A frame as shown in the figure below is required to fix on the ceiling using ISO class 5.8 bolts. The grip length may be taken as 45 mm. The frame is to support 10 kN as shown. Select a suitable bolt and determine tightening torque to be used if the connection is permanent and the fasteners are lubricated. Determine the portion of external load taken by members and bolts.
(a) The proof strength of class 5.8 steel is 380 MPa. The nominal load for each of the two bolts is 5 kN. A factor of safety of 2.5 is sufficient where the human life and the damage of other equipment are not involved. Hence assuming the same condition, a slightly higher factor of safety, say 3, is used in the present design.
Design over load for each bolt is 5 × 3 = 15 kN
Neglecting the stress concentration factor, we can write
\sigma_t=\frac{F}{A_t}
380=\frac{15000}{A_t}
A_t=39.47 \mathrm{~mm}^2
The appropriate standard size of the bolt is \mathrm{M} 10 \times 1.5 \text { with } A_t=58 \mathrm{~mm}^2
(b) The torque required for tightening a bolt can be written as
T=K F_i d
The torque coefficient for lubricated bolts is given as (Table 10.10)
K = 0.18
The preload on the bolts for a permanent connection, can be written as
F_i=0.90 F_p
The proof load on the bolts can be written as
F_p=A_t \sigma_p
The tensile stress area for metric M10 × 1.5 bolts, A_t=58 \mathrm{~mm}^2
Therefore, the proof load on the bolts is given as
F_P=380 \times 58=22.04 \mathrm{~kN}
Therefore, the preload on the bolts is given as
F_i=0.9 \times 22.04=19.836 \mathrm{~kN}
The tightening torque on the bolts is given as
T=0.18 \times 19.836 \times 10=35.71 \mathrm{~kN} \cdot \mathrm{mm}
(c) The stiffness of the bolt, k_b=\frac{A_d A_t E}{A_d l_t+A_t l_d}
The area of the unthreaded portion of the bolts is A_d=\frac{\pi d^2}{4}
Therefore, the area of the unthreaded portion of the bolts is given as
A_d=\frac{\pi \times 10^2}{4}=78.54 \mathrm{~mm}^2
The height of the hexagonal head of the bolt for a 10 mm size bolt and assuming regular hexagonal nut, is given as
H=0.65 d=0.65 \times 10=6.5 \mathrm{~mm}
The total length of the bolt is given as
\text { total length }=L_G+H
Therefore, the total length of the bolt is given by
Total length = 45 + 6.5 = 51.5 mm
The length of a standard bolt that is nearest to the value obtained above is given as L = 60 mm
The thread length, L_T=2 D+6
L_T=2 \times 10+6=26 \mathrm{~mm}
The length of the unthreaded portion in the grip, l_d=L-L_T
Therefore, the length of the unthreaded portion in the grip can be written as
l_d=60-26=34 \mathrm{~mm}
The length of the threaded portion in the grip, l_t=L_G-l_d
Therefore, the length of the threaded portion in the grip is given as
l_t=45-34=11 \mathrm{~mm}
The modulus of elasticity for the bolts assuming they are made of steel, E = 207 GPa Therefore, the stiffness of the bolt is given as
k_b=\frac{78.54 \times 58 \times 207 \times 10^3}{58 \times 34+78.54 \times 11}=332.5 \mathrm{~kN} / \mathrm{mm}
Assuming the steel surface as flat and smooth one, the stiffness are assumed to be proportional to their area.
Hence
\frac{k_b}{k_b+k_m}=\frac{A_d}{A_d+A_m}
A_m=A_c=d^2+0.68 d l+0.065 l^2 [Eq. (10.56)], l is grip length
A_c=d^2+0.68 d l+0.065 l^2 (10.56)
\frac{k_b}{k_b+k_m}=\frac{78.54}{78.54+537.625}=0.128
Therefore, the bolts carry 12.8% of the external load and the members carry 87.2% of the external load.
The load carried by the bolts can be written as F_b=C F+F_i
The total external load is specified to be 10 kN. Assuming the load is equally shared by the two bolts, the external load on each bolt is 5 kN.
Therefore, the load carried by each bolt is given as
F_b=0.128 \times 5+19.836=20.476 \mathrm{~kN}
The load carried by the members, F_m=(1-C) F-F_i
Therefore, the load carried by the members for each bolt is given as
F_m=(1-0.128) \times 5-19.836=-15.476 \mathrm{~kN}
TABLE 10.10 Nut Factors | |
Steel thread condition | K |
As received, stainless on mild or alloy | 0.30 |
As received, mild or alloy material | 0.20 |
Lubricated | 0.18 |
Cadmium plated | 0.16 |
Molybdenum-disulphide grease | 0.14 |
PTFE lubrication | 0.12 |