentric load may be imposed on welded joints in many ways. The stresses induced on
the joint may be of different nature or of the same nature. The induced stresses are combined
depending upon the nature of stresses.
simultaneously present in a joint
Maximum normal stress,
And Maximum shear stress,
Where σb = Bending stress, and
τ = Shear stress.
When the stresses are of the same nature, these may be combined
We shall now discuss the two cases of eccentric loading as follows:
Case 1
Consider a T-joint fixed at one end and subjected to an eccentric load
shown in Fig. 1
Let s = Size of weld,
l = Length of weld, and
t = Throat thickness.
The joint will be subjected to the following two types of stresses:
1. Direct shear stress due to the shear force
2. Bending stress due to the bending moment
We know that area at the throat,
A = Throat thickness × Length of weld
= t × l × 2 = 2
= 2 × 0.707 s × l = 1.414
Shear stress in the weld (assuming uniformly distributed),
Lecture Notes – 35
Eccentrically Loaded Welded Joints
An eccentric load may be imposed on welded joints in many ways. The stresses induced on
joint may be of different nature or of the same nature. The induced stresses are combined
upon the nature of stresses. When the shear and bending stresses are
(see case 1), then maximum stresses are as follows:
Fig.1. Eccentrically loaded welded joint
When the stresses are of the same nature, these may be combined vectorially (see case 2).
We shall now discuss the two cases of eccentric loading as follows:
joint fixed at one end and subjected to an eccentric load P at a distance
The joint will be subjected to the following two types of stresses:
Direct shear stress due to the shear force P acting at the welds, and
stress due to the bending moment P × e.
= Throat thickness × Length of weld
× 2 = 2 t × l ... (For double fillet weld)
= 1.414 s × l ... (since, t = s cos 45° = 0.707 s)
(assuming uniformly distributed),
Unit-3
An eccentric load may be imposed on welded joints in many ways. The stresses induced on
joint may be of different nature or of the same nature. The induced stresses are combined
When the shear and bending stresses are
(see case 1), then maximum stresses are as follows:
oaded welded joint
vectorially (see case 2).
at a distance e as
Design of Machine Members-I
Section modulus of the weld metal through the throat,
Bending moment, M = P × e
We know that the maximum normal stress,
And maximum shear stress,
Case 2
When a welded joint is loaded eccentrically
stresses are induced:
1. Direct or primary shear stress, and
2. Shear stress due to turning moment.
Fig.2
Lecture Notes – 35
Section modulus of the weld metal through the throat,
We know that the maximum normal stress,
When a welded joint is loaded eccentrically as shown in Fig.2, the following two types of the
Direct or primary shear stress, and
Shear stress due to turning moment.
Fig.2 eccentrically loaded welded joint.
Unit-3
the following two types of the
Design of Machine Members-I
Let P = Eccentric load,
e = Eccentricity i.e. perpendicular distance
centre of gravity (G) of the throat section
l = Length of single weld,
s = Size or leg of weld, and
t = Throat thickness.
Let two loads P1 and P2 (each equal to
weld system. The effect of load
be uniform over the entire weld length. The effect of load
moment of magnitude P × e which tends of rotate the joint about
the weld system. Due to the turning
We know that the direct or primary shear stress,
Since the shear stress produced due to the turning moment (
proportional to its radial distance from
proportional to AG (r2) and is in a direction at right angles to
Where τ2 is the shear stress at the maximum distance (
distance r. Consider a small section of the weld having area
Shear force on this small section
And turning moment of this shear force about
Total turning moment over the whole weld
Lecture Notes – 35
. perpendicular distance between the line of action of
) of the throat section or fillets,
= Length of single weld,
= Size or leg of weld, and
(each equal to P) are introduced at the centre of gravity ‘
system. The effect of load P1 = P is to produce direct shear stress which is assumed to
the entire weld length. The effect of load P2 = P is to produce a turning
which tends of rotate the joint about the centre of gravity ‘
the weld system. Due to the turning moment, secondary shear stress is induced.
We know that the direct or primary shear stress,
Since the shear stress produced due to the turning moment (T = P × e) at any section is
to its radial distance from G, therefore stress due to P × e at the point
is in a direction at right angles to AG. In other words,
is the shear stress at the maximum distance (r2) and τ is the shear stress at any
Consider a small section of the weld having area dA at a distance r from
= τ × dA
And turning moment of this shear force about G,
Total turning moment over the whole weld area,
Unit-3
between the line of action of load and
) are introduced at the centre of gravity ‘G' of the
is to produce direct shear stress which is assumed to
is to produce a turning
the centre of gravity ‘G' of
) at any section is
at the point A is
. In other words,
) and τ is the shear stress at any
from G.
Design of Machine Members-I Unit-3Lecture Notes – 35
Where J = Polar moment of inertia of the throat area about G.
�Shear stress due to the turning moment i.e. secondary shear stress,
In order to find the resultant stress, the primary and secondary shear stresses are combined
vectorially.
Resultant shear stress at A,
References:
1. Machine Design - V.Bandari .
2. Machine Design – R.S. Khurmi
3. Design Data hand Book - S MD Jalaludin
Design of Machine Members-I
Problem:
A welded joint as shown in Fig. 10.24, is subjected to an eccentric load of 2 kN.
of weld, if the maximum shear stress in the weld
Problem:
A bracket carrying a load of 15 kN is to required if the allowable shear stress is not to exceed 80 MPa.
Lecture Notes – 36
A welded joint as shown in Fig. 10.24, is subjected to an eccentric load of 2 kN.
of weld, if the maximum shear stress in the weld is 25 MPa.
A bracket carrying a load of 15 kN is to be welded as shown in Fig. Find the size of weld required if the allowable shear stress is not to exceed 80 MPa.
Unit-3
A welded joint as shown in Fig. 10.24, is subjected to an eccentric load of 2 kN. Find the size
the size of weld
Design of Machine Members-I
References:
1. Machine Design - V.Bandari
2. Machine Design – R.S. Khurmi
3. Design Data hand Book - S MD Jalaludin.
Lecture Notes – 36
R.S. Khurmi
S MD Jalaludin.
Unit-3