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MAURBHANJ SCHOOL OF ENGINEERINGBARIPADA : 757107 , ODISHA

Branch : Mechanical Engineering

Semester : 4th Sem

Subject : THEORY OF MACHINE

Topic : BALANCING OF MACHINE PARTS

Faculty : Er. Malabika Nayak

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Balancing

"is the process of attempting to improve the mass distribution

of a body so that it rotates in its bearings without unbalanced centrifugal forces”

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WHAT IS BALANCING OF ROTATING MEMBERS?�

Balancing means a process of restoring a rotor which has unbalance to a balanced state by adjusting the mass distribution of the rotor about its axis of rotation

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      • Mass balancing is routine for rotating machines,some reciprocating machines and vehicles
      • Mass balancing is necessary for quiet operation, high speeds , long bearing life, operator comfort, controls free of malfunctioning, or a "quality" feel

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• Pulley & gear shaft assemblies

• Starter armatures

• Airspace

components

• High speed machine

tool spindles

• flywheels

• Impellers

• Centrifuge rotors

• Electric motor rotors

• Fan and blowers

• Compressor rotors

• Turbochargers

• Precision shafts

  •  crank shafts
  •  Grinding wheels

• Steam & GasTurbine

rotors

Rotating components for balancing

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Unbalanced force on the bearing –rotor system

Bearing 1

Bearing 2

Shaft with

rotors

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      • Unbalance is caused by the displacement of the mass centerline from the axis of rotation.
      • Centrifugal force of "heavy" point of a rotor exceeds the centrifugal force exerted by the light side of the rotor and pulls the entire rotor in the direction of the heavy point.
      • Balancing is the correction of this phenomena by the removal or addition of mass

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BENEFITS OF BALANCING

    • Increase quality of operation.
    • Minimize vibration.
    • Minimize audible and signal noises.
    • Minimize structural fatigue stresses.
    • Minimize operator annoyance and fatigue.
    • Increase bearing life.
    • Minimize power loss.

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Rotating a rotor which has unbalance

causes the following problems.�

      • The whole machine vibrates.

      • Noise occurs due to vibration of

the whole machine.

      • Abrasion of bearings may shorten

the life of the machine.�

NEED FOR BALANCING

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Rotating Unbalance occurs due to the following reasons.

� ● The shape of the rotor is unsymmetrical.�� ● Un symmetrical exists due to a

machining error. � ● The material is not uniform, especially in

Castings.

● A deformation exists due to a distortion.

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An eccentricity exists due to a gap of fitting.� ● An eccentricity exists in the inner ring of

rolling bearing.

Non-uniformity exists in either keys or key

seats.

● Non-uniformity exists in the mass of flange

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  • Unbalance due to

unequal distribution

of masses

  • Unbalance due to

unequal distance of masses

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. Types of Unbalance Static Unbalance Dynamic Unbalance

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STATIC BALANCING

(SINGLE PLANE BALANCING)

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Single plane balancing

Adequate for rotors which are short in length,

such as pulleys and fans

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O2

m

r

ω

F = m r ω2

Magnitude of

unbalance

Vibration

occurs

Elasticity of the bearing

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θ1

θ2

θ3

m4r4 ω2

m1r1 ω2

m2r2 ω2

m3r3 ω2

Balancing of several masses

revolving in the same plane using a

Single balancing mass

bearing

m b

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m1r1 ω2

m2r2 ω2

m3r3 ω2

m4r4 ω2

m b r b ω2

θb

Graphical method of determination

magnitude and

Angular position of the balancing mass

Force vector polygon

O

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m1r1 ω2 cos θ1+ m2r2 ω2 cos θ 2

+ m3r3 ω2cos θ 3+ m4r4 ω2 cos θ 4

= mb cos θb

m1r1 ω2 sin θ1+ m2r2 ω2 sin θ 2

+ m3r3 ω2sin θ 3+ m4r4 ω2 sin θ 4

= mb sin θb

magnitude ‘m b and position ‘θb can be determined

by solving the above two equations.

Determination of magnitude and

Angular position of the balancing mass

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Dynamic or "Dual-Plane" balancing

Dynamic balancing is required for components such as shafts and multi-rotor assemblies.

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m r ω2

m r ω2

l

Brg A

Brg B

Statically balanced

but dynamically unbalanced

Load on each support Brg

due to unbalance = (m r ω2 l)/ L

r

r

Dynamic or "Dual-Plane" balancing

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On an arbitrary plane C

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Several masses revolving in different planes

Apply dynamic couple on the rotating shaft

Dynamic unbalance

ω

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Balancing of several masses rotating in different planes

F a

F b

F c

F d

A

B

C

D

L

M

End view

ω

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Plane

Mass

M

( kg)

Radius r

(cm)

Force / ω2,

M r =F ,

(kg. cm)

Dist. From ref plane

l , (cm)

Couple / ω2

M r l = C

(kg cm 2)

A

Ma

ra

Mara

-la

-Mara la

L

(Ref.plane)

Ml

rl

Ml rl

0

0

B

Mb

rb

Mbrb

lb

Mbrb lb

C

Mc

rc

Mcrc

lc

Mcrc lc

M

Mm

rm

Mmrm

d

Mmrmd

D

Md

rd

Mdrd

ld

Mdrdld

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la

lb

lc

ld

d

A

B

C

D

L,

Ref plane

M

Fc

Fb

Fa

Fd

Fm

F l

End view

side view of the planes

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Fc

Fb

Fa

Fd

Fm =?

F l =?

Couple polygon

force polygon

Ca

Cc

Cd

Cb

Cm=Mmrmd

Fa

Fb

Fc

Fd

Fm

Fl=Ml rl

From couple polygon, by measurement, Cm = Mm X r m X d

From force polygon, by measurement, Fl = Ml X rl

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A shaft carries four masses in parallel planes A,B,C,&D in this order. The masses at B & C are 18 kg & 12.5 kg respectively and each has an eccentricity of 6 cm. The masses at A & D have an eccentricity of 8 cm. The angle between the masses at B & C is 100 o and that between B & A is 190o both angles measured in the same sense. The axial dist. between planes A & B is 10cm and that between B & C is 20 cm. If the shaft is complete dynamic balance,

Determine,

1 masses at A & D

2. Distance between plane C &D

3. The angular position of the mass at D

Example :

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Plane

Mass

M

kg

Radius r

cm

Force / ω2,

M r ,

kg. cm

Dist. From ref plane

l , cm

Couple / ω2

M r l

kg cm 2

A

Ma=?

8

8 Ma

0

0

B

18

6

108

10

1080

C

12.5

6

75

30

2250

D

Md=?

8

8 Md

ld=?

8 Md ld

A

B

C

D

10 cm

20 cm

l d

18 kg

12.5 kg

M a

θ =190 o

θ =100o

End view

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A

B

C

D

10 cm

20 cm

l d

18 kg

12.5 kg

M a

θ =190 o

θ =100o

O

1080

2,250

8 Md ld= 2312 kg cm 2

O

108

75

8 Md =63.5 kg. cm

8 Ma = 78 kg .cm

Couple polygon

force polygon

θd= 203o

M d

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From the couple polygon,

By measurement, 8 Md ld= 2,312 kg cm 2

Md ld = 2312 / 8 = 289 kg cm

θd= 203o

From force polygon,

By measurement, 8 Md = 63.5 kg cm

8 Ma = 78.0 kg cm

Md = 7.94 kg

Ma = 9.75 kg

ld = 289 /7.94 = 36.4 cm