Mrt IM Rigid shaft bearing TLC ID Solutionsolution 1here giv
Solution
solution:
1)here given that gear ratio as
G=na/nb=Tb/Ta
Tb=number of teeth on gear b
Ta=number of teeth on gear a
G=1/3
2)here motor and first are mounted on rigid shaft hence it will not induced torsional vibration in system,hence whole inertia act on load shaft
3)hence inertia on load shaft at left end is
I1=Im+Ia+Ib/G^2
I1=Im+Ia+9Ib
and inertia on right side of shaft is
I2=Id/G^2=9Id
4)in this on load shaft this inertia acting and same torque from motor transfer to gear b hence resultant torque on system is Tr= (Tl-Tm)
5)stiffness of load shaft is given by
Kt2=Tr/m
m=angle turn by load shaft
Kt2=(Tl-Tm)/m
6)here degree of freedom of system is given by without torsion is
number of link=3
p1=lower pair=2 at beairing
p2=1 at gear contact
DOF=3(n-1)-2P1-P2=6-4-1=1
when torsion of shaft produces the system produces one more DOF and system resulatn DOF
DOF1=DOF+1=1+1=2
5)hence when opposite torque acting on two ends of shaft then it is two degree of freedom system
hence equation of motion is
for left end is
I1*m1\'\'+Kt2*m1=-Tm
in matrix form as
[Kt2-I1w1^2]m=Tm
for right end
I2*m2\'\'+Kt2m=Tl
in matrrix form
[Kt2-I2w2^2]m=Tl
8)here natural frequencies of system for 2 DOF system is as follows
w1^2*w2^2=.5{[(Kt1+Kt2)I2+Kt2*I1/I1*I2]+-[(Kt1+Kt2)I2+Kt2*I1/I1*I2]^2-4[(Kt1+Kt2)Kt2-Kt2^2/I1*i2]^.5]^.5}
on putting Kt1=0 and Kt2=[Tl-Tm/m]
we get finally
(w1*w2)^2=1.1834*[Tl-Tm/m][1/Id]
w1w2=0
9)where mode shape are given by
first mode shape
(m1/m2)1=[Kt2/(-I1w1^2+(Kt1+Kt2))]
(m1/m2)1=Kt2/-I1w1^2+Kt2
second mode shape
(m1/m2)2=Kt2/-I2w2^2+Kt2
10) if inertia of gear are consider the we have to consider three rotor system,with two rotor at end of shaft for motor,load and at gear position we have consider another rotor and it will vary natural frequency of system and node shape


