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Question Paper Code : 23850 .I
B.E./B.T~ch. ·DEGREE EXAMINATION, NOVEMBER/DECEMBER 2018.
·Fifth Semester
·Mechanical Engineering
ME 2302- DYN~CS OF MACHINERY
(Regulations 2008)
(Common to PTME 2302- Dynamics of Machinery for B.E. (Part-Time)
Four:th Semester- Mechanical Engineering - Regulations 2009)
Time : Three hours Maximum: 100 marks
Answer ALL questions.
PART A,_ (10 x 2 =20 marks)
L State:the principle of virtual work.
2. Define inertia and inert~a force.
3. Differentiate·un~alanced shaking force and shaking couple.
4. ·What do you understand by b~ancing of revolving masses?
•
5. Why transient solution is not considered in the ·response of forced damped
vibrating system?_
6. If a damper exerts a force of 30 kN at a speed of 2 m/sec, movement, determine
the damping coefficient. .
7. Define step input and harmonic: forcing function.
8. Define transmissibility.
9. The governor control system belongs to which type?
10. List some of the terms used in connection with the motion of naval ships.
BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 1
PART B- (5 x 16 =80 marks)
11. (a) A vertical.petrol engine 150 mm diameter· and 200 mm stroke has a
connecting rod 350 mm long. The mass of the piston is 1.6 kg andengine
speed is 1800 rpm. On the eJq>ansion stroke with crank angle 30° from
top dead centre, "the gas· pressure is 750 kN/m2• Determine the net thrust
on the piston. (16)
Or
(b) The turning moment diagram for mufti cylinder engine has been drawn
to a vertical scale of 1· mm' = 650 Nm and a horizontal scale of
1 mm = 4.5°. The areas above and below the mean torque line are
-28, + 380, ·-260, +310, -300, +242, -380, +265 imd -229 mm2, the
fluctuation of speed is limited to ±1.8% of the mean speed which is 400
rpm. Density of rim material is 700 kg/m3 and width of the rim is 4.5
times its thickness. The hoop stress iii the rim material is limited to 6
.N/mm2 Neglecting the effect Qf the boss and arms,. determine diameter.
and cross section, of fly wheel rim. ·(16}
12. (a) A mass of 110 kg is fuced to a rotating shaft so that distance ofits mass
centre from the ·axis o( rotation is 228 mm. Find balancing masses in
following twq conditions :
(i) Two masses - one on left of disturbing ma:ss at a distance of
100 mm and radius 400 mm; and other on right at a distance of
200 mm and ra_dius of 150 mm. (8)
(ii) Two masses placed on right of the disturbing mass respectively at
distance of 100 and 200 rilm and radii of 400 and 200 mm. The
masses are placed"in the same axial plane. (8)
Or
(b) The cylinders of twin V-erigine are set at 60° angle with both pistons
connected to a single crank through their respective connecting rods,
Each coqnecting rod is 500 nim long and the cra:n,k radius is 100 mm. The
.total rotating mass is equivalent to 1.5 kg at the crank radius and the
• reciprocating mass is 1.8 kg per piston. A balance mass is also fitted
. opposite to the crank equivalent to 2 kg at a radius of 140 )llni,
Determine the maximum. and minimum values of the ptimary and
secondary forces due to inertia of the reciprocating and the rotating:
masses if the eng{ne speed is 700 rpm. (16)
2 23850
BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 2
l
13. {a) A rotor has mass of 12 kg and is mounted midway on a 21 mm diameter
horizontal shaft supported at the ends by two bearings. The bearings are
1 m apart. The shaft rotates at 2400 rpm. Ifthe center of mass of the
rotor is 0.111 mm above from the ge~mietric centre of the rotor due to a
. certain manufacturing defects; find the amplitude of the steady state
vibration a~d the dynamic force transmitted to the bearing. Take
E =200 GN/m2• (16)
Or
(b) A shaft carries two masses. The mass A is 300 kg with radius of gyration ·
-of 0.75ni and the mass B is 500 kg with radiusof gyration of 0.9 m. The
shaft is a stepped shaft having; 100 mm diameter for 300 mm length, 150
-
· mm diameter for 160 mm length, 120 nim diameter for 125 mm ~ength
and 90 mm diameter for 400 rom length. Determine the frequency of the
natural torsional vibration. lfit is desired to have node at the mid section
of shaft· of 120 mni diameter by changing the diameter of the section
having 90 mm ·diameter, what will be the new· diameter. Take
U = 84 GN/m~.  (16)
14. (a) A flywheel having a mass of 35 kg was allowed to swing as pendulum ~
about a knife-edge at the inner side-of the rim, as shown in Fig. 14 (a). If
the measured time period o{ oscillation was 1.25 second, determine the
moment of inertia of the flywheel about its geometric axis. ·
Flywheel as pendulum.
·Fig. 14(a)
·Or
(b) The disc. of a torsional pendulum has a moment of inertia of 0.068 kg-m2
and is immersed in a vis.cous fluid. The brass shaft (G ::: 40 GN/m2)
attached to it is of 10 mm diameter and 380 mm length, ·When the
pendulum is vibrating the amplitudes on the same side of the rest
position for successive cycles are 5°, 39
and 1.8°. Determine
(i) · the logarithmic decrement,
(ii) the .damping torque :;tt unit v:elocity
':
(iii) the periodic time of vibration. What would be the frequency of
vibrations if the disc·were removed from the viscous fluid?
3 23850
BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 3
. '
15. (a) (i) Explain the function of a proell governor with the help of a neat
sketch. Derive the relationship am:ong the various forces a~ting on
the linlc · ~ (8)
(ii) What are centrifugal governors? How do they differ from inertia
governors? (8)
Or
· (b) (i) The turbine rotor of a ship has mass of 2.2 tonnes and rotates at
1800 rpm clockwise when viewed from the aft. Tl;le radius of
gyration of the rotor is 320 rpm. Determine gyroscopic Couple and
its effect when
(1) The ship turns right at a radius of·250 m ·with a speed of
25kmlh. . .
(2) The ship pitches with the bow rising at an angular velocity of
0.8 radls.
(3) Th~ ship rolls at an angular velocity of 0.1 radls. · (8)
(ii) What is the effect of gyroscopic couple on the stability of a two
wheel-vehi~le taking a turn? (8). .
.. 4 23850
BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 4

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Me2302 KINEMATICS OF MACHINERY

  • 1. Question Paper Code : 23850 .I B.E./B.T~ch. ·DEGREE EXAMINATION, NOVEMBER/DECEMBER 2018. ·Fifth Semester ·Mechanical Engineering ME 2302- DYN~CS OF MACHINERY (Regulations 2008) (Common to PTME 2302- Dynamics of Machinery for B.E. (Part-Time) Four:th Semester- Mechanical Engineering - Regulations 2009) Time : Three hours Maximum: 100 marks Answer ALL questions. PART A,_ (10 x 2 =20 marks) L State:the principle of virtual work. 2. Define inertia and inert~a force. 3. Differentiate·un~alanced shaking force and shaking couple. 4. ·What do you understand by b~ancing of revolving masses? • 5. Why transient solution is not considered in the ·response of forced damped vibrating system?_ 6. If a damper exerts a force of 30 kN at a speed of 2 m/sec, movement, determine the damping coefficient. . 7. Define step input and harmonic: forcing function. 8. Define transmissibility. 9. The governor control system belongs to which type? 10. List some of the terms used in connection with the motion of naval ships. BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 1
  • 2. PART B- (5 x 16 =80 marks) 11. (a) A vertical.petrol engine 150 mm diameter· and 200 mm stroke has a connecting rod 350 mm long. The mass of the piston is 1.6 kg andengine speed is 1800 rpm. On the eJq>ansion stroke with crank angle 30° from top dead centre, "the gas· pressure is 750 kN/m2• Determine the net thrust on the piston. (16) Or (b) The turning moment diagram for mufti cylinder engine has been drawn to a vertical scale of 1· mm' = 650 Nm and a horizontal scale of 1 mm = 4.5°. The areas above and below the mean torque line are -28, + 380, ·-260, +310, -300, +242, -380, +265 imd -229 mm2, the fluctuation of speed is limited to ±1.8% of the mean speed which is 400 rpm. Density of rim material is 700 kg/m3 and width of the rim is 4.5 times its thickness. The hoop stress iii the rim material is limited to 6 .N/mm2 Neglecting the effect Qf the boss and arms,. determine diameter. and cross section, of fly wheel rim. ·(16} 12. (a) A mass of 110 kg is fuced to a rotating shaft so that distance ofits mass centre from the ·axis o( rotation is 228 mm. Find balancing masses in following twq conditions : (i) Two masses - one on left of disturbing ma:ss at a distance of 100 mm and radius 400 mm; and other on right at a distance of 200 mm and ra_dius of 150 mm. (8) (ii) Two masses placed on right of the disturbing mass respectively at distance of 100 and 200 rilm and radii of 400 and 200 mm. The masses are placed"in the same axial plane. (8) Or (b) The cylinders of twin V-erigine are set at 60° angle with both pistons connected to a single crank through their respective connecting rods, Each coqnecting rod is 500 nim long and the cra:n,k radius is 100 mm. The .total rotating mass is equivalent to 1.5 kg at the crank radius and the • reciprocating mass is 1.8 kg per piston. A balance mass is also fitted . opposite to the crank equivalent to 2 kg at a radius of 140 )llni, Determine the maximum. and minimum values of the ptimary and secondary forces due to inertia of the reciprocating and the rotating: masses if the eng{ne speed is 700 rpm. (16) 2 23850 BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 2
  • 3. l 13. {a) A rotor has mass of 12 kg and is mounted midway on a 21 mm diameter horizontal shaft supported at the ends by two bearings. The bearings are 1 m apart. The shaft rotates at 2400 rpm. Ifthe center of mass of the rotor is 0.111 mm above from the ge~mietric centre of the rotor due to a . certain manufacturing defects; find the amplitude of the steady state vibration a~d the dynamic force transmitted to the bearing. Take E =200 GN/m2• (16) Or (b) A shaft carries two masses. The mass A is 300 kg with radius of gyration · -of 0.75ni and the mass B is 500 kg with radiusof gyration of 0.9 m. The shaft is a stepped shaft having; 100 mm diameter for 300 mm length, 150 - · mm diameter for 160 mm length, 120 nim diameter for 125 mm ~ength and 90 mm diameter for 400 rom length. Determine the frequency of the natural torsional vibration. lfit is desired to have node at the mid section of shaft· of 120 mni diameter by changing the diameter of the section having 90 mm ·diameter, what will be the new· diameter. Take U = 84 GN/m~. (16) 14. (a) A flywheel having a mass of 35 kg was allowed to swing as pendulum ~ about a knife-edge at the inner side-of the rim, as shown in Fig. 14 (a). If the measured time period o{ oscillation was 1.25 second, determine the moment of inertia of the flywheel about its geometric axis. · Flywheel as pendulum. ·Fig. 14(a) ·Or (b) The disc. of a torsional pendulum has a moment of inertia of 0.068 kg-m2 and is immersed in a vis.cous fluid. The brass shaft (G ::: 40 GN/m2) attached to it is of 10 mm diameter and 380 mm length, ·When the pendulum is vibrating the amplitudes on the same side of the rest position for successive cycles are 5°, 39 and 1.8°. Determine (i) · the logarithmic decrement, (ii) the .damping torque :;tt unit v:elocity ': (iii) the periodic time of vibration. What would be the frequency of vibrations if the disc·were removed from the viscous fluid? 3 23850 BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 3
  • 4. . ' 15. (a) (i) Explain the function of a proell governor with the help of a neat sketch. Derive the relationship am:ong the various forces a~ting on the linlc · ~ (8) (ii) What are centrifugal governors? How do they differ from inertia governors? (8) Or · (b) (i) The turbine rotor of a ship has mass of 2.2 tonnes and rotates at 1800 rpm clockwise when viewed from the aft. Tl;le radius of gyration of the rotor is 320 rpm. Determine gyroscopic Couple and its effect when (1) The ship turns right at a radius of·250 m ·with a speed of 25kmlh. . . (2) The ship pitches with the bow rising at an angular velocity of 0.8 radls. (3) Th~ ship rolls at an angular velocity of 0.1 radls. · (8) (ii) What is the effect of gyroscopic couple on the stability of a two wheel-vehi~le taking a turn? (8). . .. 4 23850 BIBIN.C / ASSOCIATE PROFESSOR / MECHANICAL ENGINEERING / RMK COLLEGE OF ENGINEERING AND TECHNOLOGY 4