Computational and Experimental Analysis of Flow Field in the Diffusers of Centrifugal Compressors

Centrifugal compressors are widely used for example in process industry, oil and gas industry, in small gas turbines and turbochargers. In order to achieve lower consumption of energy and operation costs the efficiency of the compressor needs to be improve. In the present work different pinches and low solidity vaned diffusers were utilized in order to improve the efficiency of a medium size centrifugal compressor. In this study, pinch means the decrement of the diffuser flow passage height. First different geometries were analyzed using computational fluid dynamics. The flow solver Finflo was used to solve the flow field. Finflo is a Navier-Stokes solver. The solver is capable to solve compressible, incompressible, steady and unsteady flow fields. Chien's k-e turbulence model was used. One of the numerically investigated pinched diffuser and one low solidity vaned diffuser were studied experimentally. The overall performance of the compressor and the static pressure distribution before and after the diffuser were measured. The flow entering and leaving the diffuser was measured using a three-hole Cobra-probe and Kiel-probes. The pinch and the low solidity vaned diffuser increased the efficiency of the compressor. Highest isentropic efficiency increment obtained was 3\% of the design isentropic efficiency of the original geometry. It was noticed in the numerical results that the pinch made to the hub and the shroud wall was most beneficial to the operation of the compressor. Also the pinch made to the hub was better than the pinchmade to the shroud. The pinch did not affect the operation range of the compressor, but the low solidity vaned diffuser slightly decreased the operation range.The unsteady phenomena in the vaneless diffuser were studied experimentally andnumerically. The unsteady static pressure was measured at the diffuser inlet and outlet, and time-accurate numerical simulation was conducted. The unsteady static pressure showed that most of the pressure variations lay at the passing frequency of every second blade. The pressure variations did not vanish in the diffuser and were visible at the diffuser outlet. However, the amplitude of the pressure variations decreased in the diffuser. The time-accurate calculations showed quite a good agreement with the measured data. Agreement was very good at the design operation point, even though the computational grid was not dense enough inthe volute and in the exit cone. The time-accurate calculation over-predicted the amplitude of the pressure variations at high flow.

Computational Analysis and Optimization of Real Gas Flow In Small Centrifugal Compressors

Small centrifugal compressors are more and more widely used in many industrialsystems because of their higher efficiency and better off-design performance comparing to piston and scroll compressors as while as higher work coefficient perstage than in axial compressors. Higher efficiency is always the aim of the designer of compressors. In the present work, the influence of four partsof a small centrifugal compressor that compresses heavy molecular weight real gas has been investigated in order to achieve higher efficiency. Two parts concern the impeller: tip clearance and the circumferential position of the splitter blade. The other two parts concern the diffuser: the pinch shape and vane shape. Computational fluid dynamics is applied in this study. The Reynolds averaged Navier-Stokes flow solver Finflo is used. The quasi-steady approach is utilized. Chien's k-e turbulence model is used to model the turbulence. A new practical real gas model is presented in this study. The real gas model is easily generated, accuracy controllable and fairly fast. The numerical results and measurements show good agreement. The influence of tip clearance on the performance of a small compressor is obvious. The pressure ratio and efficiency are decreased as the size of tip clearance is increased, while the total enthalpy rise keeps almost constant. The decrement of the pressure ratio and efficiency is larger at higher mass flow rates and smaller at lower mass flow rates. The flow angles at the inlet and outlet of the impeller are increased as the size of tip clearance is increased. The results of the detailed flow field show that leakingflow is the main reason for the performance drop. The secondary flow region becomes larger as the size of tip clearance is increased and the area of the main flow is compressed. The flow uniformity is then decreased. A detailed study shows that the leaking flow rate is higher near the exit of the impeller than that near the inlet of the impeller. Based on this phenomenon, a new partiallyshrouded impeller is used. The impeller is shrouded near the exit of the impeller. The results show that the flow field near the exit of the impeller is greatly changed by the partially shrouded impeller, and better performance is achievedthan with the unshrouded impeller. The loading distribution on the impeller blade and the flow fields in the impeller is changed by moving the splitter of the impeller in circumferential direction. Moving the splitter slightly to the suction side of the long blade can improve the performance of the compressor. The total enthalpy rise is reduced if only the leading edge of the splitter ismoved to the suction side of the long blade. The performance of the compressor is decreased if the blade is bended from the radius direction at the leading edge of the splitter. The total pressure rise and the enthalpy rise of thecompressor are increased if pinch is used at the diffuser inlet. Among the fivedifferent pinch shape configurations, at design and lower mass flow rates the efficiency of a straight line pinch is the highest, while at higher mass flow rate, the efficiency of a concave pinch is the highest. The sharp corner of the pinch is the main reason for the decrease of efficiency and should be avoided. The variation of the flow angles entering the diffuser in spanwise direction is decreased if pinch is applied. A three-dimensional low solidity twisted vaned diffuser is designed to match the flow angles entering the diffuser. The numerical results show that the pressure recovery in the twisted diffuser is higher than in a conventional low solidity vaned diffuser, which also leads to higher efficiency of the twisted diffuser. Investigation of the detailed flow fields shows that the separation at lower mass flow rate in the twisted diffuser is later than in the conventional low solidity vaned diffuser, which leads to a possible wider flow range of the twisted diffuser.

Numerical simulation of rotor-stator interaction and tip clearance flow in centrifugal compressors

The effect of the tip clearance and vaneless diffuser width on the stage performance and flow fields of a centrifugal compressor were studied numerically and results were compared to the experimental measurements. The diffuser width was changed by moving the shroud side of the diffuser axially and six tip clearances size from 0.5 to 3 mm were studied. Moreover, the effects of rotor-stator interaction on the diffuser and impeller flow fields and performance were studied. Also transient simulations were carried out in order to investigate the influence of the interaction on the impeller and diffuser performance parameters. It was seen that pinch could improve the performance and it help to get more uniform flow at exit and less back flow from diffuser to the impeller.

Performance Characteristics of an Axial-Flux Solid-Rotor-Core Induction Motor

The integration of electric motors and industrial appliances such as pumps, fans, and compressors is rapidly increasing. For instance, the integration of an electric motor and a centrifugal pump provides cost savings and improved performance characteristics. Material cost savings are achieved when an electric motor is integrated into the shaft of a centrifugal pump, and the motor utilizes the bearings of the pump. This arrangement leads to a smaller configuration that occupies less floor space. The performance characteristics of a pump drive can be improved by using the variable-speed technology. This enables the full speed control of the drive and the absence of a mechanical gearbox and couplers. When using rotational speeds higher than those that can be directly achieved by the network frequency the structure of the rotor has to be mechanically durable. In this thesis the performance characteristics of an axial-flux solid-rotor-core induction motor are determined. The motor studied is a one-rotor-one-stator axial-flux induction motor, and thus, there is only one air-gap between the rotor and the stator. The motor was designed for higher rotational speeds, and therefore a good mechanical strength of the solid-rotor-core rotor is required to withstand the mechanical stresses. The construction of the rotor and the high rotational speeds together produce a feature, which is not typical of traditional induction motors: the dominating loss component of the motor is the rotor eddy current loss. In the case of a typical industrial induction motor instead the dominating loss component is the stator copper loss. In this thesis, several methods to decrease the rotor eddy current losses in the case of axial-flux induction motors are presented. A prototype motor with 45 kW output power at 6000 min-1 was designed and constructed for ascertaining the results obtained from the numerical FEM calculations. In general, this thesis concentrates on the methods for improving the electromagnetic properties of an axial-flux solid-rotor-core induction motor and examines the methods for decreasing the harmonic eddy currents of the rotor. The target is to improve the efficiency of the motor and to reach the efficiency standard of the present-day industrial induction motors equipped with laminated rotors.

Radiaalikompressorin valinta hiilivetyteollisuudessa

Tutkimuksen tavoitteena oli selvittää hiilivetyteollisuudessa käytettävien radiaali-kompressorien ominaisuuksia, toimintaympäristöjä, turvallisuusasioita, etuja ja rajoitteita. Tämän lisäksi selvitettiin vaihtoehtoisia yleisesti käytettyjä menetelmiä radiaalikompressorien simuloimiseksi. Työssä tutkittiin myös kaupallisten mitoitusohjelmien soveltuvuutta laitesuunnittelun tueksi Neste Jacobs Oy:ssä. Työn kirjallisuusosassa käsiteltiin radiaalikompressorien toimintaympäristöjä, säätötapoja sekä näistäja muista tekijöistä aiheutuvia rajoitteita ja vaatimuksia. Kirjallisuustutkimuksen perusteella laadittiin tarkistuslista asioista, jotka tulee selvittää ennenvarsinaista radiaalikompressorien mitoittamista. Soveltuvaakaupallista kompressorien mitoitusohjelmaa ei tutkimuksessa löytynyt. Tämän vuoksi työn kokeellisessa osassa laadittiin Excel-laskentataulukko, joka perustuu yhteen kirjallisuusosassa esitettyyn mitoitustapaan. Laaditun laskentataulukon soveltuvuutta kompressorien esivalintaan testattiin vertailemalla ohjelman mitoituksia Neste Jacobs Oy:llä käytössä olevaan mitoitusohjelmaan ja toiseen työssä esitettyyn mitoitus-menetelmään. Lisäksi Excel-laskentataulukon ja Neste Jacobs Oy:n ohjelman mitoituksia verrattiin todellisen, käytössä olevan kompressorin suunnittelu- ja operointiarvoihin. Lisäksi tutkimuksessa arvioitiin laaditun laskentataulukon käytettävyyttä, rajoitteita ja kehitysmahdollisuuksia. Saatujen tulosten perusteella työssä laadittu laskentataulukko soveltuu sellaisenaan Neste Jacobs Oy:n radiaalikompressorien simulointiin.

Uudet DCHP-prosessit

Diplomityön tavoitteena on selvittää viiden uuden yhdistetyn sähkön- ja lämmöntuotantoprosessin taloudellisuus Suomessa ja Keski-Euroopassa. Polttoaineena käytetään maakaasua. Tehoalue on 1 kW – 1 MW. Työn alkuosassa on kerrottu kyseisten prosessien tekniset ominaisuudet ja käyttö tällä hetkellä. Työn loppuosassa on laskettu jokaisen prosessin taloudellisuus viidessä eri maassa (Suomessa, Alankomaassa, Belgiassa, Iso-Britanniassa ja Saksassa) viidessä eri skenaariossa (omakotitalot, rivitalot, kerrostalot, pienteollisuus ja keskisuuri teollisuus). Toisena aihepiirinä diplomityössä on verrattu kompressori- ja absorptiojäähdyttimiä keskenään ja kerrottu kaukokylmän tekemisestä. Työn tuloksena saatiin arvio siitä, miten taloudellisesti kannattavia kyseiset prosessit ovat tällä hetkellä verrattuna perinteisiin sähkön- ja lämmöntuotantotapoihin.

Paineilmajärjestelmän optimoinnin hyödyt tehtaan tuotantoprosessissa

Paineilmaa käytetään teollisuudessa hyvin yleisesti. Teollistuneissa maissa teollisuuden käyttämästä energiasta 8-10 % kuluu paineilman tuottamiseen. Paineilmakompressoreiden nykyaikaisen ohjausjärjestelmän avulla voidaan säästää paineilmajärjestelmän energiakustannuksia jopa 30 %. Ohjauksen optimoinnin yhteydessä on havaittu epäkohtia joiden poistaminen on parantanut tuotantolaitosten toimintaan niin, että saadut säästöt ovat olleet jopa energiasäästöjä suuremmat. Näitä optimoinnin välillisiä hyötyjä haluttiin selvittää tarkemmin. Tutkimuksessa perehdyttiin paineilman käytön ongelmiin eri tuotantolaitoksissa ja arvioitiin paineilmajärjestelmän optimoinnin vaikutuksia tehtaiden tuotantoon. Koska paineilmaa käytetään monissa tehtaiden kriittisissä kohteissa, on tutkimuskohteiden paineilmajärjestelmän ongelmista aiheutunut merkittäviä tuotannonmenetyksiä ja lisäkustannuksia. Merkittävimmät paperitehtaiden tuotantoa vaikeuttavat paineilmajärjestelmän tekniset ongelmat liittyvät paineilman puhtausvaatimuksiin ja riittävän verkkopaineen ylläpidon vaikeuteen. Organisatorisia ongelmia ovat paineilmajärjestelmän käyttöhenkilöstön asiantuntemuksen puutteellisuudet. Näistä aiheutuvaa tuotannon epäluotettavuutta voidaan merkittävästi pienentää kehittämällä paineilmakompressoreita, jälkikäsittelyä, ohjausta ja valvontaa alan asiantuntijoiden avustuksella.

Suurnopeuskompressorin tekninen markkinoilletuonti

Diplomityössä tarkastellaan suurnopeuskompressorin kehityspolkua suurnopeusteknologian lähtökohdista prototyypiksi ja edelleen teolliseksi tuotteeksi. Työssä tarkastelun kohteena on sähköteholtaan 20….250 kW oleva, suurnopeussähkökoneella ja öljyttömillä magneettilaakereilla varustettu keskipainekompressori. Tyypillisesti kompressorin painesuhde on 1,2 … 2,4. Ko. kompressorin käyttökohteina on tarkasteltu mm. pienen kunnallisen jätevedenpuhdistamon käsittelyaltaiden ilmastusta, suuren kaupungin vastaavan puhdistuslaitoksen ilmastuskäyttöä ja teollista käyttöä lasivillatehtaan ns. linkokompressorina. Suurnopeuskompressori soveltuu hyvin rinnankytkentään ns. ryhmäohjaimen avulla, jolloin rinnan voi olla kytkettynä jopa 16 kompressoria, joiden päällä oloa optimoidaan säätöteknisesti niin, että koko laitos on kuin yksi kompressori. Työssä tarkastellaan myös kompressorin em. sovellutuksista yli kahdeksan vuoden ajalta kaupallista kohteista saatuja käyttökokemuksia. Pääsäätöisesti voi sanoa, että jokaisessa uudessa sovellutuksessa ilmenee uusia reunaehtoja ja järjestelmäkohtaisia vaatimuksia, jotka täytyy huomioida kompressorin säädössä ja ominaisparametreissa.

Suurnopeuskompressorin modulaarisen runkosarjan suunnittelu

Tässä diplomityössä suunniteltiin parametrisesti modulaarinen koneen runko. Pyrkimyksenä oli suunnitella kokonaiskustannuksiltaan alhaisempi runkosarja jo olemassa oleviin suurnopeuskompressoreihin. Raportissa kerrotaan ensin modulaaristen tuoterakenteiden suunnittelusta ja käytettävästä suunnitteluohjelmistosta (SolidWorks). Sen jälkeen keskitytään suurnopeuskompressorin runkosarjan suunnitteluun esimerkkitapauksena. Aluksi keskitytään selvittämään rungolle asetettuja vaatimuksia ja ideoimaan erilaisia runkokonsepteja. Työ etenee ideoiden vertailun kautta modulaaristen konseptien luomiseen ja kahden moduulin moduulikohtaiseen suunnitteluun. Suunnitteluprosessissa käytetään rakenteen käyttäytymisen arviointiin äärellisten elementtien menetelmää (FEM). Työssä kehitettiin alkuperäisiin runkorakenteisiin verrattuna 10 % kustannuksiltaan edullisempi runkorakenneratkaisu, jonka purettavuus lisäksi alentaa rakenteen kuljetus- ja varastointikustannuksia.

Cost Optimisation of Mobile Advertising Client Data Transfer

Data traffic caused by mobile advertising client software when it is communicating with the network server can be a pain point for many application developers who are considering advertising-funded application distribution, since the cost of the data transfer might scare their users away from using the applications. For the thesis project, a simulation environment was built to mimic the real client-server solution for measuring the data transfer over varying types of connections with different usage scenarios. For optimising data transfer, a few general-purpose compressors and XML-specific compressors were tried for compressing the XML data, and a few protocol optimisations were implemented. For optimising the cost, cache usage was improved and pre-loading was enhanced to use free connections to load the data. The data traffic structure and the various optimisations were analysed, and it was found that the cache usage and pre-loading should be enhanced and that the protocol should be changed, with report aggregation and compression using WBXML or gzip.

Radiaalikompressorin juoksupyörän virtauskanavan suunnittelu

Diplomityössä on tutkittu radiaalikompressorin juoksupyörän virtauskanavan suunnittelua ja esitelty yleisesti käytetyt suunnittelumenetelmät. Virtauskanavan muodon vaikutukset virtauskenttään on esitetty. Työssä on kehitetty uusi tietokoneohjelma juoksupyörän kolmiulotteisen geometrian luomiseen, yksiulotteisesta suunnittelusta saatujen päämittojen pohjalta. Ohjelmalla luotua juoksupyörän geometriaa voidaan käyttää virtaus- ja lujuusanalyyseissä. Ohjelmaan on myös liitetty kaksiulotteinen kokoonpuristuvan viskoosittoman virtauksen ratkaisija.

Performance Improvement of Centrifugal Compressor Stage with Pinched Geometry or Vaned Diffuser

Centrifugal compressors are widely used for example in refrigeration processes, the oil and gas industry, superchargers, and waste water treatment. In this work, five different vaneless diffusers and six different vaned diffusers are investigated numerically. The vaneless diffusers vary only by their diffuser width, so that four of the geometries have pinch implemented to them. Pinch means a decrease in the diffuser width. Four of the vaned diffusers have the same vane turning angle and a different number of vanes, and two have different vane turning angles. The flow solver used to solve the flow fields is Finflo, which is a Navier-Stokes solver. All the cases are modeled with the Chien's k – έ- turbulence model, and selected cases are modeled also with the k – ώ-SST turbulence model. All five vaneless diffusers and three vaned diffusers are investigated also experimentally. For each construction, the compressor operating map is measured according to relevant standards. In addition to this, the flow fields before and after the diffuser are measured with static and total pressure, flow angle and total temperature measurements. When comparing the computational results to the measured results, it is evident that the k – ώ-SST turbulence model predicts the flow fields better. The simulation results indicate that it is possible to improve the efficiency with the pinch, and according to the numerical results, the two best geometries are the ones with most pinch at the shroud. These geometries have approximately 4 percentage points higher efficiency than the unpinched vaneless diffusers. The hub pinch does not seem to have any major benefits. In general, the pinches make the flow fields before and after the diffuser more uniform. The pinch also seems to improve the impeller efficiency. This is down to two reasons. The major reason is that the pinch decreases the size of slow flow and possible backflow region located near the shroud after the impeller. Secondly, the pinches decrease the flow velocity in the tip clearance, leading to a smaller tip leakage flow and therefore slightly better impeller efficiency. Also some of the vaned diffusers improve the efficiency, the increment being 1...3 percentage points, when compared to the vaneless unpinched geometry. The measurement results confirm that the pinch is beneficial to the performance of the compressor. The flow fields are more uniform with the pinched cases, and the slow flow regions are smaller. The peak efficiency is approximately 2 percentage points and the design point efficiency approximately 4 percentage points higher with the pinched geometries than with the un- pinched geometry. According to the measurements, the two best geometries are the ones with the most pinch at the shroud, the case with the pinch only at the shroud being slightly better of the two. The vaned diffusers also have better efficiency than the vaneless unpinched geometries. However, the pinched cases have even better efficiencies. The vaned diffusers narrow the operating range considerably, whilst the pinch has no significant effect on the operating range.

Study of a vapor-compression air-conditioning system for jetliners

Most modern passenger aeroplanes use air cycle cooling. A high-speed air cycle is a reliable and light option, but not very efficient. This thesis presents research work done to design a novel vapour cooling cycle for aeroplanes. Due to advancements in high-speed permanent magnet motors, the vapour cycle is seen as a competitive option for the air cycle in aeroplanes. The aerospace industry places tighter demands on the weight, reliability and environmental effects of the machinery than those met by conventional chillers, and thus modifications to conventional design are needed. The thesis is divided into four parts: the initial screening of the working fluid, 1-D design and performance values of the compressor, 1-D off-design value predictions of the compressor and the 3-D design of the compressor. The R245fa was selected as the working fluid based the study. The off-design range of the compressor was predicted to be wide and suitable for the application. The air-conditioning system developed is considerably smaller than previous designs using centrifugal compressors.

Insulation System in an Integrated Motor Compressor

A high-speed and high-voltage solid-rotor induction machine provides beneficial features for natural gas compressor technology. The mechanical robustness of the machine enables its use in an integrated motor-compressor. The technology uses a centrifugal compressor, which is mounted on the same shaft with the high-speed electrical machine driving it. No gearbox is needed as the speed is determined by the frequency converter. The cooling is provided by the process gas, which flows through the motor and is capable of transferring the heat away from the motor. The technology has been used in the compressors in the natural gas supply chain in the central Europe. New areas of application include natural gas compressors working at the wellheads of the subsea gas reservoir. A key challenge for the design of such a motor is the resistance of the stator insulation to the raw natural gas from the well. The gas contains water and heavy hydrocarbon compounds and it is far harsher than the sales gas in the natural gas supply network. The objective of this doctoral thesis is to discuss the resistance of the insulation to the raw natural gas and the phenomena degrading the insulation. The presence of partial discharges is analyzed in this doctoral dissertation. The breakdown voltage of the gas is measured as a function of pressure and gap distance. The partial discharge activity is measured on small samples representing the windings of the machine. The electrical field behavior is also modeled by finite element methods. Based on the measurements it has been concluded that the discharges are expected to disappear at gas pressures above 4 – 5 bar. The disappearance of discharges is caused by the breakdown strength of the gas, which increases as the pressure increases. Based on the finite element analysis, the physical length of a discharge seen in the PD measurements at atmospheric pressure was approximated to be 40 – 120 m. The chemical aging of the insulation when exposed to raw natural gas is discussed based on a vast set of experimental tests with the gas mixture representing the real gas mixture at the wellhead. The mixture was created by mixing dry hydrocarbon gas, heavy hydrocarbon compounds, monoethylene glycol, and water. The mixture was chosen to be more aggressive by increasing the amount of liquid substances. Furthermore, the temperature and pressure were increased, which resulted in accelerated test conditions. The time required to detect severe degradation was thus decreased. The test program included a comparison of materials, an analysis of the e ects of di erent compounds in the gas mixture, namely water and heavy hydrocarbons, on the aging, an analysis of the e ects of temperature and exposure duration, and also an analysis on the e ect of sudden pressure changes on the degradation of the insulating materials. It was found in the tests that an insulation consisting of mica, glass, and epoxy resin can tolerate the raw natural gas, but it experiences some degradation. The key material in the composite insulation is the resin, which largely defines the performance of the insulation system. The degradation of the insulation is mostly determined by the amount of gas mixture di used into it. The di usion was seen to follow Fick’s second law, but the coe cients were not accurately defined. The di usion was not sensitive to temperature, but it was dependent upon the thermodynamic state of the gas mixture, in other words, the amounts of liquid components in the gas. The weight increase observed was mostly related to heavy hydrocarbon compounds, which act as plasticizers in the epoxy resin. The di usion of these compounds is determined by the crosslink density of the resin. Water causes slight changes in the chemical structure, but these changes do not significantly contribute to the aging phenomena. Sudden changes in pressure can lead to severe damages in the insulation, because the motion of the di used gas is able to create internal cracks in the insulation. Therefore, the di usion only reduces the mechanical strength of the insulation, but the ultimate breakdown can potentially be caused by a sudden drop in the pressure of the process gas.

Paineilmakompressoreiden lämmön talteenoton optimointi

Tämän työn on teettänyt Vanhan Ruukin Kiinteistöpalvelu Oy ja työ on toteutettu kandidaatintyönä Lappeenrannan Teknilliselle Yliopistolle. Työn tarkoituksena oli selvittää työn teettäjän puolesta paineilmakompressoreiden lämmön talteenoton toimintaa sekä etsiä mahdollisia parannuskohteita järjestelmän hyötysuhteen nostamiseksi. Työ rajattiin koskemaan lämmön talteenoton yhtä lämmönvaihtopatteria ja siihen liittyvää nestekiertolaitteistoa. Syynä työn tekemiselle oli epäilys lämmön talteenoton huonosta hyötyprosentista. Tässä työssä oli tavoitteena ottaa kantaa myös mahdollisiin rahallisiin säästöihin joita järjestelmän kunnollisella toimintaan saattamisella olisi.