Torque vibration model of axial-flux surface-mounted permanent magnet synchronous machine

In order that the radius and thus ununiform structure of the teeth and otherelectrical and magnetic parts of the machine may be taken into consideration the calculation of an axial flux permanent magnet machine is, conventionally, doneby means of 3D FEM-methods. This calculation procedure, however, requires a lotof time and computer recourses. This study proves that also analytical methods can be applied to perform the calculation successfully. The procedure of the analytical calculation can be summarized into following steps: first the magnet is divided into slices, which makes the calculation for each section individually, and then the parts are submitted to calculation of the final results. It is obvious that using this method can save a lot of designing and calculating time. Thecalculation program is designed to model the magnetic and electrical circuits of surface mounted axial flux permanent magnet synchronous machines in such a way, that it takes into account possible magnetic saturation of the iron parts. Theresult of the calculation is the torque of the motor including the vibrations. The motor geometry and the materials and either the torque or pole angle are defined and the motor can be fed with an arbitrary shape and amplitude of three-phase currents. There are no limits for the size and number of the pole pairs nor for many other factors. The calculation steps and the number of different sections of the magnet are selectable, but the calculation time is strongly depending on this. The results are compared to the measurements of real prototypes. The permanent magnet creates part of the flux in the magnetic circuit. The form and amplitude of the flux density in the air-gap depends on the geometry and material of the magnetic circuit, on the length of the air-gap and remanence flux density of the magnet. Slotting is taken into account by using the Carter factor in the slot opening area. The calculation is simple and fast if the shape of the magnetis a square and has no skew in relation to the stator slots. With a more complicated magnet shape the calculation has to be done in several sections. It is clear that according to the increasing number of sections also the result will become more accurate. In a radial flux motor all sections of the magnets create force with a same radius. In the case of an axial flux motor, each radial section creates force with a different radius and the torque is the sum of these. The magnetic circuit of the motor, consisting of the stator iron, rotor iron, air-gap, magnet and the slot, is modelled with a reluctance net, which considers the saturation of the iron. This means, that several iterations, in which the permeability is updated, has to be done in order to get final results. The motor torque is calculated using the instantaneous linkage flux and stator currents. Flux linkage is called the part of the flux that is created by the permanent magnets and the stator currents passing through the coils in stator teeth. The angle between this flux and the phase currents define the torque created by the magnetic circuit. Due to the winding structure of the stator and in order to limit the leakage flux the slot openings of the stator are normally not made of ferromagnetic material even though, in some cases, semimagnetic slot wedges are used. In the slot opening faces the flux enters the iron almost normally (tangentially with respect to the rotor flux) creating tangential forces in the rotor. This phenomenon iscalled cogging. The flux in the slot opening area on the different sides of theopening and in the different slot openings is not equal and so these forces do not compensate each other. In the calculation it is assumed that the flux entering the left side of the opening is the component left from the geometrical centre of the slot. This torque component together with the torque component calculated using the Lorenz force make the total torque of the motor. It is easy to assume that when all the magnet edges, where the derivative component of the magnet flux density is at its highest, enter the slot openings at the same time, this will have as a result a considerable cogging torque. To reduce the cogging torquethe magnet edges can be shaped so that they are not parallel to the stator slots, which is the common way to solve the problem. In doing so, the edge may be spread along the whole slot pitch and thus also the high derivative component willbe spread to occur equally along the rotation. Besides forming the magnets theymay also be placed somewhat asymmetric on the rotor surface. The asymmetric distribution can be made in many different ways. All the magnets may have a different deflection of the symmetrical centre point or they can be for example shiftedin pairs. There are some factors that limit the deflection. The first is that the magnets cannot overlap. The magnet shape and the relative width compared to the pole define the deflection in this case. The other factor is that a shifting of the poles limits the maximum torque of the motor. If the edges of adjacent magnets are very close to each other the leakage flux from one pole to the other increases reducing thus the air-gap magnetization. The asymmetric model needs some assumptions and simplifications in order to limit the size of the model and calculation time. The reluctance net is made for symmetric distribution. If the magnets are distributed asymmetrically the flux in the different pole pairs will not be exactly the same. Therefore, the assumption that the flux flows from the edges of the model to the next pole pairs, in the calculation model from one edgeto the other, is not correct. If it were wished for that this fact should be considered in multi-pole pair machines, this would mean that all the poles, in other words the whole machine, should be modelled in reluctance net. The error resulting from this wrong assumption is, nevertheless, irrelevant.

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.

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.

Computational and Experimental Investigation of the Grooved Roll in Paper Machine Environment

In the paper machine, it is not a desired feature for the boundary layer flows in the fabric and the roll surfaces to travel into the closing nips, creating overpressure. In this thesis, the aerodynamic behavior of the grooved roll and smooth rolls is compared in order to understand the nip flow phenomena, which is the main reason why vacuum and grooved roll constructions are designed. A common method to remove the boundary layer flow from the closing nip is to use the vacuum roll construction. The downside of the use of vacuum rolls is high operational costs due to pressure losses in the vacuum roll shell. The deep grooved roll has the same goal, to create a pressure difference over the paper web and keep the paper attached to the roll or fabric surface in the drying pocket of the paper machine. A literature review revealed that the aerodynamic functionality of the grooved roll is not very well known. In this thesis, the aerodynamic functionality of the grooved roll in interaction with a permeable or impermeable wall is studied by varying the groove properties. Computational fluid dynamics simulations are utilized as the research tool. The simulations have been performed with commercial fluid dynamics software, ANSYS Fluent. Simulation results made with 3- and 2-dimensional fluid dynamics models are compared to laboratory scale measurements. The measurements have been made with a grooved roll simulator designed for the research. The variables in the comparison are the paper or fabric wrap angle, surface velocities, groove geometry and wall permeability. Present-day computational and modeling resources limit grooved roll fluid dynamics simulations in the paper machine scale. Based on the analysis of the aerodynamic functionality of the grooved roll, a grooved roll simulation tool is proposed. The smooth roll simulations show that the closing nip pressure does not depend on the length of boundary layer development. The surface velocity increase affects the pressure distribution in the closing and opening nips. The 3D grooved roll model reveals the aerodynamic functionality of the grooved roll. With the optimal groove size it is possible to avoid closing nip overpressure and keep the web attached to the fabric surface in the area of the wrap angle. The groove flow friction and minor losses play a different role when the wrap angle is changed. The proposed 2D grooved roll simulation tool is able to replicate the grooved aerodynamic behavior with reasonable accuracy. A small wrap angle predicts the pressure distribution correctly with the chosen approach for calculating the groove friction losses. With a large wrap angle, the groove friction loss shows too large pressure gradients, and the way of calculating the air flow friction losses in the groove has to be reconsidered. The aerodynamic functionality of the grooved roll is based on minor and viscous losses in the closing and opening nips as well as in the grooves. The proposed 2D grooved roll model is a simplification in order to reduce computational and modeling efforts. The simulation tool makes it possible to simulate complex paper machine constructions in the paper machine scale. In order to use the grooved roll as a replacement for the vacuum roll, the grooved roll properties have to be considered on the basis of the web handling application.

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

Air policing turvallisuuspoliittisena kysymyksenä Suomessa

Tutkimuksessa tarkastellaan air policingia turvallisuuspoliittisena kysymyksenä Suomessa, Islannin ilmavalvontahankkeen kautta. Tavoitteena oli selvittää Islannin ilmavalvonnasta käydyn julkisen keskustelun perusteella, miten air policing näyttäytyy Suomen turvallisuuspolitiikassa. Air policingilla tarkoitetaan vieraan suvereenin valtion ilmatilan koskemattomuuden valvontaa ja turvaamista rauhan aikana. Suomen turvallisuuspolitiikassa air policing on aiemmin käyttämätön työväline. Tutkimuksessa analysoitiin Suomessa käytyä julkista keskustelua Islannin ilmavalvonnasta. Keskustelua tutkittiin puolustusvoimien lakisääteisten tehtävien ja Suomen sotilaallisen liittoutumattomuuden näkökulmista. Tarkastelujen perusteella tehtiin johtopäätöksiä air policingista Suomen turvallisuuspoliittisena kysymyksenä. Tutkimuksen aineisto koostui Islannin ilmavalvontaa käsittelevistä Helsingin Sanomien, Uuden Suomen, Kylkiraudan ja Sotilasaikakauslehden kirjoituksista, eduskunnan täysistuntojen pöytäkirjoista sekä keskeisten turvallisuuspoliittisten päättäjien lausunnoista. Tarkasteltava ajanjakso oli vuoden 2009 alusta vuoden 2012 loppuun. Tutkimusmenetelmä oli sisällönanalyysi. Islannin ilmavalvonnasta käyty julkinen keskustelu koostui lyhyestä jaksosta vuonna 2009 sekä vilkkaasta ja laaja-alaisesta keskustelusta vuonna 2012. Tärkeimpiä sisältöteemoja olivat Nato ja Suomen liittoutumattomuus sekä pohjoismainen yhteistyö. Keskustelussa muodostui vastakkainasettelu, jossa toinen mielipide kannatti ja toinen vastusti Suomen osallistumista Islannin ilmavalvontaan. Puolustusvoimien lakisääteisiä tehtäviä käsiteltiin julkisuudessa vähän. Sen sijaan Suomen sotilaallinen liittoutumattomuus oli keskustelun ytimessä. Islannin ilmavalvontahankkeen kriitikot katsoivat osallistumisen vaarantavan Suomen liittoutumattomuuden Islannin Nato-jäsenyyden vuoksi. Hankkeen kannattajat perustelivat osallistumisen olevan osan tiivistyvää pohjoismaista puolustusyhteistyötä. Suomen ylin turvallisuuspoliittinen johto on ollut valmis ottamaan käyttöön air policingin Islannin ilmavalvontahankkeen yhteydessä. Kysymys on osoittautunut poliittisesti vaikeaksi, eikä konsensusta ole saavutettu. Maaliskuussa 2013 näyttää siltä, että mahdollinen osallistuminen Islannin ilmavalvontaan toteutuu harjoitusmuotoisena, jolloin siinä ei ole kyse varsinaisesta air policingista.