10.3.1 Effective Areas of Bolts
10.3.1.1
Since threads can occur in the shear plane, the area for resisting shear should normally be taken as the net tensile stress area, of the bolts. For bolts where the net tensile stress area is not defined, shall be taken as the area at the root of the threads.
10.3.1.2
Where it can be shown that the threads do not occur in the shear plane, may be taken as the cross section area, at the shank.
10.3.1.3
In the calculation of thread length, allowance should be made for tolerance and thread run off.
10.3.2
A bolt subjected to a factored shear force ( shall satisfy the condition
where is the design strength of the bolt taken as the smaller of the value as governed by shear, (see 10.3.3) and bearing, (see 10.3.4).
10.3.3 Shear Capacity of Bolt
The design strength of the bolt, as governed shear strength is given by:
where
where
ultimate tensile strength of a bolt.
- number of shear planes with thread intercepting the shear plane;
nominal plain shank area of the bolt; and
- = net shear area of the bolt at threads, may be taken as the area corresponding to root diameter at the thread.
10.3.3.1 Long joints
When the length of the joint, of a splice or end connection in a compression or tension element containing more than two bolts (that is the distance between the first and last rows of bolts in the joint, measured in the direction of the load transfer) exceeds in the direction of load, the nominal shear capacity (see 10.3.2), shall be reduced by the factor , given by:
where
= Nominal diameter of the fastener
NOTE — This provision does not apply when the distribution of shear over the length of joint is uniform, as in the connection of web of a section to the flanges.
10.3.3.2 Large grip lengths
When the grip length, (equal to the total thickness of
the connected plates) exceeds 5 times the diameter, of the bolts, the design shear capacity shall be reduced by a factor , given by:
shall not be more than given in 10.3.3.1. The grip length, shall in no case be greater than .
10.3.3.3 Packing plates
The design shear capacity of bolts carrying shear through a packing plate in excess of 6 mm shall be decreased by a factor, given by:
where
thickness of the thicker packing, in mm.
10.3.4 Bearing Capacity of the Bolt
The design bearing strength of a bolt on any plate, as governed by bearing is given by:
where
vnpb = nominal bearing strength of a bolt = 2.5 k~ d tfu
where
is smaller of ;
= end and pitch distances of the fastener along bearing direction;
diameter of the hole;
- nominal diameter of the bolt; and
- summation of the thicknesses of the connected plates experiencing bearing stress in the same direction, or if the bolts are countersunk, the thickness of the plate minus one half of the depth of countersinking.
The bearing resistance (in the direction normal to the slots in slotted holes) of bolts in holes other than standard clearance holes may be reduced by multiplying the bearing resistance obtained as above, , by the factors given below:
- a) Over size and short slotted holes – 0.7, and
- b) Long slotted holes - 0.5.
NOTE - The block shear of the edge distance due to bearing force may be checked as given in 6.4.
10.3.5 Tension Capacity
A bolt subjected to a factored tensile force, shall satisfy:
where
where
ultimate tensile stress of the bolt.
yield stress of the bolt,
net tensile stress area as specified in the appropriate Indian Standard (for bolts where the tensile stress area is not defined, shall be taken as the area at the bottom of the threads), and
shank area of the bolt.
10.3.6 Bolt Subjected to Combined Shear and Tension
A bolt required to resist both design shear force (Vsd) and design tensile force (Tb) at the same time shall satisfy:
where
- factored shear force acting on the bolt.
=
- design shear capacity (see 10.3.2)
- factored tensile force acting on the bolt, and
- design tension capacity (see 10.3.5)