Figure below shows a shaft mounted in bearings at A and D and having pulleys at B and C. The forces shown acting on the pulley surfaces represent the belt tensions. The shaft is to be made of AISI 1020 HR steel. Using a conservative failure theory with a design factor of 2.5, determine the minimum shaft diameter to avoid yielding.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Figure below shows a shaft mounted in bearings at A and D and having pulleys at B and C. The
forces shown acting on the pulley surfaces represent the belt tensions. The shaft is to be made of
AISI 1020 HR steel. Using a conservative failure theory with a design factor of 2.5, determine the
minimum shaft diameter to avoid yielding.
1218 N
1) Load determination; Ay=_
Z
100 mm
200 N
Fill in the blank with the correct answers.
B
200 mm D.
A: =
(Put a negative (-) sign if it against the direction of the axis)
300 mm D.
100 mm
N;
1618 ND
100 N
C 80 mm
Dy=
D:=
Z
N
Transcribed Image Text:Figure below shows a shaft mounted in bearings at A and D and having pulleys at B and C. The forces shown acting on the pulley surfaces represent the belt tensions. The shaft is to be made of AISI 1020 HR steel. Using a conservative failure theory with a design factor of 2.5, determine the minimum shaft diameter to avoid yielding. 1218 N 1) Load determination; Ay=_ Z 100 mm 200 N Fill in the blank with the correct answers. B 200 mm D. A: = (Put a negative (-) sign if it against the direction of the axis) 300 mm D. 100 mm N; 1618 ND 100 N C 80 mm Dy= D:= Z N
2) Bending moment load;
3) Torque at location B and C;
At location B;
At location C;
MB_z =
4) Stresses at location B and C in term of 'd';
At location B;
MB
At location C;
MB =
Ox_B=_
Ox_c=
TB=
Tmax B
Tmax C
Nm ; Mc_=_
Nm
5) Maximum shear stress at location B and C in term of 'd';
S
Nm ; Mc
Pa;
Pa;
Pa
Nm ;
Pa
Mcy=
Txy_B=_
Txy_C=
Tc=
Nm
Nm
Nm
Pa
Pa
Nm
Transcribed Image Text:2) Bending moment load; 3) Torque at location B and C; At location B; At location C; MB_z = 4) Stresses at location B and C in term of 'd'; At location B; MB At location C; MB = Ox_B=_ Ox_c= TB= Tmax B Tmax C Nm ; Mc_=_ Nm 5) Maximum shear stress at location B and C in term of 'd'; S Nm ; Mc Pa; Pa; Pa Nm ; Pa Mcy= Txy_B=_ Txy_C= Tc= Nm Nm Nm Pa Pa Nm
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