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SENSOR CALIBRATION SYSTEM AND METHODOLOGY FOR TIP CLEARANCE MEASUREMENTS IN TURBOMACHINESSantiago D Salinas (10941474) 08 June 2021 (has links)
<p>With increasingly tighter tip
clearances in modern turbomachinery, it is essential to precisely measure this
parameter during turbomachinery characterization. Benefits from measuring tip
clearances include monitoring the structural integrity of the machine and estimating
aerodynamic losses incurred due to leakage flows. At present, capacitance probes
are one of the most commonly used sensors for tip clearance measurements in
turbomachines as they are accurate and robust. One of the main challenges when using
capacitance probes is properly calibrating the sensors, which usually involves
complex positioning systems and blade representative targets. This manuscript
describes in detail the development of a
methodology for in-house calibration of capacitance probes for tip clearance
measurements. A novel calibration procedure that does not involve rotating
components is investigated and compared against established calibration
methods. First, a calibration bench was developed to demonstrate the static and
dynamic performance of the acquisition system and perform quasi-static as well
as dynamic calibrations in a controlled environment. An in-situ methodology was
then developed to calibrate the sensors once installed in a two-stage rotating
turbine rig. The proposed methodology does not require complex positioning
systems and a regression analysis using a least squares scheme resulted in a coefficient
of determination of 0.9998. The calibration was validated using specially
designed instrumentation at various speeds that span the operating envelope of
the rig. A Bayesian model that was developed to estimate measurement
uncertainties for each method showed that uncertainties as low as ± 5μm can be
achieved with the proposed system. The proposed methodology was used in a two-stage
turbine rig. Measurements taken at three different circumferential locations
were subsequently used to map the spatial distribution of tip clearances throughout
the speed operational envelope of the turbine. Finally, a reduced order rotor displacement
model was developed and fitted to capacitance probes data. The work presented
in this thesis lays the foundation for high fidelity tip clearance measurement
capabilities at the Purdue Experimental Turbine Aerothermal Laboratory and can
be implemented into any rotating rig. </p>
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Understanding the Responses of a Metal and a CMCTurbine Blade during a Controlled Rub Event using a Segmented ShroudLangenbrunner, Nisrene A. 08 August 2013 (has links)
No description available.
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Measurements of the Tip-gap Turbulent Flow Structure in a Low-speed Compressor CascadeTang, Genglin 18 May 2004 (has links)
This dissertation presents results from a thorough study of the tip-gap turbulent flow structure in a low-speed linear compressor cascade wind tunnel at Virginia Tech that includes a moving belt system to simulate the relative motion between the tip and the casing. The endwall pressure measurements and the surface oil flow visualizations were made on a stationary endwall to obtain the flow features and to determine the measurement profiles of interest. A custom-made miniature 3-orthogonal-velocity-component fiber-optic laser-Doppler velocimetry (LDV) system was used to measure all three components of velocity within a 50 mm spherical measurement volume within the gap between the endwall and the blade tip, mainly for the stationary wall with 1.65% and 3.30% tip gaps as well as some initial experiments for the moving wall.
Since all of the vorticity in a flow originates from the surfaces under the action of strong pressure gradient, it was very important to measure the nearest-wall flow on the endwall and around the blade tip. The surface skin friction velocity was measured by using viscous sublayer velocity profiles, which verified the presence of an intense lateral shear layer that was observed from surface oil flow visualizations. All second- and third-order turbulence quantities were measured to provide detailed data for any parallel CFD efforts.
The most complete data sets were acquired for 1.65% and 3.30% tip gap/chord ratios in a low-speed linear compressor cascade. This study found that tip gap flows are complex pressure-driven, unsteady three-dimensional turbulent flows. The crossflow velocity normal to the blade chord is nearly uniform in the mid tip-gap and changes substantially from the pressure to suction side. The crossflow velocity relies on the local tip pressure loading that is different from the mid-span pressure loading because of tip leakage vortex influence. The tip gap flow is highly skewed three-dimensional flow throughout the full gap. Normalized circulation within the tip gap is independent of the gap size. The tip gap flow interacts with the primary flow, separates from the endwall, and rolls up on the suction side to form the tip leakage vortex. The tip leakage vortex is unsteady from the observation of the TKE transport vector and oil flow visualizations. The reattachment of tip separation vortex on the pressure side strongly depends on the blade thickness-to-gap height ratio after the origin of tip leakage vortex but is weakly related to it before the origin of tip leakage vortex for a moderate tip gap. Other than the nearest endwall and blade tip regions, the TKE does not vary much in tip gap. The tip leakage vortex produces high turbulence intensities. The tip gap flow correlations of streamwise and wall normal velocity fluctuations decrease significantly from the leading edge to the trailing edge of the blade due to flow skewing. The tip gap flow is a strongly anisotropic turbulent flow. Rapid distortion ideas can not apply to it. A turbulence model based on stress transport equations and experimental data is necessary to reflect the tip gap flow physics. For the moving endwall, relative motion skews the inner region flow and is decorrelated with the outer layer flow. Hence, the TKE and correlations of streamwise and wall normal velocity fluctuations decrease. / Ph. D.
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Multi-axis probing system for nano-metrologyGobbalipur Ranganath, Jayanth 12 January 2009 (has links)
No description available.
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Process monitoring of turbine blades : Monitoring of blade tip clearance using eddy current sensorsAndersson, Hampus January 2022 (has links)
This thesis has been a collaboration between the Royal Institute of Technology (KTH) and Siemens Energy which invest in the research facility at KTH. The objective was to investigate the use of eddy current sensors in real-time monitoring of turbine blades. The main focus has been on finding a use for blade tip clearance and a correlation for the insufficient sampling that eddy current sensors suffer from. At the same time, it was desirable to also investigate the use of the same sampled data for blade tip vibration. The research on eddy current sensors is important for their relative low price compared to other instruments and how resistance it is to contamination found in turbines, enabling real-time monitoring. The testing has been conducted at the Energy Technology department which utilizes a scaled version of a full-sized turbine to investigate performance measurements. It is scaled to have the same stage loading for both blisks investigated. Two different blisks have been used for this project, one with thicher but fewer blades and one with thinner but more blades. On each blisk different types of sampling have been done in order to capture suitable data for both tip timing and tip vibration. This resulted in sampling with static RPM and sweeps over certain regions as well as full sweeps from design RPM to standstill. A computer model was developed to evaluate the sampled data. In the model, the sample points were interpolated to compensate for the insufficient sampling, enabling tip gap measurements. Measurements and calibration were done on the blisks for the possibility of using a compensation curve in order to be able to compensate for the signal error. The results show that eddy current sensors and setup used here have a good capability of capturing the tip clearance with precision in the range of hundreds of millimeter on the blisk with thicker blades and up to a certain rotational speed on the blisk with thinner blades. In regards to the tip vibration, eddy current system had problems capturing the time of arrival with sufficient precision correctly. / Den här uppsatsen har varit ett sammarbete mellan Kunglig Tekniska Högskolan (KTH) och Simens Energy vilka investerar i forskningen som bedrivs på KTH. Målet var att undersöka användningen av eddy current sensors för övervakning av turbinbliskar. Huvudfokus har varit att hitta användning av sensorerna för topspelsmätningar och ta fram en korregering av den otillräckliga insamlingen av data som eddy current sensorer lider av. Samtidigt var det önskvärt att samtidigt undersöka samma insamlade data för att utvärdera bladvibrationer. Forskning på eddy current sensorer är viktig för dess relativt låga pris jämfört med andra alternativ samt att de dess höga motståndskraft mot smuts som ofta finns i miljöer där turbiner används. Testerna har gjorts på instutitionen för Energiteknik vilka använder en nedskalad versioner av den verkliga storleken på turbinen för att utföra mätningar på. Två olika bliskar har använts för detta projekt, en med grövre men färre blad samt en med tunnare och fler blad. Stegbelastningen är dock samma för båda. På båda bladen har olika typer mätningar gjorts för att kunna fånga passade data för båda topspelsmätningar och bladvibrationer. Detta gav data med statiskt varvtal, långsamma svepningar över specialla regioner och svepningar över från designvarvtal ner till stillastående. En datormodell har utvecklats för utvärdera insamlade data. I modellen sker en interpolering som kompenserar för de låga antalet samplade punkter på bladet. Mätnigar och kalibreringar är gjorda på bliskarna för att skapa en kompenseringskurva åt signalfel i utdatan. Resultatet visar att eddy current systemet har goda möjligheter att visa rätt toppspel med god precition för blisken med tjocka blad och upp till ett visst varvtal på den med tunnare blad. När det kommer till bladvibrationer hade sensorerna och datormodellen svårt att fånga rätt ankomst tid för bladet med tillräckligt hög precision.
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A stochastic analysis of Turbulence Intensity influence over various sizes of HAWT : Study of hypothetical relationship between Rotor Diameter and influence level of Turbulence Intensity / En stokastisk analys av turbulensintensitet inflytande över olika storlekar av HAWT : Studie av hypotetisk relation mellan rotordiameter och inflytande nivå turbulensintensitetNicholas, Allen Christo January 2016 (has links)
This disquisition aims for the study of turbulence intensity influence over the power performance of different sizes of turbines with the intent to validate a hypothesis. The hypothesis formulated for the analysis is the relationship between the rotor diameter (turbine size) and turbulence intensity. The hypothetical relationship is that the smaller turbines tend to experience more influence on the power performance from the turbulence in comparison with larger ones. For this examination, three different wind turbines of models Vestas V90, V100, V126 were chosen from three Swedish wind farms. The power performance of turbines at various levels of turbulence intensity were analyzed and the power deviation from the mean value due to influence of turbulence were assessed. The power deviation values of different turbines were compared at same level of wind speeds and also the power coefficients at same level of tip speed ratios were compared to validate the hypothesis. It was observed that the hypothesis seemed to appear true as higher influence on power curves were observed on V90 compared to others. Nevertheless, there were some obscene results which might be due to several factors such as influence of variation in hub height, site and inadequacy of data. / Detta examensarbete syftar till att studera hur ett vindkraftverks storlek påverkar inflytande från turbulens på effektuttaget. Hypotesen är att vindkraftverk med mindre rotordiameter påverkas mer av turbulens än de större. Tre vindkraftverksmodeller (Vestas V90, V100 och V126) från svenska vindkraftsparker valdes ut. De olika modellernas effektuttag för olika grader av turbulens analyserades och avvikelsen från effektmedelvärdet jämfördes. Effektavvikelserna samt verkningsgradsavvikelsen för de olika vindkraftverksmodellerna jämfördes vid samma vindhastighet respektive löptal för att kunna testa hypotesen. Hypotesen styrks då den mista modellen (Vestas V90) påverkas mest av turbulens. Resultatet har dock troligtvis påverkats av andra faktorer såsom tornhöjd, terräng och en begränsad mängd data.
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Performance improvement of the Rover 1S/60 Gas Turbine CompressorLuiten, Ruben Vincent 03 1900 (has links)
Thesis (MEng)--Stellenbosch University, 2015. / ENGLISH ABSTRACT: The use of gas turbines in central receiver solar power plant cycles has become
an increasingly popular research topic. This has led to the need to
investigate and analyse the effect of the solar receiver on the gas turbine
cycle. The aim of this thesis is to construct an experimental gas turbine
setup to accommodate further research on utilizing solar energy to power
gas turbines. The gas turbine under consideration is the Rover Gas Turbines
1S/60. The focus of this investigation is the centrifugal compressor of the
gas turbine. An increase in static pressure is required for the gas turbine
to cope with anticipated pressure drops in the central receiver that will be
part of the gas turbine cycle. The standard compressor design is analysed
by means of 3-D (CFD) analysis using CFX® and experimental data. The
new centrifugal compressor is designed by means of 1-D and 3-D (CFD)
analysis using CompAero and CFX®. The aim is to design a compressor
that maximizes the total-to-static pressure ratio. The size of the compressor
is highly constrained by the geometry parameters of the gas turbine.
Since the turbine rotor will remain unchanged, the power input, mass flow
rate and rotational speed must stay the same. The experimental setup was
build and the numerical results of the standard compressor were validated
against the experimental results. A new centrifugal compressor was designed.
The total-to-static pressure ratio was increased from 2.50 to 3.30
at an operating speed of 46 krpm. The efficiency of the compressor was
improved from 63.8% to 85.6%. The input power of the new compressor
design deviated 1.6% from the set benchmark, and 1.3% from the numerical
data of the standard compressor. / AFRIKAANSE OPSOMMING: Die gebruik van gasturbines in sonkragstasiesiklusse met ’n sentrale ontvanger
het gegroei tot ’n gewilde navorsingsonderwerp. Dit het gelei tot
die behoefte om die effek van die sonontvanger op die gasturbinesiklus te
ondersoek en te analiseer. Die doel van hierdie tesis is om ’n eksperimentele
gasturbine opstelling te bou vir verdere navorsing oor die benutting
van sonenergie om ’n gasturbine aan te dryf. Die gasturbine in oorweging
is die Rover Gas Turbines 1S/60. Die fokus van hierdie ondersoek is die
sentrifugale kompressor van die gasturbine. ’n Toename in statiese druk
word benodig vir die gasturbine om die verwagte drukverlies in die sentrale
ontvanger, wat deel uit maak van die gasturbinesiklus, te hanteer. Die
standaard kompressor ontwerp is geanaliseer deur middel van 3-D Berekenings
Vloeimeganika (BVM) analises met behulp van CFX® en eksperimentele
data. Die nuwe sentrifugale kompressor is ontwerp deur middel van
1-D en 3-D BVM analises met behulp van CompAero en CFX®. Die doel
is om ’n kompressor te ontwerp wat die totale-tot-statiese drukverhouding
maksimeer. Die grootte van die kompressor is beperk deur die geometrie
van die gasturbine omhulsel. Aangesien die turbinerotor onveranderd sal
bly, moet die insetdrywing, massa-vloeitempo en rotasiespoed dieselfde bly.
Die eksperimentele opstelling is gebou en die numeriese resultate van die
standaard kompressor is teenoor die eksperimentele resultate gevalideer.
’n Nuwe sentrifugale kompressor is ontwerp. Die totale-tot-statiese drukverhouding
is verhoog van 2.50 tot 3.30 teen ’n rotasiespoed van 46 000
omwentelings per minuut. Die doeltreffendheid van die kompressor is verbeter
van 63.8% tot 85.6%. Die insetdrywing van die nuwe kompressor ontwerp
het met 1.6% afgewyk van die vasgestelde maatstaf, en met 1.3% van
die numeriese data van die standaard kompressor.
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LOCALIZATION OF <i>DIPLODIA PINEA</i> IN DISEASED AND LATENTLY-INFECTED <i>PINUS NIGRA</i>Flowers, Jennifer Lee 01 January 2006 (has links)
Diplodia pinea causes Diplodia tip blight on more than 30 different pine species. During the past 10 years, Diplodia tip blight has emerged as a serious problem in landscape and Christmas tree farms in this region. Surveys of diseased and symptomless Austrian pines revealed that latent infections of symptomless shoots by D. pinea were common. Latent infections may account for the recently observed rapid decline of mildly diseased pines in our region. To investigate the colonization habits of D. pinea within its host, molecular cytology was attempted and traditional histology was performed on naturally infected, diseased and asymptomatic Austrian pine tissues. I devoted much effort to developing a transformation system for D. pinea. Ultimately I did not succeed in this goal, but I was able to develop a highly efficient protocol for Agrobacterium tumefaciens-mediated transformation of another pathogenic fungus, Colletotrichum graminicola, in the process. The work that I did should help in future efforts to transform D. pinea, something that will be essential if it is to become a tractable system for the study of fungal latency. Traditional histological methods were more successful, and provided important information about the nature of latent infections. Very sparse epiphytic and subcuticular fungal growth was observed in healthy shoots, however, no fungal tissues were present within the shoots. In diseased and latently infected shoots, crevices created between the needle bundles and the shoots were filled with fungal material, and hyphae were observed colonizing the needle sheaths. Hyphae were also observed breaching the shoot epidermal layer in these crevices and colonizing the underlying periderm. D. pinea colonization was extensive in all tissues of diseased shoots early in symptom development. In contrast, localized pockets of degradation were observed in the periderm and adjacent cortical cells located around areas of needle attachment in asymptomatic, latently infected shoots. The mechanism that operates to prevent expansion of these infected pockets in the latently infected shoots is still unclear. Obvious signs of pine defense mechanisms were only observed in 2 shoots. My observations were consistent with the idea that colonization progresses into the vascular tissues, and that this results in symptom development. Vascular colonization may occur more readily if the host is stressed. My research lays the groundwork for future efforts to understand the nature of the transformation from latent to pathogenic infection.
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Potential Wildlife ConflictsDolan, Corrine, Mannan, Bill 10 1900 (has links)
2 pp. / Tips for Arizona's Rural Landowners: Wildlife Unit / The Tips for Arizona's Rural Landowners Fact Sheet Series is intended to educate homeowners who have recently purchased small acreages in Arizona. The purpose of the series is to give homeowners information about living in rural settings. The Wildlife Unit includes fact sheets on wildlife habitat enhancement, the legal status of wildlife, venomous wildlife, wildlife transmitted diseases, aggressive wildlife and pet safety, wildlife-human conflicts, fencing, safe pesticide alternatives, and invasive wildlife.
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Wildlife Habitat 101Dolan, Corrine, Mannan, Bill 10 1900 (has links)
2 pp. / Tips for Arizona's Rural Landowners: Wildlife Unit / The Tips for Arizona's Rural Landowners Fact Sheet Series is intended to educate homeowners who have recently purchased small acreages in Arizona. The purpose of the series is to give homeowners information about living in rural settings. The Wildlife Unit includes fact sheets on wildlife habitat enhancement, the legal status of wildlife, venomous wildlife, wildlife transmitted diseases, aggressive wildlife and pet safety, wildlife-human conflicts, fencing, safe pesticide alternatives, and invasive wildlife.
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