static and fatigue bolt design 03 may 2015 dr. ghassan mousa
TRANSCRIPT
STATIC AND FATIGUE BOLT DESIGN
03 May 2015
Dr. Ghassan Mousa
Thread standards & definition• d: major diameter
• p: pitch
• l: lead
• Multiple threads
Fig. 8.1 Terminology of screw threads
http://www.gizmology.net/nutsbolts.htm
• The thread size is specified by the p for metric sizes.
• At is tensile stress area of unthreaded rod.
Table 8-1 Geometrical data for Standard Bolts (SI)
Bolt Types
Three types of threaded fastener. (a) Bolt and nut; (c) Cap screw; (c) stud.
Bolt strength
Bolts in axial loading fail at the:
•Fillet under the head.
•Thread runout.
•1st thread engaged in the nut.
Table 8-11 Material properties of steel bolts
Tension joints• Fi: preload
• Fb = Pb + Fi . Total force in each bolt
• Fm = Pm – Fi. Force Carried by the Joint
• P: external tensile load per bolt
• Pb: portion of P taken by bolt
• Pm: portion of P taken by members
• C: stiffness constant of the joints
(joint constant)
Fig. 8.13 A bolted connection loaded in tension by the forces P
¿𝐹 𝑏=𝐹 𝑖+𝑃𝐶
Static load
Fi can be determined as:where SP is the proof strength and can be found in tables 8 -11
𝑛𝑝=𝑆𝑝 𝐴𝑡
𝐶𝑃+𝐹𝑖
Yield factor of safety guarding against exceeding Sp
𝑛𝐿=𝑆𝑝 𝐴𝑡−𝐹 𝑖
𝐶𝑃Load factor of safety guarding against overloading
𝑛0=𝐹𝑖
¿¿Load factor for joint separation
b: Joint Separation
BOLT FAILURE MODES
0Fm
To separate the joint:
𝑛0=𝑃𝑚𝑎𝑥
𝑃
a: tensile failure
𝜎 𝑏=𝐹 𝑏
𝐴𝑡
𝑛𝑏=𝑆𝑏
𝜎𝑏
𝑛𝑝=𝑆𝑝 𝐴𝑡
𝐶𝑃+𝐹𝑖
𝑛𝐿=𝑆𝑝 𝐴𝑡−𝐹 𝑖
𝐶𝑃
𝑛0=𝐹𝑖
¿¿
An M14x2 grade 5.8 bolt is used in a bolted connection. The joint constant is C = 0.3498. The factors of safety to be applied are 2 against tensile stress failure and 3.5 against joint separation.
Calculate the maximum force (P) that can be applied to this unit for reusable application.
Example of bolt under static load
Solution.
a) Tensile Failure
2t mm115A MPa380S p
𝑛𝐿=𝑆𝑝 𝐴𝑡−𝐹 𝑖
𝐶𝑃
From table 8-1 & 8-11
= 15.6 kN
b) Joint separation
𝑛0=𝐹𝑖
¿¿ = 14.4 kN
𝐹 𝑖=0.75𝑆𝑝 𝐴𝑡
= 32.775 kN
Gasketed joints
𝑛𝑝=𝑆𝑝 𝐴𝑡
𝐶 (𝑃 𝑡𝑜𝑡𝑎𝑙 /𝑁 )+𝐹 𝑖
𝑛𝐿=𝑆𝑝 𝐴𝑡−𝐹 𝑖
𝐶 (𝑃 𝑡𝑜𝑡𝑎𝑙/𝑁 )
𝑛0=𝐹𝑖
¿¿
3≤𝜋 𝐷𝑏
𝑁𝑑≤6
Where:
• N is the no. of bolts
• is the diameter of the bolt circle
• is 0.75 or 0.9
𝑁 𝐴𝑡=𝑛𝐿𝐶𝑃
(1−𝛼)𝑆𝑃
𝑁 𝐴𝑡=𝑛0(1−𝐶 )𝑃
𝛼𝑆𝑃
OR
OR
𝐷𝑏
A cylinder of internal diameter 1000mm and wall thickness 3mm is subjected to an internal pressure equivalent to 1.5 MPa. Assume safety factors of 2.5 against bolt tensile failure, 3.5 against joint separation, and class 8.8 bolts in either fine or coarse threads.
Design a suitable bolt group for the cylinder head for reusable application and an assumed joint constant of 0.45. Give a suitable bolt pitch circle diameter, .
Example of bolt under static load (gasket joint)
Solution
MPaS p 600 From table 8-1 & 8-11
=
𝐶=𝑝𝑖𝐷
f∨a siutable spacingbetween bolts ,𝑁 canbe estimated as 36bolts
Solution (cont.)
, we can select M20x1.5 from Table 8-1
𝐷𝑏canbeestimated as
1000 + 2(3)+2(47) = 1100
𝜋 𝐷𝑏
𝑁𝑑𝜋 110036∗20
=4.8
NUMBER OF BOLTS = 36BOLT DESIGNATION : M20 X 1.5BOLT PITCH CIRCLE DIAMETER = 1100 mm(NOTE: This is only one possible solution)
Load variation Per Bolt
N
CPFi
min
N
CPFi
max
iFt
Dynamic Loading a) Tensile Failure
The alternating and mean forces per bolt are, respectively,
N
PCNCP
FN
CPF
P aii
a
2
minmax
N
PCF
NCP
FN
CPF
P mi
ii
m
2
minmax
Dynamic Loading (cont.)
2
PPP minmaxa
2
PPP minmaxm
where
where
Applying to the external load at both equations and substitute in Goodman line and rearranging:
emuta
puttef SPSP
SS
C
NASn
put
emuta
e
ft SS
SPSP
NS
CnA
where
a) Tensile Failure
Load variation Per Bolt
N
PCFi
min)1(
N
PCFi
max)1(
Fmt
Dynamic Loading (cont.)b) Joint Separation
1)1( max
2
PC
NFn if
Dynamic Loading (cont.)
where
b) Joint Separation
Table 8-17 Material Properties (Endurance Strength) for Standard Bolts (SI)
The fluctuating pressure in the cylinder shown is given by:
Using Class 10.9 M24x2 bolts with a factor of safety of 2.5 against bolt tensile failure and 3 against joint separation.
determine the number of bolts which should be used for the application. Assume that the bolts carry 25% of the external load. Assume a reusable application.
Example of bolt under dynamic load
26m/N)tcos2(10p
Solution.
2384 mmAt MPaS p 830 From table 8-1 & 8-11𝑆𝑢𝑡=1040MPa
𝑆𝑒=162MPa From table 8-17
= 0.75 𝐶=0.25
N4
1*10*3P
26
max
N4
1*10*1P
26
min
N4
1*10*1
2
PPP
26minmax
a
N4
1*10*2
2
PPP
26minmax
m
N4
1*10*3P
26
max
N4
1*10*1P
26
min
N4
1*10*1
2
PPP
26minmax
a
N4
1*10*2
2
PPP
26minmax
m
N4
1*10*3P
26
max
N4
1*10*1P
26
min
N4
1*10*1
2
PPP
26minmax
a
N4
1*10*2
2
PPP
26minmax
m
N4
1*10*3P
26
max
N4
1*10*1P
26
min
N4
1*10*1
2
PPP
26minmax
a
N4
1*10*2
2
PPP
26minmax
m
Solution (cont.)a) Tensile Failure b) Joint separation
1.22
)1( max
tpf AS
PCnN
26
put
emuta
te
f
SS
SPSP
AS
CnN
𝜋 𝐷𝑏
𝑁𝑑𝜋 11602 6∗24
=5 .8
Check the bolt spacing with N is 26:
Check the bolt spacing with N is 30:
𝜋 116030∗24
=5 .06