bearings and fluid-induced instability in rotordynamics
DESCRIPTION
Bearings and Fluid-Induced Instability in Rotordynamics. Dr. Mehmet Sunar ME 562. Fluid Induced Instabilities. Fluid induced Instability is self-excited vibrations induced by internal mechanism that transfers rotational energy into the shaft as lateral vibrations. - PowerPoint PPT PresentationTRANSCRIPT
Bearings and Fluid-Induced Instability in Rotordynamics
Dr. Mehmet Sunar
ME 562
Fluid Induced Instabilities
Fluid induced Instability is self-excited vibrations induced by internal mechanism that transfers rotational energy into the shaft as lateral vibrations.
Properties of fluid induced instability
Created and controlled by fluid flow around the rotor.
Self excited. Non synchronous. Considered more destructive in fatigue view
point.
Categories of fluid induced instability
Fluid Induced Instability
Lube OilProcess Fluid
(Pumps or Compressors)Cooling Fluids
(like air in turbines)
Areas to control Fluid Induced Instability
Possible Areas
Bearing Rotor
Design Lube Oil
Flow rate
Viscosity
Preload
Clearance
Bearing type
Mathematical complexity due non-linearities in the bearing properties. Specially, in post instability conditions.
Modeling of bearing mechanical properties. Transient rotor response changes the fluid film bearing properties.
•Average Circumferential Velocity Ratio.
•Complex Dynamic Stiffness.
Fluid average circumferential velocity ratioIt is the ratio of average
fluid velocity to the average rotor velocity
Lambda ( λ )= ū/ω
Eccentricity (e)
It is the distance from the center of bearing to the center of rotor.
Ratio=e/c. Sometimes
called radial deflection.
e
Effect of eccentricity on stability in fluid film bearings
Higher eccentricity leads to lower fluid average velocity.
Lower fluid average velocity leads to better stability.
Bearing Stiffness
Higher eccentricity leads to higher stiffness.
Higher stiffness leads to better stability.
Complex dynamic stiffness
Total stiffness of fluid film bearings is considered to be complex and dynamic. Real part is called direct stiffness Imaginary part is called quadrature stiffness. KT=KD+jKQ
KT=[KS-Mrω2]+j[ω(DS+D)-λDΩ]
Dynamic since it is speed dependant.
Threshold of instability
The speed at which fluid induced instability commences. (e.g. 1900 rpm)
Two types of Fluid Induced Instabilities
Whirl. Forward precession. Usually starts earlier. Frequency holds a
constant order of rotor speed. (dependent on rotor speed)
Whip. Forward precession. Starts after whirl dies.
(it may exist without being preceded by whirl)
Frequency holds constant value (independent on rotor speed).
Fluid Induced Instability
Stable
Whip
Whirl
Orbit= 2D shaft vibration
FII Vibration symptoms:
* Large Amplitude * Subsynchronous
* Circular Orbit * Forward Precession
Experimental Setup
Experiments have been carried out at KFUPM MED Advanced Mechanics Lab.
Setup consists of Bently Nevada rotor kit with fluid film bearing
option. Speed controller. Oil pump. Vibration pickups and ADRE software.
Rotor kit
Fluid film bearing
Speed controller
Oil pump
Effect of fluid wedge support CCW rotation
Effect of fluid wedge support CW rotation
Typical experimental test results:
Vibration spectrum
Shaft average centerline, clearance circle and average eccentricity ratio. Gradual concentricity.
Zoomed run-up cascade. Instability threshold and frequency.
Threshold of instability change with oil pressure during start up
0
2150 2250
1620
2070
2500
0
500
1000
1500
2000
2500
3000
0.6 0.8 1 1.2 1.4 1.6
Pressure (psi)
Speed
(rp
m)
0
200
400
600
800
1000
1200
1400
1600
1800
2000
0.6 0.8 1 1.2 1.4 1.6
Pressure (psi)
Speed
(rp
m)
Threshold of instability change with oil pressure during shutdown
How oil behaves at the threshold of instability
1. Disk Location (A)
2. Shaft Length (B)
3. Disk Unbalance (Unb)
Unbalance effect (as function of rpm).
-9.3
-9.2
-9.1
-9
-8.9
-8.8
-8.7
-8.6
-8.5
0 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000
C0930001
C0930101
C0930201
Unb=2g
Unb=0g
Conclusions from experimental work
Higher flow rate of lubricating oil should raise the threshold of instability.
The unbalance has effect on instability.
THERORITICAL WORK
System response at P=0.6 psi at 1800 rpm
Displacement Transient Response
-15
-10
-5
0
5
10
15
0 0.5 1 1.5 2
Time, sec
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 0.6 psi at 1800 rpmStn (2): Fluid Film Bearing
Displacement Transient Response
-15
-10
-5
0
5
10
15
-15 -5 5 15 25 35
D(2)x, mils
D(2
)y, m
ils
D(2)x
Pressure is 0.6 psi at 1800 rpmStn (2): Fluid Film Bearing
System response at P=0.6 psi at 1800 rpm (Cont’d)
Displacement Transient Response
0
1
2
3
4
5
6
7
0 50 100 150 200
Frequency, Hz
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 0.6 psi at 1800 rpmStn (2): Fluid Film Bearing
System response at P=0.6 psi at 1800 rpm (Cont’d)
F=30 Hz=1800 cpm
F=11.72 Hz=703 cpm
Displacement Transient Response
-4
-3
-2
-1
0
1
2
3
4
0 0.5 1 1.5 2
Time, sec
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 0.6 psi at 1700 rpmStn (2): Fluid Film Bearing
System response at P=0.6 psi at 1700 rpm
Displacement Transient Response
-4
-3
-2
-1
0
1
2
3
4
-4 -2 0 2 4 6 8 10
D(2)x, mils
D(2
)y, m
ils
D(2)x
Pressure is 0.6 psi at 1700 rpmStn (2): Fluid Film Bearing
System response at P=0.6 psi at 1700 rpm (Cont’d)
System response at P=1.2 psi at 2300 rpm
Displacement Transient Response
-10
-8
-6
-4
-2
0
2
4
6
8
10
0 0.5 1 1.5 2 2.5 3 3.5
Time, sec
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 1.2 psi at 2300 rpmStn (2): Fluid Film Bearing
System response at P=1.2 psi at 2300 rpm (Cont’d)
Displacement Transient Response
-10
-5
0
5
10
-8 -3 2 7 12 17 22 27
D(2)x, mils
D(2
)y, m
ils
D(2)x
Pressure is 1.2 psi at 2300 rpmStn (2): Fluid Film Bearing
System response at P=1.2 psi at 2300 rpm (Cont’d)
Displacement Transient Response
0
0.5
1
1.5
2
2.5
3
3.5
4
4.5
0 50 100 150 200
Frequency, Hz
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 1.2 psi at 2300 rpmStn (2): Fluid Film Bearing
F=38.4 Hz=2300 cpm
F=13.67 Hz=820 cpm
System response at P=1.2 psi at 2200 rpm
Displacement Transient Response
-4
-3
-2
-1
0
1
2
3
4
0 0.5 1 1.5 2 2.5 3 3.5
Time, sec
Dis
pla
cem
ent,
mils
D(2)x
D(2)y
Pressure is 1.2 psi at 2200Stn (2): Fluid Film Bearing
System response at P=1.2 psi at 2200 rpm (Cont’d)
Displacement Transient Response
-4
-3
-2
-1
0
1
2
3
4
-4 -2 0 2 4 6 8 10
D(2)x, mils
D(2
)y, m
ils
D(2)x
Pressure is 1.2 psi at 2200Stn (2): Fluid Film Bearing
Conclusions from theoretical work
Effect of Viscosity on the stability is expected. Higher bearing pressure leads to higher
threshold of instability.