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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front. Mech. Eng.    2022, Vol. 17 Issue (4) : 57    https://doi.org/10.1007/s11465-022-0713-3
RESEARCH ARTICLE
Gear fault diagnosis using gear meshing stiffness identified by gearbox housing vibration signals
Xiaoluo YU1, Yifan HUANGFU1, Yang YANG2, Minggang DU2, Qingbo HE1(), Zhike PENG1
1. State Key Laboratory of Mechanical System and Vibration, Shanghai Jiao Tong University, Shanghai 200240, China
2. Science and Technology on Vehicle Transmission Laboratory, China North Vehicle Research Institute, Beijing 100072, China
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Abstract

Gearbox fault diagnosis based on vibration sensing has drawn much attention for a long time. For highly integrated complicated mechanical systems, the intercoupling of structure transfer paths results in a great reduction or even change of signal characteristics during the process of original vibration transmission. Therefore, using gearbox housing vibration signal to identify gear meshing excitation signal is of great significance to eliminate the influence of structure transfer paths, but accompanied by huge scientific challenges. This paper establishes an analytical mathematical description of the whole transfer process from gear meshing excitation to housing vibration. The gear meshing stiffness (GMS) identification approach is proposed by using housing vibration signals for two stages of inversion based on the mathematical description. Specifically, the linear system equations of transfer path analysis are first inverted to identify the bearing dynamic forces. Then the dynamic differential equations are inverted to identify the GMS. Numerical simulation and experimental results demonstrate the proposed method can realize gear fault diagnosis better than the original housing vibration signal and has the potential to be generalized to other speeds and loads. Some interesting properties are discovered in the identified GMS spectra, and the results also validate the rationality of using meshing stiffness to describe the actual gear meshing process. The identified GMS has a clear physical meaning and is thus very useful for fault diagnosis of the complicated equipment.

Keywords gearbox fault diagnosis      meshing stiffness      identification      transfer path      signal processing     
Corresponding Author(s): Qingbo HE   
Just Accepted Date: 15 June 2022   Issue Date: 23 November 2022
 Cite this article:   
Xiaoluo YU,Yifan HUANGFU,Yang YANG, et al. Gear fault diagnosis using gear meshing stiffness identified by gearbox housing vibration signals[J]. Front. Mech. Eng., 2022, 17(4): 57.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-022-0713-3
https://academic.hep.com.cn/fme/EN/Y2022/V17/I4/57
Fig.1  Gearbox vibration modeling by combining dynamics and transfer path analysis.
Fig.2  Assembly method of the gear?shaft?bearing system matrix.
Fig.3  Flowchart of gear meshing stiffness identification with its application.
Fig.3  Flowchart of gear meshing stiffness identification with its application.
GearTeeth numberFace width/mmInner diameter/mmModuleShaft length/mm
Gear at driving shaft2516252.5405
Gear at driven shaft5816252.5405
Tab.1  Parameters of gears and shafts
GearTeeth numberFace width/mmInner diameter/mmModuleShaft length/mm
Gear at driving shaft2516252.5405
Gear at driven shaft5816252.5405
Tab.1  Parameters of gears and shafts
Fig.4  Simulated gear meshing stiffness (a) waveforms and (b) spectra of healthy and two typical gear faults.
Fig.4  Simulated gear meshing stiffness (a) waveforms and (b) spectra of healthy and two typical gear faults.
Fig.5  Simulated housing vibration response at two measuring points.
Fig.5  Simulated housing vibration response at two measuring points.
Fig.6  Identified bearing dynamic forces compared with theoretical ones.
Fig.6  Identified bearing dynamic forces compared with theoretical ones.
Fig.7  Identified gear meshing stiffness: (a) waveforms of healthy, pitting, and wear gear; and (b) spectra of healthy, pitting, and wear gear.
Fig.7  Identified gear meshing stiffness: (a) waveforms of healthy, pitting, and wear gear; and (b) spectra of healthy, pitting, and wear gear.
Case of combinationS2 for pittingSe for wear
Identified healthy GMS & basis healthy GMS0.35510.7748
Identified healthy GMS & basis fault GMS0.68321.0605
Identified fault GMS & basis healthy GMS0.65420.5202
Identified fault GMS & basis fault GMS0.33820.7121
Tab.2  Similarity index results of the simulation example under 600 r/min
Case of combinationS2 for pittingSe for wear
Identified healthy GMS & basis healthy GMS0.35510.7748
Identified healthy GMS & basis fault GMS0.68321.0605
Identified fault GMS & basis healthy GMS0.65420.5202
Identified fault GMS & basis fault GMS0.33820.7121
Tab.2  Similarity index results of the simulation example under 600 r/min
GearTooth numberMeshing frequency orderRotating frequency order
Gear on the driving shaft21211
Gear on the driven shaft82210.2561
Tab.3  Gear parameters of the single-stage gearbox test rig
GearTooth numberMeshing frequency orderRotating frequency order
Gear on the driving shaft21211
Gear on the driven shaft82210.2561
Tab.3  Gear parameters of the single-stage gearbox test rig
Fig.8  Gearbox test rig and different fault gears.
Fig.8  Gearbox test rig and different fault gears.
Fig.9  Decoupling frequency response functions (FRFs) test (take excitation at 1x as an example).
Fig.9  Decoupling frequency response functions (FRFs) test (take excitation at 1x as an example).
Fig.10  Spectra of the measured vibration signals for different fault types.
Fig.10  Spectra of the measured vibration signals for different fault types.
Fig.11  Spectra of the identified bearing dynamic forces in the experiment.
Fig.11  Spectra of the identified bearing dynamic forces in the experiment.
Fig.12  Dynamic modeling of the gear?shaft?bearing system of the test rig.
Fig.12  Dynamic modeling of the gear?shaft?bearing system of the test rig.
Fig.13  Identified gear meshing stiffness in the experiment: (a) waveforms of healthy, pitting, wear gear, (b) spectra of healthy, pitting, wear gear, and (c) fault characteristic frequency magnitude of healthy, pitting, wear gear.
Fig.13  Identified gear meshing stiffness in the experiment: (a) waveforms of healthy, pitting, wear gear, (b) spectra of healthy, pitting, wear gear, and (c) fault characteristic frequency magnitude of healthy, pitting, wear gear.
Fig.14  Comparison study of the proposed gear meshing stiffness identification and traditional fault diagnosis approach: (a) waveform and time?frequency distribution of the intrinsic mode function and (b) normalization RMS of different measuring points and the identified gear meshing stiffness (GMS).
Fig.14  Comparison study of the proposed gear meshing stiffness identification and traditional fault diagnosis approach: (a) waveform and time?frequency distribution of the intrinsic mode function and (b) normalization RMS of different measuring points and the identified gear meshing stiffness (GMS).
Fig.15  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy, wear, and pitting gear using (a) measuring points 2#?4# and (b) measuring points 3#?5#.
Fig.15  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy, wear, and pitting gear using (a) measuring points 2#?4# and (b) measuring points 3#?5#.
Fig.16  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy, wear, and pitting gear under another speed.
Fig.16  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy, wear, and pitting gear under another speed.
Conditions of vibration signals or GMSS2
Healthy housing vibration signal basisPitting housing vibration signal basisWear housing vibration signal basisHealthy GMS basisPitting GMS basisWear GMS basis
Healthy (2400 r/min)2.85522.92232.95566.09813.98265.9761
Pitting (2400 r/min)2.31201.47092.57076.69853.82856.0991
Wear (2400 r/min)2.36882.02412.80346.41005.99215.7597
Tab.4  Similarity index results under different speed using the housing vibration signals or the identified GMS under 1800 r/min and 9 N?m conditions as the basis
Conditions of vibration signals or GMSS2
Healthy housing vibration signal basisPitting housing vibration signal basisWear housing vibration signal basisHealthy GMS basisPitting GMS basisWear GMS basis
Healthy (2400 r/min)2.85522.92232.95566.09813.98265.9761
Pitting (2400 r/min)2.31201.47092.57076.69853.82856.0991
Wear (2400 r/min)2.36882.02412.80346.41005.99215.7597
Tab.4  Similarity index results under different speed using the housing vibration signals or the identified GMS under 1800 r/min and 9 N?m conditions as the basis
Fig.17  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy and pitting gear under another load.
Fig.17  Identified gear meshing stiffness in the experiment: fault characteristic frequency magnitude of healthy and pitting gear under another load.
Conditions of vibration signals or GMSS2
Healthy housing vibration signal basisPitting housing vibration signal basisHealthy GMS basisPitting GMS basis
Healthy (T = 3 N?m)2.54242.48646.31554.0944
Pitting (T = 3 N?m)2.37111.95536.49633.9728
Tab.5  Similarity index results under different load using the housing vibration signals or the identified GMS under 1800 r/min and 9 N?m conditions as the basis
Conditions of vibration signals or GMSS2
Healthy housing vibration signal basisPitting housing vibration signal basisHealthy GMS basisPitting GMS basis
Healthy (T = 3 N?m)2.54242.48646.31554.0944
Pitting (T = 3 N?m)2.37111.95536.49633.9728
Tab.5  Similarity index results under different load using the housing vibration signals or the identified GMS under 1800 r/min and 9 N?m conditions as the basis
Fig.18  Spectrum noise level of the identified gear meshing stiffness indicates gear fault severity. Cond1: measuring points 1#?3#, 1800 r/min, and 9 N?m; Cond2: measuring points 2#?4#, 1800 r/min, and 9 N?m; Cond3: measuring points 3#?5#, 1800 r/min, and 9 N?m; Cond4: measuring points 1#?3#, 2400 r/min, and 9 N?m; Cond5: measuring points 1#?3#, 1800 r/min, and 3 N?m.
Fig.18  Spectrum noise level of the identified gear meshing stiffness indicates gear fault severity. Cond1: measuring points 1#?3#, 1800 r/min, and 9 N?m; Cond2: measuring points 2#?4#, 1800 r/min, and 9 N?m; Cond3: measuring points 3#?5#, 1800 r/min, and 9 N?m; Cond4: measuring points 1#?3#, 2400 r/min, and 9 N?m; Cond5: measuring points 1#?3#, 1800 r/min, and 3 N?m.
Abbreviations
DOFDegree of freedom
FEMFinite element method
FTFourier Transform
FRFFrequency response function
GMSGear meshing stiffness
GMSIGear meshing stiffness identification
IMFIntrinsic mode function
IFTInverse Fourier Transform
Variables
DSystem damping matrix
fixR,, fixIReal and imaginary parts of the x component of bearing dynamic force at bearing i, respectively
fmMeshing frequency
fdIntermediate variable of the decoupled bearing dynamic force excitation spectra vector
FExternal excitation
F12External load
FbBearing dynamic force excitation spectra vector
FBBearing force
FdDecoupled bearing dynamic force excitation spectra vector
FeLoad caused by no-load transfer error of the gear pair
HixRjxR,HixIjxIFrequency response functions
HTransfer function matrix
HdDecoupled transfer function matrix
HTTransition matrix
I1, I2 Transverse moments of inertia of gears 1 and 2, respectively
J1, J2 Polar moments of inertia of gears 1 and 2, respectively
k12Meshing stiffness of the gear pair
kmiMeshing stiffness of gear pair i
kxx, kyy, kzzBearing stiffnesses of translational DOF in x-, y-, and z-direction, respectively
kθxθx, kθyθyBearing stiffnesses of rotational DOF in x and y directions, respectively
kbBearing flexibility vector
kBBearing stiffness vector
k~mTemporary variable containing meshing stiffness of all gear pairs
KSystem stiffness matrix
K12Meshing stiffness matrix of the gear pair
KisUnit stiffness matrix of the system
K~mEstimated whole meshing stiffness matrix
KmiMeshing stiffness matrix of gear pair i
mNumber of bearing dynamic force excitation channels
mg Mass of gear
m1, m2 Masses of gears 1 and 2, respectively
MSystem mass matrix
MgMass matrix of a lumped mass model
M12Mass matrix of the gear pair
nNumber of response channels
niNode number
rb1,rb2Radii of base circle
S22-norm similarity index
SeEnergy ratio similarity index
T1, T2 Torques applied on the input shaft and output shaft, respectively
uNodes displacement vector
ueDOF of the beam model
ufVibration response of all nodes in the frequency domain
wiElement of the weighted matrix
WWeighted matrix
xTranslational DOF of beam in x direction
x1,x2Translational DOFs of gears 1 and 2 in x direction, respectively
xbTranslational DOF of bearing in x direction
xjxR,xjxIReal and imaginary parts of the x component of housing vibration response at location j, respectively
xResponse channel spectra vector
x~bVibration response of all bearing nodes
xBDisplacement vector of bearing
xdDecoupled response channel spectra vector
X12Generalized coordinate of the gear pair
yTranslational DOF of beam in y direction
y1, y2Translational DOFs of gears 1 and 2 in y direction, respectively
ybTranslational DOF of bearing in y direction
zTranslational DOF of beam in z direction
z1, z2Translational DOFs of gears 1 and 2 in z direction, respectively
zbTranslational DOF of bearing in z direction
αWeighted factor
α12Projection vector of the gear pair
ψ12Angle between the positive y axis and the meshing surface
ΨProjection matrix of all gear nodes
δNumerical error
ωAngular frequency
θx, θy, θzRotational DOFs of beam in x, y, and z directions, respectively
θx1, θx2Rotational DOFs of gears 1 and 2 in x direction, respectively
θy1, θy2Rotational DOFs of gears 1 and 2 in y direction, respectively
θz1, θz2Rotational DOFs of gears 1 and 2 in z direction
θxb, θyb, θzbRotational DOFs of bearing in x, y, and z directions, respectively
ΘiProjection matrix
  
Abbreviations
DOFDegree of freedom
FEMFinite element method
FTFourier Transform
FRFFrequency response function
GMSGear meshing stiffness
GMSIGear meshing stiffness identification
IMFIntrinsic mode function
IFTInverse Fourier Transform
Variables
DSystem damping matrix
fixR,, fixIReal and imaginary parts of the x component of bearing dynamic force at bearing i, respectively
fmMeshing frequency
fdIntermediate variable of the decoupled bearing dynamic force excitation spectra vector
FExternal excitation
F12External load
FbBearing dynamic force excitation spectra vector
FBBearing force
FdDecoupled bearing dynamic force excitation spectra vector
FeLoad caused by no-load transfer error of the gear pair
HixRjxR,HixIjxIFrequency response functions
HTransfer function matrix
HdDecoupled transfer function matrix
HTTransition matrix
I1, I2 Transverse moments of inertia of gears 1 and 2, respectively
J1, J2 Polar moments of inertia of gears 1 and 2, respectively
k12Meshing stiffness of the gear pair
kmiMeshing stiffness of gear pair i
kxx, kyy, kzzBearing stiffnesses of translational DOF in x-, y-, and z-direction, respectively
kθxθx, kθyθyBearing stiffnesses of rotational DOF in x and y directions, respectively
kbBearing flexibility vector
kBBearing stiffness vector
k~mTemporary variable containing meshing stiffness of all gear pairs
KSystem stiffness matrix
K12Meshing stiffness matrix of the gear pair
KisUnit stiffness matrix of the system
K~mEstimated whole meshing stiffness matrix
KmiMeshing stiffness matrix of gear pair i
mNumber of bearing dynamic force excitation channels
mg Mass of gear
m1, m2 Masses of gears 1 and 2, respectively
MSystem mass matrix
MgMass matrix of a lumped mass model
M12Mass matrix of the gear pair
nNumber of response channels
niNode number
rb1,rb2Radii of base circle
S22-norm similarity index
SeEnergy ratio similarity index
T1, T2 Torques applied on the input shaft and output shaft, respectively
uNodes displacement vector
ueDOF of the beam model
ufVibration response of all nodes in the frequency domain
wiElement of the weighted matrix
WWeighted matrix
xTranslational DOF of beam in x direction
x1,x2Translational DOFs of gears 1 and 2 in x direction, respectively
xbTranslational DOF of bearing in x direction
xjxR,xjxIReal and imaginary parts of the x component of housing vibration response at location j, respectively
xResponse channel spectra vector
x~bVibration response of all bearing nodes
xBDisplacement vector of bearing
xdDecoupled response channel spectra vector
X12Generalized coordinate of the gear pair
yTranslational DOF of beam in y direction
y1, y2Translational DOFs of gears 1 and 2 in y direction, respectively
ybTranslational DOF of bearing in y direction
zTranslational DOF of beam in z direction
z1, z2Translational DOFs of gears 1 and 2 in z direction, respectively
zbTranslational DOF of bearing in z direction
αWeighted factor
α12Projection vector of the gear pair
ψ12Angle between the positive y axis and the meshing surface
ΨProjection matrix of all gear nodes
δNumerical error
ωAngular frequency
θx, θy, θzRotational DOFs of beam in x, y, and z directions, respectively
θx1, θx2Rotational DOFs of gears 1 and 2 in x direction, respectively
θy1, θy2Rotational DOFs of gears 1 and 2 in y direction, respectively
θz1, θz2Rotational DOFs of gears 1 and 2 in z direction
θxb, θyb, θzbRotational DOFs of bearing in x, y, and z directions, respectively
ΘiProjection matrix
  
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