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11/6/2014 1
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
Unit 4: Balancing of Rotating Masses
• Static and dynamic balancing
• Balancing of single rotating mass by balancing
masses in same plane and in different planes.
• Balancing of several rotating masses by
balancing masses in same plane and in different
planes.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
2
What is Balancing ?
• Often an unbalance of forces is produced in rotary or
reciprocating machinery due to the inertia forces
associated with the moving masses.
• Balancing is the process of designing or modifying
machinery so that the unbalance is reduced to an
acceptable level and if possible is eliminated entirely.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
3
• A particle or mass moving in a circular path experiences a centripetal
acceleration and a force is required to produce it.
• An equal and opposite force acting radially outwards acts on the axis
of rotation and is known as centrifugal force .
• This is a disturbing force on the axis of rotation, the magnitude of
which is constant but the direction changes with the rotation of the
mass.
• In a revolving rotor, the centrifugal force remains balanced as long as
the centre of the mass of the rotor lies on the axis of the shaft.
• When the centre of mass does not lie on the axis or there is an
eccentricity, an unbalanced force is produced
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
4
Why Balancing is necessary?
• The high speed of engines and other machines is a
common phenomenon now-a-days.
• It is, therefore, very essential that all the rotating and
reciprocating parts should be completely balanced as
far as possible.
• If these parts are not properly balanced, the dynamic
forces are set up.
• These forces not only increase the loads on bearings
and stresses in the various members, but also produce
unpleasant and even dangerous vibrations.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
5
Balancing of Rotating Masses
• Whenever a certain mass is attached to a rotating shaft, it
exerts some centrifugal force, whose effect is to bend the
shaft and to produce vibrations in it.
• In order to prevent the effect of centrifugal force, another
mass is attached to the opposite side of the shaft, at such a
position so as to balance the effect of the centrifugal force
of the first mass.
• This is done in such a way that the centrifugal force of both
the masses are made to be equal and opposite.
• The process of providing the second mass in order to
counteract the effect of the centrifugal force of the first
mass, is called balancing of rotating masses.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
6
Balancing of Rotating Masses
• The following cases are important from the subject point of
view:
1. Balancing of a single rotating mass by a single mass rotating in
the same plane.
2. Balancing of a single rotating mass by two masses rotating in
different planes.
3. Balancing of different masses rotating in the same plane.
4. Balancing of different masses rotating in different planes.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
7
Balancing of a Single Rotating Mass By a Single Mass Rotating in the
Same Plane
• Consider a disturbing mass m1 attached to a shaft rotating at ω rad/s as shown in
Fig.
• Let r1 be the radius of rotation of the mass m1 (i.e. distance between the axis of
rotation of the shaft and the centre of gravity of the mass m1).
• We know that the centrifugal force exerted by the mass m1 on the shaft,
• This centrifugal force acts radially outwards and thus produces bending moment on
the shaft.
• In order to counteract the effect of this force, a balancing mass (m2) may be
attached in the same plane of rotation as that of disturbing mass (m1) such that
the centrifugal forces due to the two masses are equal and opposite.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
8
Balancing of a Single Rotating Mass By a Single Mass Rotating in the
Same Plane
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
9
Balancing of a Single Rotating Mass By Two Masses Rotating in
Different Planes
• In the previous arrangement for balancing gives rise to a couple which tends to
rock the shaft in its bearings.
• Therefore in order to put the system in complete balance, two balancing masses
are placed in two different planes, parallel to the plane of rotation of the disturbing
mass, in such a way that they satisfy the following two conditions of equilibrium.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
10
The conditions (1) and (2) together give
dynamic balancing.
Balancing of a Single Rotating Mass By Two Masses
Rotating in Different Planes
• The following two possibilities may arise while
attaching the two balancing masses :
1. The plane of the disturbing mass may be in between
the planes of the two balancing masses, and
2. The plane of the disturbing mass may lie on the left or
right of the two planes containing the balancing
masses.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
11
1. When the plane of the disturbing mass lies in between the planes
of the two balancing masses
• Consider a disturbing mass m lying in a plane A to be balanced by two rotating
masses m1 and m2 lying in two different planes L and M as shown in Fig.
• Let r, r1 and r2 be the radii of rotation of the masses in planes A, L and M
respectively.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
12
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
13
• It may be noted that equation (i) represents the condition for static
balance, but in order to achieve dynamic balance, equations (ii) or (iii)
must also be satisfied.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
14
When the plane of the disturbing mass lies on one end of the planes of
the balancing masses
• In this case, the mass m lies in the plane A and the balancing masses
lie in the planes L and M, as shown in Fig.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
15
As discussed above, the following conditions must be satisfied in order
to balance the system, i.e.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
16
Balancing of Several Masses Rotating in the Same Plane
• The magnitude and position of the balancing
mass may be found out analytically or
graphically as discussed below :
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
17
1. Analytical method
• The magnitude and direction of the balancing mass may be obtained, analytically,
as discussed below :
1. First of all, find out the centrifugal force exerted by each mass on the rotating shaft.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
18
2. Graphical method
• The magnitude and position of the balancing mass may also be
obtained graphically as discussed below :
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
19
2. Graphical method
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
20
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
22
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
23
Take: 10kg-m=1cm
Balancing of Several Masses Rotating in Different Planes
• When several masses revolve in different planes, they may be transferred to a
reference plane (briefly written as R.P.), which may be defined as the plane passing
through a point on the axis of rotation and perpendicular to it.
• The effect of transferring a revolving mass (in one plane) to a reference plane is to
cause a force of magnitude equal to the centrifugal force of the revolving mass to
act in the reference plane, together with a couple of magnitude equal to the
product of the force and the distance between the plane of rotation and the
reference plane.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
24
Balancing of Several Masses Rotating in Different Planes
• In order to have a complete balance of the several revolving masses
in different planes, the following two conditions must be satisfied :
1. The forces in the reference plane must balance, i.e. the resultant force must
be zero.
2. The couples about the reference plane must balance, i.e. the resultant couple
must be zero.
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
25
Balancing of Several Masses Rotating in Different Planes
• Let us now consider four masses m1, m2, m3 and m4 revolving in planes 1, 2, 3 and
4 respectively as shown in Fig. (a).
• The relative angular positions of these masses are shown in the end view [Fig. (b)].
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
26
The magnitude of the balancing masses mL and mM in planes L and M
may be obtained as discussed below :
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
27
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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in the clockwise direction from mass mA
in the clockwise direction from mass mA
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
34
11/6/2014
Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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Hareesha N G, Dept of Aero Engg, DSCE,
Blore
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11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 37
11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 38
It is assumed that the mass of pulley B acts in vertical direction.
For the static balance of the pulleys, the centre of gravity of the system
must lie on the axis of rotation. Therefore a force polygon must be a
closed figure.
11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 39
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11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 52
11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 53

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Balancing ppt

  • 1. 11/6/2014 1 Hareesha N G, Dept of Aero Engg, DSCE, Blore
  • 2. Unit 4: Balancing of Rotating Masses • Static and dynamic balancing • Balancing of single rotating mass by balancing masses in same plane and in different planes. • Balancing of several rotating masses by balancing masses in same plane and in different planes. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 2
  • 3. What is Balancing ? • Often an unbalance of forces is produced in rotary or reciprocating machinery due to the inertia forces associated with the moving masses. • Balancing is the process of designing or modifying machinery so that the unbalance is reduced to an acceptable level and if possible is eliminated entirely. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 3
  • 4. • A particle or mass moving in a circular path experiences a centripetal acceleration and a force is required to produce it. • An equal and opposite force acting radially outwards acts on the axis of rotation and is known as centrifugal force . • This is a disturbing force on the axis of rotation, the magnitude of which is constant but the direction changes with the rotation of the mass. • In a revolving rotor, the centrifugal force remains balanced as long as the centre of the mass of the rotor lies on the axis of the shaft. • When the centre of mass does not lie on the axis or there is an eccentricity, an unbalanced force is produced 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 4
  • 5. Why Balancing is necessary? • The high speed of engines and other machines is a common phenomenon now-a-days. • It is, therefore, very essential that all the rotating and reciprocating parts should be completely balanced as far as possible. • If these parts are not properly balanced, the dynamic forces are set up. • These forces not only increase the loads on bearings and stresses in the various members, but also produce unpleasant and even dangerous vibrations. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 5
  • 6. Balancing of Rotating Masses • Whenever a certain mass is attached to a rotating shaft, it exerts some centrifugal force, whose effect is to bend the shaft and to produce vibrations in it. • In order to prevent the effect of centrifugal force, another mass is attached to the opposite side of the shaft, at such a position so as to balance the effect of the centrifugal force of the first mass. • This is done in such a way that the centrifugal force of both the masses are made to be equal and opposite. • The process of providing the second mass in order to counteract the effect of the centrifugal force of the first mass, is called balancing of rotating masses. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 6
  • 7. Balancing of Rotating Masses • The following cases are important from the subject point of view: 1. Balancing of a single rotating mass by a single mass rotating in the same plane. 2. Balancing of a single rotating mass by two masses rotating in different planes. 3. Balancing of different masses rotating in the same plane. 4. Balancing of different masses rotating in different planes. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 7
  • 8. Balancing of a Single Rotating Mass By a Single Mass Rotating in the Same Plane • Consider a disturbing mass m1 attached to a shaft rotating at ω rad/s as shown in Fig. • Let r1 be the radius of rotation of the mass m1 (i.e. distance between the axis of rotation of the shaft and the centre of gravity of the mass m1). • We know that the centrifugal force exerted by the mass m1 on the shaft, • This centrifugal force acts radially outwards and thus produces bending moment on the shaft. • In order to counteract the effect of this force, a balancing mass (m2) may be attached in the same plane of rotation as that of disturbing mass (m1) such that the centrifugal forces due to the two masses are equal and opposite. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 8
  • 9. Balancing of a Single Rotating Mass By a Single Mass Rotating in the Same Plane 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 9
  • 10. Balancing of a Single Rotating Mass By Two Masses Rotating in Different Planes • In the previous arrangement for balancing gives rise to a couple which tends to rock the shaft in its bearings. • Therefore in order to put the system in complete balance, two balancing masses are placed in two different planes, parallel to the plane of rotation of the disturbing mass, in such a way that they satisfy the following two conditions of equilibrium. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 10 The conditions (1) and (2) together give dynamic balancing.
  • 11. Balancing of a Single Rotating Mass By Two Masses Rotating in Different Planes • The following two possibilities may arise while attaching the two balancing masses : 1. The plane of the disturbing mass may be in between the planes of the two balancing masses, and 2. The plane of the disturbing mass may lie on the left or right of the two planes containing the balancing masses. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 11
  • 12. 1. When the plane of the disturbing mass lies in between the planes of the two balancing masses • Consider a disturbing mass m lying in a plane A to be balanced by two rotating masses m1 and m2 lying in two different planes L and M as shown in Fig. • Let r, r1 and r2 be the radii of rotation of the masses in planes A, L and M respectively. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 12
  • 13. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 13
  • 14. • It may be noted that equation (i) represents the condition for static balance, but in order to achieve dynamic balance, equations (ii) or (iii) must also be satisfied. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 14
  • 15. When the plane of the disturbing mass lies on one end of the planes of the balancing masses • In this case, the mass m lies in the plane A and the balancing masses lie in the planes L and M, as shown in Fig. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 15
  • 16. As discussed above, the following conditions must be satisfied in order to balance the system, i.e. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 16
  • 17. Balancing of Several Masses Rotating in the Same Plane • The magnitude and position of the balancing mass may be found out analytically or graphically as discussed below : 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 17
  • 18. 1. Analytical method • The magnitude and direction of the balancing mass may be obtained, analytically, as discussed below : 1. First of all, find out the centrifugal force exerted by each mass on the rotating shaft. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 18
  • 19. 2. Graphical method • The magnitude and position of the balancing mass may also be obtained graphically as discussed below : 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 19
  • 20. 2. Graphical method 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 20
  • 21. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 21
  • 22. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 22
  • 23. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 23 Take: 10kg-m=1cm
  • 24. Balancing of Several Masses Rotating in Different Planes • When several masses revolve in different planes, they may be transferred to a reference plane (briefly written as R.P.), which may be defined as the plane passing through a point on the axis of rotation and perpendicular to it. • The effect of transferring a revolving mass (in one plane) to a reference plane is to cause a force of magnitude equal to the centrifugal force of the revolving mass to act in the reference plane, together with a couple of magnitude equal to the product of the force and the distance between the plane of rotation and the reference plane. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 24
  • 25. Balancing of Several Masses Rotating in Different Planes • In order to have a complete balance of the several revolving masses in different planes, the following two conditions must be satisfied : 1. The forces in the reference plane must balance, i.e. the resultant force must be zero. 2. The couples about the reference plane must balance, i.e. the resultant couple must be zero. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 25
  • 26. Balancing of Several Masses Rotating in Different Planes • Let us now consider four masses m1, m2, m3 and m4 revolving in planes 1, 2, 3 and 4 respectively as shown in Fig. (a). • The relative angular positions of these masses are shown in the end view [Fig. (b)]. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 26
  • 27. The magnitude of the balancing masses mL and mM in planes L and M may be obtained as discussed below : 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 27
  • 28. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 28
  • 29. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 29
  • 30. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 30
  • 31. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 31
  • 32. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 32
  • 33. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 33 in the clockwise direction from mass mA in the clockwise direction from mass mA
  • 34. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 34
  • 35. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 35
  • 36. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 36
  • 37. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 37
  • 38. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 38 It is assumed that the mass of pulley B acts in vertical direction. For the static balance of the pulleys, the centre of gravity of the system must lie on the axis of rotation. Therefore a force polygon must be a closed figure.
  • 39. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 39
  • 40. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 40
  • 41. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 41
  • 42. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 42
  • 43. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 43
  • 44. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 44
  • 45. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 45
  • 46. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 46
  • 47. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 47
  • 48. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 48
  • 49. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 49
  • 50. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 50
  • 51. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 51
  • 52. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 52
  • 53. 11/6/2014 Hareesha N G, Dept of Aero Engg, DSCE, Blore 53