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.

Practical applications of a systematic approach to the chemical abatement of pollutants in water and air

The present dissertation is devoted to the systematic approach to the development of organic toxic and refractory pollutants abatement by chemical decomposition methods in aqueous and gaseous phases. The systematic approach outlines the basic scenario of chemical decomposition process applications with a step-by-step approximation to the most effective result with a predictable outcome for the full-scale application, confirmed by successful experience. The strategy includes the following steps: chemistry studies, reaction kinetic studies in interaction with the mass transfer processes under conditions of different control parameters, contact equipment design and studies, mathematical description of the process for its modelling and simulation, processes integration into treatment technology and its optimisation, and the treatment plant design. The main idea of the systematic approach for oxidation process introduction consists of a search for the most effective combination between the chemical reaction and the treatment device, in which the reaction is supposed to take place. Under this strategy,a knowledge of the reaction pathways, its products, stoichiometry and kinetics is fundamental and, unfortunately, often unavailable from the preliminary knowledge. Therefore, research made in chemistry on novel treatment methods, comprisesnowadays a substantial part of the efforts. Chemical decomposition methods in the aqueous phase include oxidation by ozonation, ozone-associated methods (O3/H2O2, O3/UV, O3/TiO2), Fenton reagent (H2O2/Fe2+/3+) and photocatalytic oxidation (PCO). In the gaseous phase, PCO and catalytic hydrolysis over zero valent ironsare developed. The experimental studies within the described methodology involve aqueous phase oxidation of natural organic matter (NOM) of potable water, phenolic and aromatic amino compounds, ethylene glycol and its derivatives as de-icing agents, and oxygenated motor fuel additives ¿ methyl tert-butyl ether (MTBE) ¿ in leachates and polluted groundwater. Gas-phase chemical decomposition includes PCO of volatile organic compounds and dechlorination of chlorinated methane derivatives. The results of the research summarised here are presented in fifteenattachments (publications and papers submitted for publication and under preparation).

Numerical and ExperimentalModelling of Gas Flow and Heat Transfer in the Air Gap of An Electric Machine

This work deals with the cooling of high-speed electric machines, such as motors and generators, through an air gap. It consists of numerical and experimental modelling of gas flow and heat transfer in an annular channel. Velocity and temperature profiles are modelled in the air gap of a high-speed testmachine. Local and mean heat transfer coefficients and total friction coefficients are attained for a smooth rotor-stator combination at a large velocity range. The aim is to solve the heat transfer numerically and experimentally. The FINFLO software, developed at Helsinki University of Technology, has been used in the flow solution, and the commercial IGG and Field view programs for the grid generation and post processing. The annular channel is discretized as a sector mesh. Calculation is performed with constant mass flow rate on six rotational speeds. The effect of turbulence is calculated using three turbulence models. The friction coefficient and velocity factor are attained via total friction power. The first part of experimental section consists of finding the proper sensors and calibrating them in a straight pipe. After preliminary tests, a RdF-sensor is glued on the walls of stator and rotor surfaces. Telemetry is needed to be able to measure the heat transfer coefficients at the rotor. The mean heat transfer coefficients are measured in a test machine on four cooling air mass flow rates at a wide Couette Reynolds number range. The calculated values concerning the friction and heat transfer coefficients are compared with measured and semi-empirical data. Heat is transferred from the hotter stator and rotor surfaces to the coolerair flow in the air gap, not from the rotor to the stator via the air gap, althought the stator temperature is lower than the rotor temperature. The calculatedfriction coefficients fits well with the semi-empirical equations and precedingmeasurements. On constant mass flow rate the rotor heat transfer coefficient attains a saturation point at a higher rotational speed, while the heat transfer coefficient of the stator grows uniformly. The magnitudes of the heat transfer coefficients are almost constant with different turbulence models. The calibrationof sensors in a straight pipe is only an advisory step in the selection process. Telemetry is tested in the pipe conditions and compared to the same measurements with a plain sensor. The magnitudes of the measured data and the data from the semi-empirical equation are higher for the heat transfer coefficients than thenumerical data considered on the velocity range. Friction and heat transfer coefficients are presented in a large velocity range in the report. The goals are reached acceptably using numerical and experimental research. The next challenge is to achieve results for grooved stator-rotor combinations. The work contains also results for an air gap with a grooved stator with 36 slots. The velocity field by the numerical method does not match in every respect the estimated flow mode. The absence of secondary Taylor vortices is evident when using time averagednumerical simulation.

Measurement of the air permeability profile on SC paper machine

Tämän diplomityön tarkoituksena oli asentaa ja kehittää UPM-Kymmene Rauman tehtaiden PK2:lle luotettava ja toimiva ilmanläpäisyprofiilin mittaus. Työn tarkoituksena oli myös kartoittaa tietoja ilmanläpäisyprofiiliin vaikuttavista seikoista sekä mahdollisuuksista säätää ilmanläpäisyprofiilia. Lisäksi työn tavoitteena oli löytää toimiva menetelmä verrata online mitattua ilmanläpäisyprofiilia laboratoriossa mitattuun ilmanläpäisyprofiiliin online mittauksen luotettavuuden näkökulmasta. Työn aikana selvitettiin myös ilmanläpäisyprofiilin mittauksen mahdollisuutta superkalanteroidusta SC paperista. Työn kirjallisessa osassa käsiteltiin paperin huokoisuutta ja ilmanläpäisyä, huokoisuustasoon ja huokoisuus profiiliin vaikuttavia tekijöitä, ilmanläpäisevyyden merkitystä SC paperin valmistukselle ja SC paperin painettavuudelle sekä ilmanläpäisevyyden laboratorio- sekä online mittausta. Kirjallisessa osassa käsiteltiin myös Honeywellin uutta Poros ilmanläpäisysensoria. Työn kokeellisessa osassa tutkittiin ilmanläpäisyprofiilimittauksen luotettavuutta CD ja MD suunnassa sekä laboratorio- ja online-mittausten välisiä eroavaisuuksia ennen PK2 uusintaa. PK2 uusinnan jälkeen kokeellisessa osassa keskityttiin luotettavuuden varmentamiseen CD ja MD suunnassa sekä kartoittamaan tekijöitä, jotka aiheuttivat pieniä tasoeroja mittausten välillä. Mittaukset todettiin luotettaviksi ja niiden pohjalta suoritettiin mitattujen online profiilien välisiä vertailuja. Ilmanläpäisyprofiililla todettiin olevan positiivinen korrelaatio neliömassaprofiilin ja kosteusprofiilin kanssa sekä negatiivinen korrelaatio tuhkaprofiilin kanssa. PK2 uusinnan yhteydessä tehtiin koeajoja, jotka liittyivät laadunoptimointiin viira- ja puristinosalla. Koeajoissa tutkittujen asioiden lisäksi tutkittiin muutettujen parametrien vaikutusta ilmanläpäisyprofiiliin. Höyrylaatikon vaikutusta ilmanläpäisyprofiiliin tutkittiin säätöjen virityksen yhteydessä.

Improvements in Air Intake on Frame 6 Gas Turbines

Työssä tarkastellaan kahta kaasuturbiinin imuilman sisäänottojärjestelmän kehitysmenetelmää, imuilman jäähdytystä ja sähköstaattista suodatusta. Imuilman jäähdytysmenetelmien tarkastelussa käytettiin kahta kaasuturbiinin tehonlisäystekniikoiden laskentatyökalua. Arviointi kohdistettiin Glanford Brigg Generating Station -voimalaitoksen kaasuturbiinityyppiin ja paikallisiin englantilaisiin ilmasto-olosuhteisiin. Tarkastelussa olivat kostutusjäähdytys ja overspray. Tuloksia vertailtiin keskenään ja näiden perusteella arvioitiin menetelmien vaikutuksia tehoon, hyötysuhteeseen sekä veden kulutukseen. Sähköstaattisen suodattimen prototyyppi oli rakennettu Briggin voimalaitokselle. Järjestelmää kehitetään kaupalliseksi tuotteeksi ja tätä varten kerättiin tekninen dokumentaatio kokonaisuudeksi, jota voitiin hyödyntää tuotteistusprosessissa. Imuilman jäähdyttämisellä voidaan saavuttaa merkittävä tehonlisäys ilmasto-olosuhteista riippuen. Menetelmällä voidaan myös tasata lämpötilan vuorokausi-vaihtelusta aiheutuvia tehoeroja. Sähköstaattisen suodattimen prototyyppi saavutti kehitysvaiheelle asetetut tavoitteet. Sähköstaattinen suodatus tarjoaa useita etuja perinteiseen mekaaniseen suodatukseen verrattuna.

Työpöytäsovellus Adobe Air -tekniikalla

Työn kirjallinen osuus aloitettiin kertaamalla lyhyesti web-sovellukset ja niiden ominaisuudet. Tekniikan kehittyminen on mahdollistanut rikkaat Internet-sovellukset, joiden periaate ja toiminta esitettiin, ja lisäksi perehdyttiin rikkaiden Internet-sovellusten vaatimuksiin. Adobe Air on käyttöjärjestelmäriippumaton ajoympäristö työpöytäsovellusten toteuttamiseen web-tekniikoilla. Air-tekniikkaan tutustuttiin käymällä läpi ajoympäristön tärkeimmät komponentit ja niiden merkitys sekä Air-sovelluksen tietoturvamalli. Air-sovellus voidaan toteuttaa vaihtoehtoisilla sovellustekniikoilla, jotka esitellään lyhyesti ja pohditaan valintaan vaikuttavia ominaisuuksia. Lisäksi esitettiin sovelluskehitykseen tarjolla olevia työkaluja ja Air-sovelluskehityksen ominaispiirteitä.Työssä toteutettiin Asiakasselain-sovellus, jonka on tarkoitus korvata tulevaisuudessa tällä hetkellä käytössä oleva Asiakaspääte-sovellus. Asiakasselaimen avulla asiakas voi etsiä tuotteita ja lisätietoja tavarataloissa. Air-sovelluksen sovellustekniikaksi valittiin HTML/Ajax-tekniikka. Sovellus hyödyntää tavaratalon varasto-tietokantaa sekä verkko-kaupan kuva- ja tuoteinformaatiota. Työn päätavoitteena oli tutustua Adobe Air -tekniikkaan ja sen tarjoamiin mahdollisuuksiin. Air osoittautui mielenkiintoiseksi ja helpoksi vaihtoehdoksi työpöytäsovelluksen toteutta-misessa perinteisillä web-tekniikoilla.

Air de Tancrede avec Variations pour le Piano Forte par Gelinek

Simananniemen käsikirjoituskokoelma.

Air d’armade

Soitinnus: sooloääni. Simananniemen käsikirjoituskokoelma.

Developing service offering of an air freight carrier

The thesis examined service offering development of an air freight carrier from the customers' point of view. The study was limited to the biggest business clients of the carrier. Service offering development can be divided into service concept, process and system. The thesis was based on these three themes and quality. Compared to product development, systematic and well-structured service development has been studied little, especially in business market. However, service development is a current issue. Due to growing competition companies should carefully listen to their clients' needs and respond to them by offering right services. Methodology of the thesis is qualitative and representatives of three forwarding companies were interviewed. It was found out that the forwarding companies consider themselves as partners of the airline. In addition to general reliability, the customers value the most fluent terminal processes and electronic communication.

Life cycle costs in heating, ventilation and air-conditioning systems with drive

Energy consumption and energy efficiency have become an issue. Energy consumption is rising all over the world and because of that, and the climate change, energy is becoming more and more expensive. Buildings are major consumers of energy, and inside the buildings the major consumers are heating, ventilation and air-conditioning systems. They usually run at constant speed without efficient control. In most cases HVAC equipment is also oversized. Traditionally heating, ventilation and air-conditioning systems have been sized to meet conditions that rarely occur. The theory part in this thesis represents the basics of life cycle costs and calculations for the whole life cycle of a system. It also represents HVAC systems, equipment, systems controls and ways to save energy in these systems. The empirical part of this thesis represents life cycle cost calculations for HVAC systems. With these calculations it is possible to compute costs for the whole life cycle for the wanted variables. Life cycle costs make it possible to compare which variable causes most of the costs from the whole life point of view. Life cycle costs were studied through two real life cases which were focused on two different kinds of HVAC systems. In both of these cases the renovations were already made, so that the comparison between the old and the new, now existing system would be easier. The study indicates that energy can be saved in HVAC systems by using variable speed drive as a control method.

Air des Bijoux

Oopperasta Faust.

Theoretical Analysis and Numerical Simulation of Spectral Radiative Properties of Combustion Gases in Oxy/Air-Fired Combustion Systems

Energy efficiency is one of the major objectives which should be achieved in order to implement the limited energy resources of the world in a sustainable way. Since radiative heat transfer is the dominant heat transfer mechanism in most of fossil fuel combustion systems, more accurate insight and models may cause improvement in the energy efficiency of the new designed combustion systems. The radiative properties of combustion gases are highly wavelength dependent. Better models for calculating the radiative properties of combustion gases are highly required in the modeling of large scale industrial combustion systems. With detailed knowledge of spectral radiative properties of gases, the modeling of combustion processes in the different applications can be more accurate. In order to propose a new method for effective non gray modeling of radiative heat transfer in combustion systems, different models for the spectral properties of gases including SNBM, EWBM, and WSGGM have been studied in this research. Using this detailed analysis of different approaches, the thesis presents new methods for gray and non gray radiative heat transfer modeling in homogeneous and inhomogeneous H2O–CO2 mixtures at atmospheric pressure. The proposed method is able to support the modeling of a wide range of combustion systems including the oxy-fired combustion scenario. The new methods are based on implementing some pre-obtained correlations for the total emissivity and band absorption coefficient of H2O–CO2 mixtures in different temperatures, gas compositions, and optical path lengths. They can be easily used within any commercial CFD software for radiative heat transfer modeling resulting in more accurate, simple, and fast calculations. The new methods were successfully used in CFD modeling by applying them to industrial scale backpass channel under oxy-fired conditions. The developed approaches are more accurate compared with other methods; moreover, they can provide complete explanation and detailed analysis of the radiation heat transfer in different systems under different combustion conditions. The methods were verified by applying them to some benchmarks, and they showed a good level of accuracy and computational speed compared to other methods. Furthermore, the implementation of the suggested banded approach in CFD software is very easy and straightforward.

Mikä on air-fligt-periaate?

kuv., 14 x 22 cm

Mikä on air-fligt-periaate?

kuv., 14 x 22 cm