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Fault signature detection for rolling element bearings in electric machinesStack, Jason R. 12 1900 (has links)
No description available.
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Fabrication and calibration of an open architecture diamond turning machineUlmer, Bernard C., Jr. 12 1900 (has links)
No description available.
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Helicopter tail boom vibration analysis and suppressionFunnell, M. E. (Marc Edwin) 04 1900 (has links)
Thesis (MScEng)--University of Stellenbosch, 2002. / ENGLISH ABSTRACT: An experimental investigation was conducted usmg a cantilever beam to illustrate an
understanding of vibration techniques and phenomena. The [Tee and forced vibration of the
cantilever beam was investigated using various modelling strategies. Theoretical models such
as the Lumped parameter, Myklestad, Distributed Parameter and Finite Element Methods
were analysed and compared with experimental measurements. Excellent agreement of the
natural frequencies, mode shapes and the harmonic transfer functions were found.
To investigate tail boom vibration, a Finite Element Model of a simplified helicopter tail
boom design was tested against experimentally measured data. The results correlated
accurately and the model was used to evaluate the effectiveness of a vibration suppression
system designed for the tail boom.
The vibration suppression system was designed using two, parallel dynamic absorbers to
reduce tail boom vibrations at its two dominant frequencies. For the purposes of this thesis,
the dynamic absorbers were tuned to reduce the resonant peaks at the dominant excitation
frequencies of the excitation force in-line with the thrust of the tail rotor only. This excitation
force was estimated using a simplified tail rotor dynamic model, which when compared with
actual vibration data was assumed to predict the basic frequency trends of the force, reliably.
Incorporating the designed components into an accurate Lumped Parameter model of a
cantilever beam structure and simulating the response of the structure at the dominant
excitation frequencies of the calculated excitation force, tested the vibration suppression
system. The results of this investigation proved the effectiveness of the design procedure and
optimisation process of the design parameters. A similarly designed suppression system was
incorporated into the Finite Element tail boom model and from the analytical results obtained
it was shown to cause a fair reduction in the vibration response at the two dominant
frequencies of the excitation force.
Finally, two possible applications were suggested from the research presented in this thesis.
The first application was the simplified configuration of a vibration monitoring system for the
tail boom. The second application was the possible development of a system using the
response of vibration suppression absorbers to predict the magnitudes of the excitation forces
on the tail boom. / AFRIKAANSE OPSOMMING: 'n Experimentele ondersoek is ondemeem deur gebruik te maak van 'n ingeklemde balk om
vibrasie tegnieke te illustreer. Die vrye en geforseerde vibrasie van die ingeklemde balk is
ondersoek deur verskillende model tegnieke te gebruik. Teoretiese modelle soos die Lumped
parameter, Myklestad, Distributed Parameter en Eindige Element Metodes was geanaliseer
en vergelyk met die eksperimentele waardes. Uitstekende ooreenstemmings was gevind
tussen die natuurlike frekwensies, die eievektore en die harmoniese oordragsfunk:sie.
Om stert vibrasie te ondersoek, was'n eindige element model van 'n helikopter stert getoets
teenoor die eksperimentele data. Die resultate het akuraat gekorreleer en dus was die model
gebruik om die effektiwiteit van 'n vibrasie supressie sisteem te evalueer.
Die vibrasie supressie sisteem was ontwerp deur gebruik te maak van twee parallele
dinamiese absorbeerders om die helikopter stert se eerste twee dominante vibrasie
frekwensies te minimeer. Vir die doel van hierdie tesis was die dinamiese absorbeerders
ingestel om net die resonante pieke van die opgewende krag wat in lyn is met die drykrag van
die stert rotor te minimeer Hierdie opgewende krag was, deur gebruik te maak van 'n basiese
stert rotor dinamiese model, aanvaar om die basiese frekwensie tendense van die krag te
voorspel. Die supressie sisteem wat ontwerp was, was getoets op die lumped parameter balk
en het veroorsaak dat die voorspelde opgewende krag by al twee van sy dominante .
frekwensies baie geminirneer was. Die effektiwiteit van die sisteem was dus bewys en die
sisteem was gebruik om die respons van die eindige element model van die stert te verbeter.
Die resultate het 'n aanvaarbare reduksie in die respons by die twee dominante frekwensies
van die opgewende krag, gewys.
Laastens, deur gebruik te maak van die resultate in hierdie tesis. was twee moontlikhede
voorgestel. Die eerste een was die konfigurasie van 'n vibrasie moniterings sisteem vir die
helikopter stert. Die tweede mmontlikheid was die moontlike ontwikkeling van 'n sisteem
wat die grootte van die opgewende krag by die stert rotor kon voorspel, deur gebruik te maak
van die vibrasie suppressie absorbeerders.
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Design of structures and foundations for vibrating machines.Ulassi, V. R. January 2002 (has links)
The lack of methods for rigorous dynamic analysis of foundations and structures for
vibrating machines has resulted in below optimum performance and in some cases
reduction of life of machines, structures and foundations. The costs and complexities
of these machines make it necessary to conduct proper geotechnical site investigations.
and dynamic analyses to obtain the response of the soil, foundation and structure as a
system to excitation. In order to highlight the use of dynamic analyses, the response of
the foundations and structures were compared to the "rule of thumb" which is based on
mass ratio. Furthermore sensitivity analyses were carried out comprising the following
variables:
• Shear modulus of soil, G
• Poisson's ratio of soil,Y
• Type of structure (ie raft, table top and multi-storey)
• Stiffness of structure
• Stiffness of foundation
The fundamentals of structural dynamics have not been dealt with in this dissertation.
The dynamic analyses were carried out using a finite element analysis program called
Strand 7. The results were typical of a finite element analysis, giving stresses, strains,
deflections, amplitudes, frequencies and velocities of vibration.
The traditional "elastic halfspace model" is deficient as it does not account for soil
comprising various layers. The theory has been based on an isolated circular footing.
Most foundations are located in soils with layered mediums, are rectangular and in
some cases are affected by the interaction of foundations in close proximity.
Furthermore there is a need to account for the non-linear effects and properties of soil.
It is therefore becoming more attractive to adopt mathematical models of soils using
finite elements, where the visco-elastoplastic properties of soils can be realized and
modeled. Furthermore the finite element method overcomes limitations such as
layering and shapes or foot-prints of foundations.
The "rule of thumb" or mass ratio method of design procedure is as follows:-
• firstly the requirements of stresses and serviceability must be satisfied. This is
usual in a statically loaded system. the ratio of the machine mass to that of the foundation together with the
structure should be greater than 3 in the case of a revolving machine and 5 in
the case of a reciprocating machine.
• in order to obtain uniform settlement of the foundation the distance of the
combined centre of gravity of the machine and foundation from the centre of
area in contact with the soil is limited to 5% of the corresponding dimension of
the foundation.
It is evident that the mass ratio lacks accuracy in that there are several parameters that
are required to describe the satisfactory performance of a system such as amplitude,
frequency and velocity of vibration. The finite element method allows for calibration of
the model to account for the real behaviour of the system. Calibration is generally
conducted using sensitive transducers called accelerometers. The accelerometers
produce power spectral density (PSD) graphs from which deflections and stresses can
be back calculated. The deflections and stresses are compared with calculated
deflections and stresses. Descriptions of the methods of analysis followed by
presentation of results, discussions and interpretations have been included. To
motivate the use of dynamic analyses case histories have been presented and
discussed. Finally the dissertation concludes with findings of the study together with
recommendations for the way forward in terms of research. / Thesis (M.Sc.)-University of Natal, Durban, 2002.
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A study of the effect of lubrication on the dynamics of spinning spindlesSoo, S. L. (Shao-lee) 05 1900 (has links)
No description available.
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Current-based sensorless vibration monitoring of small ac machinesRiley, Caryn M 08 1900 (has links)
No description available.
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Vibration excitation of axial compressor rotor bladesRaubenheimer, Gert 12 1900 (has links)
Thesis (MScEng)--Stellenbosch University, 2011. / ENGLISH ABSTRACT: Turbomachines are exposed to several environmental factors which may
cause failure of components. One of these factors, high cycle fatigue, is often
caused by blade utter. This thesis forms part of a project of the European
Seventh Framework Programme (FP7), called project Future. Project Future
is doing theoretical and experimental investigation into the occurrence
of utter in turbomachinery. The objective of this thesis was to evaluate the
effectiveness of a gas injection system as a means of exciting vibrations on the
rst stage rotor blades of a compressor. Unsteady simulations of the excitation
velocity perturbations were performed in the Computational Fluid Dynamics
(CFD) software, Numeca FINE/Turbo. Experimental testing on the in-house
Rofanco compressor test bench, using one prototype of the 15 injector system,
provided data that was used to implement boundary conditions and to verify
certain aspects of the unsteady simulation results. The simulation results revealed
the following: the injector bypass frequency was so dominant that the
excitation frequency was hardly detectable in the majority of cases. Furthermore,
several secondary frequencies were consistently present. The injector
bypass frequency, as well as the secondary frequencies, occurred as a result
of the convolution of Fast Fourier Transforms. While the injector bypass frequencies
can theoretically be eliminated, it will not be possible to eliminate
the secondary frequencies from the blade response. In conclusion, according to
the CFD results, it will not be possible to excite a single excitation frequency
by making use of a nite number of gas injector vibration exciters. / AFRIKAANSE OPSOMMING: Turbomasjiene word onderwerp aan verskeie omgewingsfaktore wat falings
van komponente kan veroorsaak. Een van hierdie faktore, naamlik hoëfrekwensie vermoeidheid, word onder andere veroorsaak deur lem adder. Hierdie
tesis is deel van 'n projek in die Sewende Europese Raamwerk Program
(European Seventh Framework Programme - FP7), projek Future. Projek
Future doen teoretiese en eksperimentele ondersoek na die voorkoms van lemfl adder in turbomasjienerie. Die doelwit van hierdie tesis was om die effektiwiteit
van 'n gasinspuiter vibrasie-opwekkingstelsel te evalueer, deur gebruik te
maak van onbestendige simulasie in die berekenings vloei-meganika sagtewarepakket,
Numeca FINE/Turbo. Eksperimentele toetswerk op die plaaslike
Rofanco kompressortoetsbank, met 'n prototipe van die 15 inspuiter stelsel,
het inligting verskaf wat gebruik is om die inlaattoestande te spesi seer en
simulasieresultate te korreleer. Die simulasieresultate het getoon dat die frekwensie
waarteen 'n lem by die inspuiters verbybeweeg, so prominent is, dat
dit in die meerderheid van gevalle baie meer prominent is as die opwekkingsfrekwensie.
Verder was daar ook deurgaans 'n aantal sekondêre frekwensies
teenwoordig. Die teenwoordigheid van die inspuiter verbybeweeg frekwensie
en die sekondêre frekwensies is die resultaat van die konvolusie van Vinnige
Fourier Transforme. Alhoewel dit in teorie moontlik sal wees om die inspuiter
verbybeweeg frekwensie te elimineer, is dit onmoontlik om die sekondêre
frekwensies uit die lem vibrasie te elimineer. Ter opsomming, volgens die berekenings
vloei-meganika resultate, is dit nie moontlik om met 'n stelsel van
'n eindige aantal inspuiters, 'n enkele vibrasie frekwensie op te wek nie.
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Stochastic Mechanical SystemsBost, Robert Berton 08 1900 (has links)
To understand the phenomena associated with such stochastic processes and to predict, at least qualitatively, the behavior of mechanical systems within environments which are completely random in time, new mechanical tools are necessary. Fortunately, the derivation of these tools does not necessitate a complete departure from existing theories. In fact, they may be considered as an extension of the well-defined theory of the integral transform, in particular, the exponential Fourier integral transform.
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Diagnostics, prognostics and fault simulation for rolling element bearingsSawalhi, Nader, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW January 2007 (has links)
Vibration signals generated from spalled elements in rolling element bearings (REBs) are investigated in this thesis. A novel signal-processing algorithm to diagnose localized faults in rolling element bearings has been developed and tested on a variety of signals. The algorithm is based on Spectral Kurtosis (SK), which has special qualities for detecting REBs faults. The algorithm includes three steps. It starts by pre-whitening the signal's power spectral density using an autoregressive (AR) model. The impulses, which are contained in the residual of the AR model, are then enhanced using the minimum entropy deconvolution (MED) technique, which effectively deconvolves the effect of the transmission path and clarifies the impulses. Finally the output of the MED filter is decomposed using complex Morlet wavelets and the SK is calculated to select the best filter for the envelope analysis. Results show the superiority of the developed algorithm and its effectiveness in extracting fault features from the raw vibration signal. The problem of modelling the vibration signals from a spalled bearing in a gearbox environment is discussed. This problem has been addressed through the incorporation of a time varying, non-linear stiffness bearing model into a previously developed gear model. It has the new capacity of modeling localized faults and extended faults in the different components of the bearing. The simulated signals were found to have the same basic characteristics as measured signals, and moreover were found to have a characteristic seen in the measured signals, and also referred to in the literature, of double pulses corresponding to entry into and exit from a localized fault, which could be made more evident by the MED technique. The simulation model is useful for producing typical fault signals from gearboxes to test new diagnostic algorithms, and also prognostic algorithms. The thesis provides two main tools (SK algorithm and the gear bearing simulation model), which could be effectively employed to develop a successful prognostic model.
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Diagnostics, prognostics and fault simulation for rolling element bearingsSawalhi, Nader, Mechanical & Manufacturing Engineering, Faculty of Engineering, UNSW January 2007 (has links)
Vibration signals generated from spalled elements in rolling element bearings (REBs) are investigated in this thesis. A novel signal-processing algorithm to diagnose localized faults in rolling element bearings has been developed and tested on a variety of signals. The algorithm is based on Spectral Kurtosis (SK), which has special qualities for detecting REBs faults. The algorithm includes three steps. It starts by pre-whitening the signal's power spectral density using an autoregressive (AR) model. The impulses, which are contained in the residual of the AR model, are then enhanced using the minimum entropy deconvolution (MED) technique, which effectively deconvolves the effect of the transmission path and clarifies the impulses. Finally the output of the MED filter is decomposed using complex Morlet wavelets and the SK is calculated to select the best filter for the envelope analysis. Results show the superiority of the developed algorithm and its effectiveness in extracting fault features from the raw vibration signal. The problem of modelling the vibration signals from a spalled bearing in a gearbox environment is discussed. This problem has been addressed through the incorporation of a time varying, non-linear stiffness bearing model into a previously developed gear model. It has the new capacity of modeling localized faults and extended faults in the different components of the bearing. The simulated signals were found to have the same basic characteristics as measured signals, and moreover were found to have a characteristic seen in the measured signals, and also referred to in the literature, of double pulses corresponding to entry into and exit from a localized fault, which could be made more evident by the MED technique. The simulation model is useful for producing typical fault signals from gearboxes to test new diagnostic algorithms, and also prognostic algorithms. The thesis provides two main tools (SK algorithm and the gear bearing simulation model), which could be effectively employed to develop a successful prognostic model.
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