7 resultados para Motor Skill. Work. Potency

em Doria (National Library of Finland DSpace Services) - National Library of Finland, Finland


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Induction motors are widely used in industry, and they are generally considered very reliable. They often have a critical role in industrial processes, and their failure can lead to significant losses as a result of shutdown times. Typical failures of induction motors can be classified into stator, rotor, and bearing failures. One of the reasons for a bearing damage and eventually a bearing failure is bearing currents. Bearing currents in induction motors can be divided into two main categories; classical bearing currents and inverter-induced bearing currents. A bearing damage caused by bearing currents results, for instance, from electrical discharges that take place through the lubricant film between the raceways of the inner and the outer ring and the rolling elements of a bearing. This phenomenon can be considered similar to the one of electrical discharge machining, where material is removed by a series of rapidly recurring electrical arcing discharges between an electrode and a workpiece. This thesis concentrates on bearing currents with a special reference to bearing current detection in induction motors. A bearing current detection method based on radio frequency impulse reception and detection is studied. The thesis describes how a motor can work as a “spark gap” transmitter and discusses a discharge in a bearing as a source of radio frequency impulse. It is shown that a discharge, occurring due to bearing currents, can be detected at a distance of several meters from the motor. The issues of interference, detection, and location techniques are discussed. The applicability of the method is shown with a series of measurements with a specially constructed test motor and an unmodified frequency-converter-driven motor. The radio frequency method studied provides a nonintrusive method to detect harmful bearing currents in the drive system. If bearing current mitigation techniques are applied, their effectiveness can be immediately verified with the proposed method. The method also gives a tool to estimate the harmfulness of the bearing currents by making it possible to detect and locate individual discharges inside the bearings of electric motors.

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The work aims to analyze the possibilities of utilizing old crane driving AC induction motors in modern pulse-width-modulated variable frequency drives. Bearing currents and voltage stresses are the two main problems associated with modern IGBT inverters, and they may cause premature failure of an old induction motor. The origins of these two problems are studied. An analysis of the mechanism of bearing failure is proposed. Certain types of bearing currents are considered in detail. The most effective and economical means are chosen for bearing currents mitigation. Transient phenomena of cables and mechanism of over voltages occurring at motor terminals are studied in the work. The weakest places of the stator winding insulation system are shown and recommendations are given considering the mitigation of voltage stresses. Only the most appropriate and cost effective preventative methods are chosen for old motor drives. Rewinding of old motors is also considered.

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Synchronous machines with an AC converter are used mainly in large drives, for example in ship propulsion drives as well as in rolling mill drives in steel industry. These motors are used because of their high efficiency, high overload capacity and good performance in the field weakening area. Present day drives for electrically excited synchronous motors are equipped with position sensors. Most drives for electrically excited synchronous motors will be equipped with position sensors also in future. This kind of drives with good dynamics are mainly used in metal industry. Drives without a position sensor can be used e.g. in ship propulsion and in large pump and blower drives. Nowadays, these drives are equipped with a position sensor, too. The tendency is to avoid a position sensor if possible, since a sensor reduces the reliability of the drive and increases costs (latter is not very significant for large drives). A new control technique for a synchronous motor drive is a combination of the Direct Flux Linkage Control (DFLC) based on a voltage model and a supervising method (e.g. current model). This combination is called Direct Torque Control method (DTC). In the case of the position sensorless drive, the DTC can be implemented by using other supervising methods that keep the stator flux linkage origin centered. In this thesis, a method for the observation of the drift of the real stator flux linkage in the DTC drive is introduced. It is also shown how this method can be used as a supervising method that keeps the stator flux linkage origin centered in the case of the DTC. In the position sensorless case, a synchronous motor can be started up with the DTC control, when a method for the determination of the initial rotor position presented in this thesis is used. The load characteristics of such a drive are not very good at low rotational speeds. Furthermore, continuous operation at a zero speed and at a low rotational speed is not possible, which is partly due to the problems related to the flux linkage estimate. For operation in a low speed area, a stator current control method based on the DFLC modulator (DMCQ is presented. With the DMCC, it is possible to start up and operate a synchronous motor at a zero speed and at low rotational speeds in general. The DMCC is necessary in situations where high torque (e.g. nominal torque) is required at the starting moment, or if the motor runs several seconds at a zero speed or at a low speed range (up to 2 Hz). The behaviour of the described methods is shown with test results. The test results are presented for the direct flux linkage and torque controlled test drive system with a 14.5 kVA, four pole salient pole synchronous motor with a damper winding and electric excitation. The static accuracy of the drive is verified by measuring the torque in a static load operation, and the dynamics of the drive is proven in load transient tests. The performance of the drive concept presented in this work is sufficient e.g. for ship propulsion and for large pump drives. Furthermore, the developed methods are almost independent of the machine parameters.

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Direct torque control (DTC) is a new control method for rotating field electrical machines. DTC controls directly the motor stator flux linkage with the stator voltage, and no stator current controllers are used. With the DTC method very good torque dynamics can be achieved. Until now, DTC has been applied to asynchronous motor drives. The purpose of this work is to analyse the applicability of DTC to electrically excited synchronous motor drives. Compared with asynchronous motor drives, electrically excited synchronous motor drives require an additional control for the rotor field current. The field current control is called excitation control in this study. The dependence of the static and dynamic performance of DTC synchronous motor drives on the excitation control has been analysed and a straightforward excitation control method has been developed and tested. In the field weakening range the stator flux linkage modulus must be reduced in order to keep the electro motive force of the synchronous motor smaller than the stator voltage and in order to maintain a sufficient voltage reserve. The dynamic performance of the DTC synchronous motor drive depends on the stator flux linkage modulus. Another important factor for the dynamic performance in the field weakening range is the excitation control. The field weakening analysis considers both dependencies. A modified excitation control method, which maximises the dynamic performance in the field weakening range, has been developed. In synchronous motor drives the load angle must be kept in a stabile working area in order to avoid loss of synchronism. The traditional vector control methods allow to adjust the load angle of the synchronous motor directly by the stator current control. In the DTC synchronous motor drive the load angle is not a directly controllable variable, but it is formed freely according to the motor’s electromagnetic state and load. The load angle can be limited indirectly by limiting the torque reference. This method is however parameter sensitive and requires a safety margin between the theoretical torque maximum and the actual torque limit. The DTC modulation principle allows however a direct load angle adjustment without any current control. In this work a direct load angle control method has been developed. The method keeps the drive stabile and allows the maximal utilisation of the drive without a safety margin in the torque limitation.

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This bachelor’s thesis is a part of the research project realized in the summer 2011 in Lappeenranta University of Technology. The goal of the project was to create an automation concept for controlling an electrically excited synchronous motor. This thesis concentrates on the setup and requirements specification part of the concept. The setup consists of ABB AC500 as the PLC master device, DCS800 as an exciter and ACS800 as a frequency converter. The ACS800 frequency converter uses permanent magnet synchronous machine software to control the stator’s magnetic field, the DC drive handles the excitation and the AC500 PLC master controls the communication and functionality of the system. The requirements specification briefly explains the general over-view of the concept, the use and functionality of the PLC program and the requirements needed for the whole concept and the PLC program to work as intended.

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Kirjallisuudesta välittyy useitten vuosikymmenten ajalta tietämys sotilaslentämisen fyysisestä kuormittavuudesta. G-voimista aiheutuva kuormittuminen näyttää johtavan joko akuutisti tai pitkäaikaisesti lentäjän tuki- ja liikuntaelimistön toimintakykyä alentaviin ongelmiin. Erityisesti on selvitetty niskan alueen työperäisten ongelmien syntyä, jolloin on havaittu lentotoiminnan fyysisen kuormittavuuden johtavan ennenaikaiseen rakenteelliseen rappeumaan, haittaa aiheuttavan oireen lisäksi. Kansainvälisen kirjallisuuden mukaan ammatista johtuvista eli työperäisistä oireista kärsii vähintään 2/3 kaikista sotilaslentäjistä. Tietyin edellytyksin lentäjien kaularangan alueen rappeuma on Suomessa hyväksytty ammattitaudiksi vuodesta 1995 alkaen. On arveltu, että hyvästä fyysisestä suorituskyvystä olisi apua tuki- ja liikuntaelin (TULE)-oireilun ennaltaehkäisemisessä ja toimintakyvyn ylläpitämisessä. Tutkimusnäyttö tästä on lentäjien osalta ollut toistaiseksi erittäin niukkaa. Tämän tutkimuksen tavoitteena oli selvittää suomalaisten sotilaslentäjien työperäisen TULE-oireilun esiintyvyyttä, oireista koetun haitan tasoa, lentäjien fyysisen kunnon tasoja virkauran aikana ja näitten kaikkien välisiä yhteyksiä sekä työperäisen TULE-oireen merkitystä sotilaan toimintakykyyn. Tutkimus jakautui kahteen osaan. Poikkileikkauksena lentotoimintaperäisiä TULE-oireita kartoitettiin kyselytutkimuksella, johon vastasi vuositarkastuksen yhteydessä 267 lentäjää vuosina 2004-2005. Joukosta poimittiin ne 195 lentäjää, jotka olivat suorittaneet yleissotilaalliset kuntotestit puolen vuoden sisällä kyselyyn vastaamisesta, ja mitatut testitulokset yhdistettiin kyselytutkimusaineistoon. Tässä aineistossa toteutettiin fyysisesti erilailla kuormittuvien lentäjäryhmien välisiä vertailuja fyysisen kunnon, TULE-esiintyvyyden ja koetun haitan suhteen. Poikkileikkausosassa tutkittiin myös lentäjien virkauran aikaisia tasoeroja yleissotilaallisissa kuntotesteissä (n=195) verrattuna muihin suomalaisiin sotilaisiin. Lisäksi (N=289) selvitettiin ilmailulääketieteellisen tarkastuksen yhteydessä mitattuja, ns. ammatillisia fyysisiä erityisominaisuuksia eri ikäluokissa. Pitkittäisosassa seurattiin 67:n Hawk-suihkuharjoituskoneella aloittaneen Ilmavoimien sotilaslentäjien lentouran aikaista lentotoimintaperäisten TULE-oireitten esiintyvyyttä vuosien 1996 ja 2008 välillä. Lisäksi tutkittiin lentäjien kontakteja työterveyshuoltoon, oireen aiheuttamaa lentokelvottomuusaikaa, työn kuormituksen kumulatiivista kertymää lentotuntien lisääntyessä ja TULE-oireiden esiintyvyyden kannalta kriittisiä ajankohtia lentouran aikana. Tulokset osoittivat, että kaikki seurannassa olleet suomalaiset sotilaslentäjät kokivat jonkinasteisen lentotoimintaperäisen TULE-oireen uransa aikana. Niskan ammattitautiluokituksen tasoisen ongelman esiintyvyys oli 4 % koko lentäjäpopulaatiosta ja 10 % suihkuharjoituskonevaiheen jo läpäisseistä, mutta vastaavanlaisia TULE-ongelmia, ilman riittävää näyttöä ammattitaudista, esiintyi lähes joka kolmannella sotilaslentäjällä. Alaselän osalta lentäjät oireilivat lähes samassa määrin, mutta näitä oireita ei toistaiseksi ole mahdollista määrittää ammattitaudiksi. Lentäjät kävivät varsin vähän valittamassa oireistaan työterveyshuoltoon, jossa käytäneen vasta silloin, kun oire jo selvästi heikentää työtehtävissä vaadittavaa toimintakykyä. Merkittävin lentotoimintaperäisten oireitten esiintymisen kasvu ajoittui 200 Hawk-lentotunnin kohdalle, jolloin koneella saavutetaan eräänlainen optimaalinen G-indeksi eli taktisen liikehtelyn G-tasoylitysten vaihtelu. Tämän jälkeen lentäjät ovat erityisen alttiina akuuteille lennonaikaisille TULE-ongelmille. Oireitten esiintyminen kasvoi eksponentiaalisesti noin 600 lentotuntiin asti. Monimuuttujamallien mukaan työperäisen TULE-oireen esiintyvyysriskiä vähensivät alaraajojen hyvä motoriikka, korkeat valintapisteet ja korkea kaulan fleksion voimataso maksimaalisessa isometrisessä testissä. Yleissotilaallisilla kuntotasoilla ei ollut yhteyttä oireiluun, mutta lihaskunnoltaan voimakkaimmat lentäjät kärsivät tilastollisesti merkittävästi vähemmän haittaa lentotoimintaperäisistä TULE-oireistaan. Yleissotilaallisissa kuntotesteissä lentäjät olivat parempia kuin muut suomalaiset sotilaat. Aktiivisimman lentouran aikana, 30-40-vuotiaina, lentäjien fyysinen suorituskyky oli normaaliväestöön nähden vain keskimääräinen ja urheilijoihin nähden keskimääräistä heikompi. Käytännössä lentäjät eivät kyenneet ylläpitämään valintavaiheen fyysistä suorituskykyään edes kadettivaiheen loppuun asti. Huomattavaa oli lisäksi, että aktiivisen lentouran päätyttyä fyysinen kunto näytti jossain määrin palautuvan kohti lähtötasoa lentäjien ikääntymisestä huolimatta. Lentäjien valintavaiheen aikana mitatun fyysisen suorituskyvyn tason säilyminen aktiivisen lentopalveluksen loppuun asti vaatisi lentäjien fyysisen toimintakyvyn ylläpidon ja kehittämisen tehostamista koulutuksen ja työuran eri vaihessa. Tähän tavoitteeseen nähden Ilmavoimien fyysisen kasvatuksen järjestelyt vaikuttivat alimitoitetuilta. Operatiivisesti huolestuttavaa oli Ilmavoimien ohjaajien fyysisen suorituskyvyn heikentyminen silloin, kun heidän taitojensa puolesta olisi pitänyt olla suorituskykyisimpiä taistelutehtäviinsä. Myös lentäjän terveyttä ja toimintakykyä pitäisi pystyä reaaliaikaisemmin seuraamaan koko lentouran aikana. Ilmavoimille suositellaan moniammatillista lähestymistä sotilaslentäjien toimintakyvyn ylläpitämiseen ja terveysriskien hallintaan yhdessä liikunnan, työterveyshuollon, lentoturvallisuusalan ja operatiivisen suunnittelun asiantuntijoitten kanssa. Lisäksi suositellaan avoimempaa ja eettisesti kestävämpää suhtautumista ammattiin liittyvien terveysongelmien kuvaamiseen sekä fyysisen kunnon kysymyksiin jo lentäjien rekrytointivaiheessa.

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C-Jun N-terminal kinase (JNK) is traditionally recognized as a crucial factor in stress response and inducer of apoptosis upon various stimulations. Three isoforms build the JNK subfamily of MAPK; generally expressed JNK1 and JNK2 and brain specific JNK3. Degenerative potency placed JNK in the spotlight as potential pharmacological option for intervention. Unfortunately, adverse effects of potential drugs and observation that expression of only JNK2 and JNK3 are induced upon stress, restrained initial enthusiasm. Notably, JNK1 demonstrated atypical high constitutive activity in neurons that is not responsive to cellular stresses and indicated existence of physiological activity. This thesis aimed at revealing the physiological functions of JNK1 in actin homeostasis through novel effector MARCKS-Like 1 (MARCKSL1) protein, neuronal trafficking mediated by major kinesin-1 motor protein and microtubule (MT) dynamics via STMN2/SCG10. The screen for novel physiological JNK substrates revealed specific phosphorylation of C-terminal end of MARCKSL1 at S120, T148 and T183 both ex vivo and in vitro. By utilizing site-specific mutagenesis, various actin dynamics and migrations assays we were able to demonstrate that JNK1 phosphorylation specifically facilitates F-actin bundling and thus filament stabilisation. Consecutively, this molecular mechanism was proved to enhance formation of filopodia; cell surface projections that allow cell sensing surrounding environment and migrate efficiently. Our results visualize JNK dependent and MARCKSL1 executed induction of filopodia in neurons and fibroblast indicating general mechanism. Subsequently, inactivation of JNK action on MARCKSL1 shifts cellular actin machinery into lamellipodial dynamic arrangement. Tuning of actin cytoskeleton inevitably melds with cell migration. We observed that both active JNK and JNK pseudo-phosphorylated form of MARCKSL1 reduce actin turnover in intact cells leading to overall diminished cell motility. We demonstrate that tumour transformed cells from breast, prostate, lung and muscle-derived cancers upregulate MARCKSL1. We showed on the example of prostate cancer PC-3 cell line that JNK phosphorylation negatively controls MARCKSL1 ability to induce migration, which precedes cancer cell metastasis. The second round of identification of JNK physiological substrates resulted in detection of predominant motor protein kinesin-1 (Kif5). Mass spectrometry detailed analysis showed evident endogenous phosphorylation of kinesin-1 on S176 within motor domain that interacts with MT. In vitro phosphorylation of bacterially expressed kinesin heavy chain by JNK isoforms displayed higher specificity of JNK1 when compared to JNK3. Since, JNK1 is constitutively active in neurons it signified physiological aspect of kinesin-1 regulation. Subsequent biochemical examination revealed that kinesin-1, when not phosphorylated on JNK site, exhibits much higher affinity toward MTs. Expression of the JNK non-phosphorable kinesin-1 mutant in intact cells as well as in vitro single molecule imaging using total internal reflection fluorescence microscopy indicated that the mutant loses normal speed and is not able to move processively into proper cellular compartments. We identify novel kinesin-1 cargo protein STMN2/SCG10, which along with known kinesin-1 cargo BDNF is showing impaired trafficking when JNK activity is inhibited. Our data postulates that constitutive JNK activity in neurons is crucial for unperturbed physiologically relevant transport of kinesin-1 dependant cargo. Additionally, my work helps to validate another novel physiological JNK1 effector STMN2/SCG10 as determinant of axodendritic neurites dynamics in the developing brain through regulation of MT turnover. We show successively that this increased MT dynamics is crucial during developmental radial migration when brain layering occurs. Successively, we are able to show that introduction of JNK phosphorylation mimicking STMN2/SCG10 S62/73D mutant rescues completely JNK1 genetic deletion migration phenotype. We prove that STMN2/SCG10 is predominant JNK effector responsible for MT depolymerising activity and neurite length during brain development. Summarizing, this work describes identification of three novel JNK substrates MARCKSL1, kinesin-1 and STMN2/SCG10 and investigation of their roles in cytoskeleton dynamics and cargo transport. This data is of high importance to understand physiological meaning of JNK activity, which might have an adverse effect during pharmaceutical intervention aiming at blocking pathological JNK action.