Vibration due to Air gap eccentricity

INVESTIGATION ON STATOR AND ROTOR VIBRATION CHARACTERISTICS OFTURBO-GENERATOR UNDER AIR GAP ECCENTRICITY FAULT

Shuting Wan, Yuling HeDepartment of Mechanical Engineering, North China Electric Power University, Baoding 071003, China

E-mail: [email protected]

Received July 2010, Accepted March 2011

No. 10-CSME-48, E.I.C. Accession 3211

ABSTRACTThis paper investigates the stator and the rotor vibration characteristics of turbo-generator

under the air gap eccentricity fault. Firstly the air gap magnetic flux density of the fault isdeduced, and the formula of the magnetic pull per unit area acting on the stator and theunbalanced magnetic pulls of x-axis and y-axis acting on the rotor are respectively gotten. Thenthe static eccentricity, the dynamic eccentricity and the mixed eccentricity are respectivelystudied to analyze the stator and the rotor vibration characteristics. Finally experiments aredone on a SDF-9 non-salient fault simulating generator to verify the theoretical results. Theinvestigation results of this paper will be beneficial to the air gap eccentricity fault diagnosis ofturbo-generator.

Keywords: turbo-generator; air-gap eccentricity; vibration characteristics; stator; rotor.

ETUDE SUR LES CARACTERISTIQUES DES VIBRATIONS DU STATOR ET DUROTOR DUN TURBOGENERATEUR COMPORTANT UN DEFAUT

DEXCENTRICITE DE LENTREFER

Cette etude porte sur les caracteristiques des vibrations du stator et du rotor dunturbogenerateur comportant un defaut dexcentricite de lentrefer. En premier lieu, ladetermination de la densite du flux magnetique de lentrefer, et la formule dattractionmagnetique par unite de surface agissant sur le stator et sur le desequilibre de lattractionmagnetique de laxe x et laxe y agissant sur le rotor, sont respectivement obtenues. Ensuite, lesexcentricites statiques, dynamiques et mixtes sont etudiees pour analyser les caracteristiques desvibrations du stator et du rotor. Finalement, des experiences sont menees sur un SDF-9, unesimulation de generateur a` defaut non-saillant pour verifier les resultats theoriques. Cesresultats seront benefiques pour le diagnostic du defaut dexcentricite de lentrefer duturbogenerateur.

Mots-cles : turbogenerateur; excentricite de lentrefer; caracteristiques des vibrations; stator;rotor.

Transactions of the Canadian Society for Mechanical Engineering, Vol. 35, No. 2, 2011 161

1. INTRODUCTION

Air gap eccentricity is one of the main mechanical faults, which could exist in almost everygenerator. This fault can cause the magnetic pull per unit area acting on the stator and theunbalanced magnetic pull (UMP) acting on the rotor, which can deteriorate the bearingworking condition, increase the stator and rotor vibration, and deform the stator core anddamage the winding insulation. Thus, investigation of the UMP characteristics and thevibration characteristics of the stator and the rotor will be beneficial to the air gap eccentricityfault diagnosis of turbo-generator.

The UMP on the rotor caused by the air gap eccentricity was studied by many authors [115],among these papers, most of them are about motors [14]. For turbo-generator, the diagnosis,causes, and preventive maintenance for the air gap eccentricity fault were investigated firstly byL. T. Rosenberg [5]. Then the simulation and modeling of this fault were presented [6,7]. Thefinite element method and the modified winding function method have been used as powerfultools to calculate the electrical parameters and the magnetic fields [8]. Meanwhile, the UMP onthe rotor caused by the air gap eccentricity fault and the radial vibration characteristics werestudied [914]. Besides the radial vibration, the axial vibration also exists [15].

The current researches have presented important findings and they are the basis of the on-lineand the off-line detecting the air gap eccentricity fault. However, these researchers have paidattention to the rotor vibration characteristics caused by the UMP, and the stator vibrationcharacteristics are rarely studied. Actually, the stator vibration characteristics have largequantity of fault information, and they can also be used to diagnose generator faults and

NOMENCLATURE

f magnetomotive force (A), andfrequency (Hz)

t time(s)F value of magnetomotive forces

(A), and unbalanced magneticpull (N)

I vector of stator currentE0 vector of stator electromotive

forceF vector of magnetomotive forcesg radial length of the air

gap (mm)q magnetic pull per unit area

(N/m2)B magnetic flux density (Wb/m2)L axial length of the air gap (m)R radius of the rotor (m)Greek symbols

a circumferential angle (rad)v angular frequency (rad/s)

y internal power-angle of gen-erator (rad)

b angle between magnetomotiveforces (rad)

d relative air gap eccentricityL magnetic permeance (H)m0 magnetic permeability of the

air (H/m)

Subscriptss denotes static eccentricity or

statord denotes dynamic eccentricityr denotes mechanical rotation or

rotorm denotes mechanical parametera denotes average parameterc denotes composite parameter0 denotes constant parameterX denotes components in X

directionY denotes components in Y

direction


sometimes may even be more effective. Based on these researches, this paper intends to studythe magnetic pull per unit area acting on the stator and the UMP acting on the rotor, and theninvestigate the vibration characteristics of the stator and the rotor caused by the air gapeccentricity fault.

2. AIR GAP MAGNETIC FLUX DENSITY UNDER NORMAL CONDITION AND AIRGAP ECCENTRICITY FAULT

Under normal condition without air gap eccentricity, and assuming that the air gap magneticflux distribution is symmetrical, the air gap magnetic permeance per unit area can be expressedas

L~m0g

1

The air gap magnetomotive forces under normal condition are shown in Fig. 1, where Fr isthe main magnetomotive force, Fs is the magnetomotive force produced by the armaturereaction, and Fc is the composite magnetomotive force. The phasors indicated by a dot in Fig. 1are time vectors, while the phasors indicated by a bar are space vectors. Considering the effectof the air gap location on the magnetomotive force, a mechanical angle written as am is used,and the air gap magnetomotive forces can be expressed as

f am,t ~Fs cos vt{am{y{ p2

zFr cos vt{am ~Fc cos vt{am{b 2

where: v52pf, v is the electrical angular frequency, f is the electrical frequency, and am is anangle used to indicate the circumferential location of the air gap. Then Fc and b can becalculated as

Fc~

F2s cos

2yz Fr{Fs siny 2q

b~arctgFs cosy

Fr{Fs siny

8>: 3

According to Eqs. (1) and (2), the magnetic flux density under normal condition can beexpressed as

Fig. 1. Air gap magnetomotive forces under normal condition.


B am,t ~f am,t L~Fc cos vt{am{b m0g

4

When the air gap eccentricity fault happens, the air gap length g is not constant because ofthe air gap eccentricity, and the magnetic permeance will be changed while the magnetomotiveforces will keep stable. For convenience, the coordinate system shown in Fig. 2 is adopted. Theline through the minimum air gap of the static eccentricity is defined as the x-axis. Meanwhile, itis also defined as the original point of the angle am. The air gap length can be expressed as

g am,t ~ga{ds cosam{dd cos vrt{am ~ga 1{drs cosam{drd cos vrt{am 5

where ga is the average air gap length which generally equals to g, ds is the static eccentricitylength, dd is the dynamic eccentricity length, drs5ds/ga is the value of the relatively staticeccentricity, drd5dd/ga is the value of the relatively dynamic eccentricity, and vr52pfr, vr is themechanical angular frequency, fr is the mechanical frequency. For turbo-generator, vr equals tothe electrical angular frequency v. In the following text, all angular frequency is written as v,and fr is written as f.

The magnetic permeance per unit area can be expanded by power series, and the higherharmonic components can be ignored because of their tiny values. Then the magneticpermeance per unit area is

L am,t ~ m0g am,t ~

m0ga 1{ drs cosamzdrd cos vrt{am

~L0 1zdrs cosamzdrd cos vt{am z drs cosamzdrd cos vrt{am 2

2!z

" #

&L0 1zdrs cosamzdrd cos vt{am ~L0zLs cosamzLd cos vt{am

6

where L0 is the constant component of the air gap magnetic permeance, Ls5L0drs is thecomponent caused by the static eccentricity, and Ld5L0drd is the component caused by thedynamic eccentricity.

According to Eqs. (2) and (6), the magnetic flux density under the air gap eccentricity faultcan be expressed as

Fig. 2. Coordinate system set for air gap eccentricity.


B am,t ~f am,t L am,t ~Fc cos vt{am{b L0zLs cosamzLd cos vt{am 7

3. MAGNETIC PULL OF PER UNIT AREA

According to Eq. (4), the magnetic pull per unit area under normal condition can beexpressed as

q am,t ~ B am,t 2

2m0~

Fc cos vt{am{b m0=g 22m0

~m0Fc

2

4g21zcos 2vt{2am{2b

~Fc

2L02

4m01zcos 2vt{2am{2b

8

detailed information about the amplitudes is shown in Table 1.

According to Eqs. (3) and (7), the magnetic pull per unit area under the air gap eccentricityfault can be derived as

q am,t ~ B am,t 2

2m0~

F2C8m0

2L20zL2szL

2d

z 4L0Ls cosam z L2s cos2am

zL2d2cos 2b

!z 2LsLd cosvt z 4L0Ld cos vt{am z 2LsLd cos vt{2am

z LsLd cos vt{2b z 2L0Ld vt{am{2b z LsLd cos vt{2am{2b

z L2d cos 2vt{2am zL2s2cos 2vt{2b

" #z 2L0Ls cos 2vt{am{2b

z 2L20zL2szL

2d

cos 2vt{2am{2b

z 2L0Ls cos 2vt{3am{2b

zL2s2cos 2vt{4am{2b

" #z LsLd cos 3vt{2am{2b

z 2L0Ld cos 3vt{3am{2b z LsLd cos 3vt{4am{2b

zL2d2cos 4vt{4am{2b

" #g

9

Table 1. Amplitude of the magnetic pull per unit area on stator under normal condition.

Components Amplitude formula Essentially influential factors

Constant Fc2L0

2/4m0 y, If , and gPulsating (2f) Fc

2L02/4m0 y, If , and g


4. STATOR VIBRATION CHARACTERISTICS UNDER NORMAL CONDITIONAND AIR GAP ECCENTRICITY FAULT

The stator core is made up of lots of overlapped silicon sheets, and its mechanical modelis a hollow elastic shell cylinder. The essentially influential factor for the stator vibrationcharacteristics is the pulsating peculiarity of the magnetic pull acting on the stator. Therefore,the stator vibration characteristics can be studied via the magnetic pull per unit area.

According to Eq. (8), the pulsating peculiarity of the magnetic pull acting on the stator undernormal condition can be gained. The amplitude of the magnetic pull of 2f is

q2f~m0F

2c

4g2~

F2cL20

4m010

which will cause the stator vibration at 2f.

When the air gap eccentricity fault happens, the magnetic pull acting on the stator will havedifferent formulas due to different eccentricity types. There are three types of eccentricities, i.e.static eccentricity, dynamic eccentricity, and mixed eccentricity composed by the previous two.Based on Eq. (9), the further analysis of the stator vibration characteristics under the faults isgiven as follows.

4.1 Static Eccentricity FaultIn this case, Ld50, Ls?0, then Eq. (9) can be simplified as

q am,t ~ F2C

8m02L20zL

2sz4L0Ls cosamzL

2s cos2amz

L2s2cos 2vt{2b

"

z2L0Ls cos 2vt{am{2b z 2L20zL2s

cos 2vt{2am{2b

z2L0Ls cos 2vt{3am{2b zL2s

2cos 2vt{4am{2b

# 11

As seen in Eq. (11), there are constant components and pulsating components of 2f, and theamplitudes of the magnetic pull per unit area on stator and the essentially influential factors areshown in Table 2. The constant components do not cause the stator vibration, while thepulsating components cause the stator vibration at 2f.

Table 2. Amplitude of the magnetic pull per unit area on stator under static eccentricity fault.


Constant Fc2(2L0

2+Ls2+4L0Lscosam+Ls2cos2am)/8m0 y, If, ga, ds and ampulsating (2f) Fc

2 (2Ls2+2L02+4L0Ls)/8m0 y, If, ga and ds


The amplitude of the magnetic pull of 2f is

q2f0~

F2c 2L2sz2L

20z4L0Ls

8m0

12

Comparing Eq. (10) with Eq. (12), it is obvious that the amplitude of the magnetic pull of 2funder the static eccentricity fault is larger than that under normal condition, and the statorvibration at 2f under the static eccentricity fault will be obviously larger than that under normalcondition. As indicated in Eq. (3), the internal power-angle y affects FC and b. FC determinesthe amplitude of the stator vibration while b and am only affect the vibration amplitude whenthe excitation begins, more details are shown in Table 2, where the exciting current If affects FC,ga determines L0, and ds determines Ls.

4.2 Dynamic Eccentricity FaultIn this case, Ld?0, Ls50, then Eq. (9) can be simplified as

q am,t ~FC2

8m02L0

2zLd2z

Ld2

2cos 2bz4L0Ld cos vt{am z2L0Ld vt{am{2b

"

zLd2 cos 2vt{2am z 2L02zLd2

cos 2vt{2am{2b

z2L0Ld cos 3vt{3am{2b zLd2

2cos 4vt{4am{2b

# 13

As seen in Eq. (13), there are constant components and pulsating components of f, 2f, 3f and4f, and the amplitudes of the magnetic pull per unit area on stator and the essentially influentialfactors are shown in Table 3. The constant components do not cause the stator vibration, whilethe pulsating components cause the stator vibration at f, 2f, 3f and 4f. Moreover, comparing themagnetic pull amplitudes in Table 3 with those in Table 1, it is obvious that the amplitude ofeach frequency under the dynamic eccentricity fault is larger than that under normal condition,and the vibration amplitude of the stator will increase as the dynamic eccentricity increases. Theangle b influenced by y affects the amplitude of the constant components. Besides, b and amdetermines the initial vibration amplitude when the excitation begins.

Table 3. Amplitude of the magnetic pull per unit area on stator under dynamic eccentricity fault.


Constant Fc2(2L0

2+Ld2+0.5Ld2cosb)/8m0 y, If, ga and ddpulsating f Fc

2(6L0Ld)/8m0 y, If, ga and dd2f Fc

2(2L02+2Ld2)/8m0 y, If, ga and dd

3f Fc2(2L0Ld)/8m0 y, If, ga and dd

4f, Fc2(0.5Ld

2)/8m0 y, If, ga and dd


4.3 Mixed Eccentricity FaultIn this case, Ls?0, Ld?0. then Eq. (9) is the magnetic pull per unit area acting on the stator.

As seen in Eq. (9), the magnetic pull per unit area has constant components and pulsatingcomponents of f, 2f, 3f and 4f , and the amplitudes of the magnetic pull per unit area on statorand the essentially influential factors are shown in Table 4. The constant components do notcause the stator vibration, while the pulsating components cause the stator vibration at f, 2f, 3fand 4f. Moreover, comparing the magnetic pull amplitudes in Table 4 with those in Table 1, it isobvious that the amplitude of each frequency under the mixed eccentricity fault is larger thanthat under normal condition, and the vibration amplitude of the stator will increase as theeccentricity no matter static or dynamic increases. b and am affect the vibration amplitude whenthe excitation begins, while y, If, ds and dd determine the vibration amplitude on the wholeoperating process.

Based on the previous analysis, a general conclusion can be gained: the static eccentricityfault can cause the stator vibration at 2f, and the dynamic eccentricity and the mixedeccentricity can cause the stator vibrations at f, 2f, 3f and 4f. The exciting current and theinternal power-angle which depends on the load nature of the generator directly determine thevibration amplitude. Besides, the vibration amplitude will also increase as the eccentricityincreases.

These forced vibrations may deform the stator core and damage the windings insulation.Moreover, the bars of the stator end winding may even have abruptions if the vibrationfrequency is similar to the bars natural frequency.

5. ROTOR VIBRATION CHARACTERISTICS UNDER NORMAL CONDITION ANDAIR GAP ECCENTRICITY FAULT

The mechanical model of the rotor is a stuffed cylinder. The unit magnetic pull is not enoughto cause rotor vibrate because of its large rigidity. The essentially influential factor for the rotorvibration characteristics is the unbalanced magnetic pull (UMP). And the UMP of x-axis and y-axis can be calculated as follows

FX~LR 2p0

q am,t cos amdamFY~LR

2p0

q am,t sin amdamF~

FX

2zFY2

p8>>>: 14

where F is the composite UMP, FX and FY are respectively its components in x-axis and y-axis.

Table 4. Amplitude of the magnetic pull per unit area on stator under mixed eccentricity fault.


ConstantFc

2(2L02+Ls2+Ld2+4L0Lscosam

+Ls2cos2am +0.5Ld2cosb)/8m0 y, If, ga, am, ds and ddpulsating f Fc

2(6L0Ld +6LsLd)/8m0 y, If, ga, ds and dd2f Fc

2(2L02+2Ld2+2Ls2+4L0Ls)/8m0 y, If, ga, ds and dd

3f Fc2(2L0Ld+2LsLd)/8m0 y, If, ga, ds and dd

4f Fc2(0.5Ld

2)/8m0 y, If, ga and dd


According to Eqs. (8) and (14), the UMP under normal condition can be gained, which isF5FX5FY50. Thus, the rotor does not vibrate in theory. However, the situation will bedifferent if the air gap eccentricity fault happens.

According to Eqs. (9) and (14), The UMP under the air gap eccentricity fault can be derivedas

FX~LRF 2Cp

4m02L0Lsz2L0Ld cosvtzL0Ld cos vt{2b zL0Ls cos 2vt{2b

FY~LRF 2Cp

4m02L0Ld sinvtzL0Ld sin vt{2b zL0Lssin 2vt{2b

F~LRFC

2pL04m0

5Ls

2z5Ld2z4Ld

2 cos2bz10LdLs cosvt

z8LdLs cos vt{2b z4Ls2cos 2vt{2b

s

8>>>>>>>>>>>>>>>>>:

15

Based on Eq. (15), the further analysis of the rotor vibration characteristics under the air gapeccentricity fault is given as follows.

5.1 Static Eccentricity FaultIn this case, Ld50, Ls?0, then Eq. (15) can be simplified as

FX~LRF2Cp2L0LszL0Ls cos 2vt{2b

4m0

FY~LRF2CpL0Ls sin 2vt{2b

4m0

F~5z4 cos 2vt{2b p LRFC2pL0Ls4m0

8>: 16

As seen in Eq. (16), the UMP consists of constant components and pulsating components of2f, and the amplitudes of UMP and the essentially influential factors are shown in Table 5. Theconstant components do not cause the rotor vibration, while the pulsating components causethe rotor vibration at 2f. Obviously, the rotor vibration amplitude will also increase as the staticeccentricity increases. The internal power-angle y affects FC and b so that the UMP no matterat the beginning of the excitation or on the running process will be influenced.

Since the air gap eccentricity direction under this fault is stationary, the UMP also keeps aconstant direction. Therefore, the eccentricity direction can be reflected by the UMP direction.Moreover, the static eccentricity causes can be further deduced, as shown in Fig. 3. It is easy to findthat the UMP direction is along the line that through the minimum air gap of the static eccentricity.

Table 5. Amplitude of the UMP on rotor under static eccentricity fault.


FX constant LRFc2p(2L0Ls)/4m0 y, If, ga, and ds

pulsating (2f) LRFc2pL0Ls/4m0 y, If, ga, and ds

FY constant 0 -pulsating (2f) LRFc

2pL0Ls/4m0 y, If, ga, and dsF constant

5

pLRFc

2pL0Ls/4m0 y, If, ga, and dspulsating (2f) 2 LRFc

2pL0Ls/4m0 y, If, ga, and ds


Both bearing offset and stator core deformation are probable to cause this appearance. The UMPdirection is the same as the bearing offset direction and the stator core deforming direction. Besides,a composite force composed of the UMP and the rotors gravity is produced, which also pulls therotor from a constant direction and worsens the bearing load condition. As the rotor rotates, thecomposite force will act on the rotors different circumferential positions.

5.2 Dynamic Eccentricity FaultIn this case, Ld?0,Ls50, then Eq. (15) can be simplified as

FX~LRF2Cp 2L0Ld cosvtzL0Ld cos vt{2b

4m0

FY~LRF2Cp 2L0Ld sinvtzL0Ld sin vt{2b

4m0

F~5z4 cos2b

pLRFC

2L0Ld

4m0

8>: 17

As seen in Eq. (17), the values of FX and FY will change as the rotor rotates while the value ofthe composite UMP will keep the same. However, since it is dynamic eccentricity, theeccentricity location of the air-gap and the composite UMPs direction will change as the rotorrotates. Thus, the dynamic eccentricity will cause the rotor vibration at f. The internal power-angle y affects FC and b, so that the UMP no matter at the beginning of the excitation or on the

Fig. 3. Static eccentricity causes reflected by the direction of the UMP, (a) Bearing offset, (b)Deformation of stator core.

Table 6. Amplitude of the UMP on rotor under dynamic eccentricity fault.

Components Amplitude formula

Essentially influential

factors

FX constant 0 -pulsating (f)

5{4 cos2b

pLRFC

2L0Ld

4m0 y, If, ga, and dd

FY constant 0 -pulsating (f)

5{4 cos2b

pLRFC

2L0Ld


F constant 0 -pulsating (f)

5z4 cos2b

pLRFC

2L0Ld



whole running process will be influenced. More details are shown in Table 6, where theamplitude formulas of FX and FY are gained through the vectorial resultant method.

Although the direction of the UMP changes as the rotor rotates, it acts on a certaincircumferential position of the rotor. The changing direction of the UMP reflects the dynamiceccentricity direction, and the dynamic eccentricity causes can be further deduced, as shown inFig. 4. Since the UMP has the same direction as the dynamic eccentricity, rotor flexuredeformation will be caused or worsened due to the continuous pull action. Moreover, rub-impact accident may even be caused after a long period.

5.3 Mixed Eccentricity FaultIn this case, Ls?0, Ld?0, then Eq. (15) is the formula of the UMP. As shown in Eq. (15), the

UMP will cause the rotor vibration at f and 2f, and the vibration amplitudes of the rotor willalso increase as the static eccentricity or the dynamic eccentricity increases. The initial vibrationamplitude is affected by y when the excitation begins. Besides, y and If affect the vibrationamplitudes on the whole process via FC. More details can be found in Table 7, where theamplitude formulas of FX, FY and F at f are deduced through the vectorial resultant method.

Table 7. Amplitude of the UMP on rotor under mixed eccentricity fault.

Components Amplitude formula

Essentially influen-

tial factors

FX constant LRFc2p(2L0Ls)/4m0 y, If, ga, and ds

pulsating f5{4 cos2b

p|LRFC

2L0Ld


2f LRFc2pL0Ls/4m0 y, If, ga, and ds

FY constant 0 -pulsating f

5{4 cos2b

p|LRFC

2L0Ld


2f LRFc2pL0Ls/4m0 y, If, ga, and ds

F constant5L2sz5L

2dz4L

2d cos2b

q|LRF2c pL0

4m0

y, If, ga, and dd

pulsating f 32LdLs

p|LRFC

2pL0

4m0 y, If, ga, ds, and dd

2f 2 LRFc2pL0Ls/4m0 y, If, ga, and ds

Fig. 4. Dynamic eccentricity causes reflected by the direction of the UMP, (a) Deflection of rotorroundness, (b) Flexure deformation of rotor.


Since the mixed eccentricity is composed of the static eccentricity and the dynamiceccentricity, the UMP can be also treated as a composite force composed of two componentforces. One component force that has a constant direction is caused by the static eccentricity,and the other one whose direction will change as the rotor rotates is caused by the dynamiceccentricity. The directions of the two component forces can also reflect the static eccentricitydirection and the dynamic eccentricity direction. And the eccentricity causes shown in Fig. 3and Fig. 4 can be also deduced. The effect of the UMP under mixed eccentricity fault equals tothe superposition of the static one and the dynamic one.

6. EXPERIMENT VERIFICATION

6.1 Experiment Equipment and MethodThe experiment is based on a SDF-9 non-salient pole fault simulating generator, as shown in

Fig. 5(a). The stator winding is two-layer and pitch-shortening, and the correspondingparameters are:

Fig. 5. SDF-9 non-salient fault simulating generator, (a) General outlook, (b) Method to set staticeccentricity.

Fig. 6. Method to set speed sensors.


Fig. 7. Stator vibration spectrum under normal condition and static eccentricity fault, (a) Normalcondition, (b) 25% static eccentricity, (c) 50% static eccentricity.


Fig. 8. Rotor vibration spectrum under normal condition and static eccentricity fault. (a) Normalcondition, (b) 25% static eccentricity, (c) 50% static eccentricity.


Rated capacity: 7.5kVA

Rated exciting current: 1.5A

Rated speed: nr53000 r/minNumber of pole-pairs: p51Radial length of air gap: 0.8 mm

The generator stator can be moved along the horizontally radial direction while the rotorkeeps stable. The movement can be performed by two bolts and controlled by two dialindicators so that the static eccentricity can be simulated, as shown in Fig. 5(b). A CD-21Sspeed sensor and a CD-21C speed sensor (both made by Beijing vibration measurer factory, thesensitivity is 30 mv/mm/s) are respectively set on the bearing block in the horizontal directionand the stator core in vertical direction, as shown in Fig. 6. U60116C collector made by BeijingBopu Co.,Ltd is used. The sampling frequency is 10 kHz. During the experiment, the generatoris operated under the rated condition.

6.2 Experimental Results and DiscussionsThe exciting current If51.5A, and 25% and 50% static eccentricity are set respectively, the

experiment results are shown in Fig. 7 and Fig. 8.

Under normal condition, the stator should only vibrate at 2f and the rotor shouldnt vibratein theory. However, the stator and the rotor vibrations at f, 2f exist in the experiment systemdue to the asymmetry inside the generator.

As shown in Fig. 7 and Fig. 8, the results show that the static air gap eccentricity faultgenerally increases the stator and the rotor vibration at 2f, and the experiment results complywith the theoretical analysis.

7. CONCLUSIONS

This paper investigates the stator and the rotor vibration characteristics under normalcondition and the air gap eccentricity fault, the experiment verifications are also provided. Theconclusions drawn from the theoretical and experimental investigation can be given as follows:

(1) The static eccentricity fault causes the stator and the rotor vibration at 2f, and the dynamiceccentricity fault and the mixed eccentricity fault cause the stator vibration at f, 2f, 3f, 4f ,and cause the rotor vibration at f and 2f.

(2) Under the air gap eccentricity fault, the vibration amplitude of the stator and the rotor willincrease as the eccentricity develops. And the eccentricity direction can be reflected by thedirection of the UMP.

(3) Under the air gap eccentricity fault, the stator and the rotor vibration amplitudes will beaffected by the value of the eccentricity, the internal power-angle of the generator and theexciting current.

The proposed vibration characteristics have significant value for the air gap eccentricity faultdiagnosis. However, the experiments of dynamic air gap eccentricity fault and mixed air gapeccentricity fault are still needed to be performed in future.

ACKNOWLEDGMENTS

This work is supported by Natural Science Foundation of Hebei province(E2011502024) andthe Fundamental Research Funds for the Central Universities (09MG30).


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Vibration due to Air gap eccentricity

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