The trend of modern turbomachines towards lighter and slimmer blades exposed to higher loadings has made forced response problems emerge as a major concern in the design process of these machines. Forced response accounts for unsteady forces on the blade due to non-uniformities in the flow field. The clocking method, which consists in this case in changing the relative circumferential position between two consecutive stator blade rows, represents a possibility to reduce the excitation level of the blade’s natural modes. The goal of this investigation was to analyze the influence of the clocking method on a transonic compressor in order to find an optimum regarding aerodynamic forcing. The investigation was carried out in three parts. The first consisted in a computational fluid dynamics analysis which aimed at calculating the unsteady forces acting on the blades. The second consisted in a finite element analysis with the purpose of obtaining the mode shapes of the dangerous natural modes of the blades. In third part, the two analyses were coupled in order to evaluate the excitation level of the blades for seven equally-spaced clocking cases that covered a complete circumferential pitch. The results revealed that changing the circumferential position of the inlet guide vane with respect to the first stator blade row can reduce the excitation level of the rotor blade row in between by more than 50 percent and of the stator blade row by about 30 percent. Variations of the force distribution affecting sensible zones of the blade were detected, which explains the changes for the different clocking positions. An optimal clocking position was proposed regarding minimum excitation levels of the critical modes. Keywords: turbomachine, forced response, unsteady forces, clocking

<p>Today’s microprocessors with millions of transistors perform high-complexity computing at multi-gigahertz clock frequencies. The ever-increasing chip size and speed call for new methodologies in clock distribution network. Conventional global synchronization techniques exhibit many drawbacks in the advanced VLSI chips such as high-speed microprocessors. A significant percentage of the total power consumption in a microprocessor is dissipated in the clock distribution network. Also since the chip dimensions increase, clock skew management becomes very challenging in the framework of conventional methodology. Long interconnect delays limit the maximum clock frequency and become a bottleneck for future microprocessor design. In such a situation, new alternative techniques for synchronization in system-on-chip are demanded.</p><p>This thesis presents new alternatives for traditional clocking and synchronization methods, in which, speed and power consumption bottlenecks are treated. For this purpose, two new techniques based on mesochronous synchronization and resonant clocking are investigated. The mesochronous synchronization technique deals with remedies for skew and delay management. Using this technique, clock frequency up to 5 GHz for on-chip communication is achievable in 0.18-<em>μ</em>m CMOS process. On the other hand the resonant clocking solves significant power dissipation problem in the clock network. This method shows a great potential in power saving in very large-scale integrated circuits. According to measurements, 2.3X power saving in clock distribution network is achieved in 130-nm CMOS process. In the resonant clocking, oscillator plays a crucial role as a clock generator. Therefore an investigation about oscillators and possible techniques for jitter and phase noise reduction in clock generators has been done in this research framework. For this purpose a study of injection locking phenomenon in ring oscillators is presented. This phenomenon can be used as a jitter suppression mechanism in the oscillators. Also a new implementation of the DLL-based clock generators using ring oscillators is presented in 130-nm CMOS process. The measurements show that this structure operates in the frequency range of 100 MHz-1.5 GHz, and consumes less power and area compared to the previously reported structures. Finally a new implementation of a 1.8-GHz quadrature oscillator with wide tuning range is presented. The quadrature oscillators potentially can be used as future clock generators where multi-phase clock is needed.</p> / Report code: LiU-TEK-LIC-2006:22

The Smartphone revolution and the Internet of Things (IoTs) have triggered rapid advances in complex system-on-chips (SoCs) that increasing provide more functionality within a tight power budget. Highly power efficient on die switched-capacitor voltage regulators suffer from large output voltage ripple preventing their widespread use in modern integrated circuits. With technology scaling and increasing architectural complexity, the number of transistors switching in a power domain is growing rapidly leading to major issues with respect to voltage noise. The large voltage and frequency guard-bands present in current microprocessor designs to combat voltage noise both degrade the performance and erode the energy efficiency of the design. In an effort to reduce guard-bands, adaptive clocking based systems combat the problem of voltage noise by adjusting the clock frequency during a voltage droop to avoid timing failure. This thesis presents an integrated power management and clocking scheme that utilizes clock-data compensation to achieve adaptive clocking. The design is capable of automatically con figuring the supply voltage given a target clock frequency for the load circuit. Furthermore, during a voltage droop the design adjusts clock frequency to meet critical path timing margins while simultaneously increasing the current delivered to the load to recover from the droop. The design was implemented in IBM's 130nm technology and simulation results show that the design is able to clock the load circuit from 30 MHz to 800 Mhz with current efficiencies as high as 97%.

Dr. Paul V. Gratz Network-on-Chip (NoC) designs have emerged as a replacement for traditional shared-bus designs for on-chip communications. As with all current VLSI design, however, reducing power consumption in NoCs is a critical challenge. One approach to reduce power is to dynamically scale the voltage and frequency of each network node or groups of nodes (DVFS). Another approach to reduce power consumption is to replace the balanced clock tree with a globally-asynchronous, locally-synchronous (GALS) clocking scheme. NoCs implemented with either of these schemes, however, tend to have high latencies as packets must be synchronized at the intermediate nodes between source and destination. In this work, we propose a novel router microarchitecture which offers superior performance versus typical synchroniz- ing router designs. Our approach features Asynchronous Bypass Channels (ABCs) at intermediate nodes thus avoiding synchronization delay. We also propose a new network topology and routing algorithm that leverage the advantages of the bypass channel offered by our router design. Our experiments show that our design improves the performance of a conventional synchronizing design with similar resources by up to 26 percent at low loads and increases saturation throughput by up to 50 percent.

This thesis includes two topics. The first topic is a CMOS SRAM using dynamic threshold voltage wordline-transistors, which is focused on high speed applications. The second one is a high voltage generator for FLASH memories. The generated high voltages are applied to the wordline controlled transistors during access and verification operations. By taking advantage of the large current provided by low Vth and low leakage current provided by high Vth, a CMOS SRAM using dynamic threshold voltage wordline transistors is presented. The design of a 4-Kb SRAM is measured to possess a 2.2 ns access time, and consume 43.6 mW in the standby mode. The highest operating clock rate is estimated to be 667 MHz. A high voltage generator using 4 clocks with two phases is presented to provide a high voltage supply required by FLASH memories during programming mode and erase mode operations. The circuit is implemented by TSMC 0.25um 1P5M CMOS process. It can provide as high as +11.7 V and -11.6 V by given VDD=2.5 V.

Due to more and more aggressive designs in turbomachinery, assuring the structural integrity of its components has become challenging. Also influenced by this trend is blade design, where lighter and slimmer blades, in combination with higher loading, lead to an increased risk of failure, e.g. in the form of blade vibration. Methods have been proposed to reduce vibration amplitudes for subsonic engines, but cannot directly be applied to transonic regimes due to the additional physical phenomena involved. Therefore the present work investigates numerically the influence of two methods for reducing blade vibration amplitudes in transonic turbomachines, namely varying the blade count ratio and clocking. As it is known that clocking affects the efficiency, the concurrent effects on vibration amplitudes and efficiency are analyzed and discussed in detail. For the computational investigations, the proprietary Fortran-based non-linear, viscous 3D-CFD solver VolSol is applied on two transonic compressor cases and one transonic turbine case. In order to reduce calculation time and to generate the different blade count ratios a scaling technique is applied. The first and main part of this work focuses on the influence of the reduction techniques on aerodynamic forcing. Both the change in blade count ratio and clocking position are found to have significant potential for reducing aerodynamic force amplitudes. Manipulation of the phasing of excitation sources is found herein to be a major contributor to the amplitude variation. The lowest stimulus results are achieved for de-phased excitation sources and results in multiple blade force peaks per blade passing. In the case of blade count ratio variation it was found that blockage for high blade count ratios and the change in potential field size have significant impacts on the blade forcing. For the clocking investigation, three additional operating points and blade count ratios are analyzed and prove to have an impact on the force reduction achievable by clocking. The second part of the work evaluates the influence of clocking on the efficiency of a transonic compressor. It is found that the efficiency can be increased, but the magnitude of the change and the optimal wake impingement location depend on the operating point. Moreover it is shown that optimal efficiency and aerodynamic forcing settings are not directly related. In order to approximate the range of changes of both parameters, an ellipse approximation is suggested. / <p>QC 20130911</p> / TURBOPOWER

The gas turbine has an important role for the energy distribution due to its stability and flexibility. By increasing turbine inlet temperature (TIT) an increased thermal efficiency of the turbine can be achieved. The biggest limitation of the TIT is the material of the turbine components. To avoid this limitation, cooling is needed in the first stages of the turbine by air from the compressor. The downside of the cooling is the decrease of efficiency with excess of cooling air. To achieve an optimum cooling flow, the designing process is important. One major tool in the designing process is simulations by Computational Fluid Dynamics (CFD). For optimum and correct cooling design, the CFD simulations needs to accurate predict the temperature transport through the turbine. Therefore, this study focused to estimate the accuracy of different CFD methods in predicting the temperature distribution through a 1.5 stage turbine with experimental results. The CFD simulations were done by using Ansys CFX and divided into two study cases with steady RANS. One with different turbulence models;  –, Wilcox –  and SST – . The other with two different simulation approaches of interfaces for frame change; Mixing plane and Frozen rotor. All simulations included two configurations of swirlers clocking for interest of their differences within the turbine and validation of the CFD simulations; Passage (PA) and Leading Edge (LE) clockings. The experimental results showed a formation of gradually more uniformed temperature profile with the fluid. This could not be seen in the same extend with any of the simulations. The temperature difference between the hot and cold section with all simulations were marginally decreased in comparison of the measurements. All results with steady RANS simulations tended to over and under predict the temperatures of the hot respectively cold sections within the fluid flow through the turbine. This occurred already after the first stage guide vanes and the difference from the measurements increased after the first stage rotor. This since the steady RANS tended to under predict the mixing process through the turbine. Differences between the turbulence models were noticeable after the rotor blades, where the   – turbulence model predicted most mixing of the evaluated turbulence models but badly compared to the measurements. Another outcome from this study was that the frozen rotor interface with several positions of the rotor blades did not stated better results compared to mixing plane interface for temperature distribution in axial turbines. On the other hand, one simulation of one position of the rotor with frozen rotor interface could be used to simulate an approximatively similar circumferential average temperature as the mixing plane with better convergence with the disadvantage of bigger domain. The gas turbine has an important role for the energy distribution due to its stability and flexibility. By increasing turbine inlet temperature (TIT) an increased thermal efficiency of the turbine can be achieved. The biggest limitation of the TIT is the material of the turbine components. To avoid this limitation, cooling is needed in the first stages of the turbine by air from the compressor. The downside of the cooling is the decrease of efficiency with excess of cooling air. To achieve an optimum cooling flow, the designing process is important. One major tool in the designing process is simulations by Computational Fluid Dynamics (CFD). For optimum and correct cooling design, the CFD simulations needs to accurate predict the temperature transport through the turbine. Therefore, this study focused to estimate the accuracy of different CFD methods in predicting the temperature distribution through a 1.5 stage turbine with experimental results. The CFD simulations were done by using Ansys CFX and divided into two study cases with steady RANS. One with different turbulence models;  –, Wilcox –  and SST – . The other with two different simulation approaches of interfaces for frame change; Mixing plane and Frozen rotor. All simulations included two configurations of swirlers clocking for interest of their differences within the turbine and validation of the CFD simulations; Passage (PA) and Leading Edge (LE) clockings. The experimental results showed a formation of gradually more uniformed temperature profile with the fluid. This could not be seen in the same extend with any of the simulations. The temperature difference between the hot and cold section with all simulations were marginally decreased in comparison of the measurements. All results with steady RANS simulations tended to over and under predict the temperatures of the hot respectively cold sections within the fluid flow through the turbine. This occurred already after the first stage guide vanes and the difference from the measurements increased after the first stage rotor. This since the steady RANS tended to under predict the mixing process through the turbine. Differences between the turbulence models were noticeable after the rotor blades, where the   – turbulence model predicted most mixing of the evaluated turbulence models but badly compared to the measurements. Another outcome from this study was that the frozen rotor interface with several positions of the rotor blades did not stated better results compared to mixing plane interface for temperature distribution in axial turbines. On the other hand, one simulation of one position of the rotor with frozen rotor interface could be used to simulate an approximatively similar circumferential average temperature as the mixing plane with better convergence with the disadvantage of bigger domain. / Gasturbinen har en viktig roll i nutida och framtida energidistribution för elektricitet på grund av dess stabilitet samt flexibilitet. Genom att öka temperaturen in till turbinen ökar den termiska effektiviteten. Den största begränsning av denna temperaturökning är materialen av komponenterna i turbinen. För att kringgå detta används kylning i turbinen med luft från kompressorn. Effektiviteten kan däremot minskas vid överdriven användning av kylluft och därav är designen av kylningen viktig för optimal användning av kylluft. Ett verktyg som oftast används vid design av turbiner är simuleringar med Computational Fluid Dynamics (CFD). För att uppnå en optimal design av kylningen behöver CFD simuleringarna korrekt prediktera temperaturtransporten genom turbinen. Därför fokuserade denna studie på att uppskatta och validera olika CFD metoders förmåga att prediktera temperaturtransporten genom en 1,5 stegs axiell turbin med experimentella resultat. Stationära CFD simuleringar gjordes med RANS av olika turbulensmodeller; k – ε, Wilcox k – ω and SST k – ω. Dessutom jämfördes två olika sätt att simulera gränssnittet mellan stationära och roterande domän; Mixing plane och Frozen rotor. Samtliga simuleringsmetoder inkluderade två olika konfigurationer av virvlarepositioner; Passage (PA) och Leading edge (LE) klockningar. Experimentella resultat visade en stegvis mer enhetlig temperaturprofil med fluidflödet genom turbinen. Detta sågs dock inte i samma utsträckning i någon av simuleringarna. Temperaturskillnaden mellan de varma och kalla stråken i samtliga simuleringar minskade marginellt i jämförelse med de experimentella resultaten. Samtliga resultat med stationära RANS simuleringar tenderade att över och under prediktera temperaturen av de varma respektive kalla stråken. Detta inträffade redan efter förstastegsledskenorna, där skillnaden från de uppmätta temperaturerna ökade över första stegs rotor. Detta på grund av att mixningen i fluiden under predikterades. Skillnader mellan de olika turbulensmodellerna var synliga efter första stegs rotor där  – turbulensmodell predikterade mest mixning av samtliga simuleringar av turbulensmodeller. Däremot predikterade den marginellt bättre i jämförelse med mätningarna. Andra resultat från denna studie var att gränssnittet med frozen rotor med flera positioner inte anger bättre mixning av fluiden genom rotordomänen än vad gränssnittet med mixing plane där liknande radiella temperaturprofiler fås. Däremot gav en simulering med en position av rotorn liknande resultat med radiellt fördelade temperaturer som mixing plan och skulle kunna användas för approximativa simuleringar med bättre konvergens.

As memory I/O bandwidth continues to increase beyond the current multi-gigabit rates for high performance computer systems, there remains a need for a stable and robust method of clock synchronization capable of transferring data reliability between main memory and a CPU memory controller. A Delay Locked Loop (DLL) is often utilized in such a system where synchronization and removal of clock skew are necessary. Synchronization in DLL’s is carried out by continually adjusting the phase of a clock signal by adding or removing delay based on feedback provided by a Phase Detector (PD). Once phase alignment occurs, the DLL is said to be in a “Locked” state. Delay can be produced with either a VCDL (Voltage Controlled Delay Line), or a DCDL (Digitally Controlled Delay Line). Each type of delay line has their own benefits and drawbacks, many of which will be discussed throughout this paper. This thesis provides an overview of previous DLL design research, and presents a functional 45nm CMOS, 200-833 MHz delay locked loop.

Ziel dieser Arbeit war, die Auswirkungen von Clocking der Leitreihen eines mehrstufigen Axialverdichters auf Potentiale hinsichtlich der Beeinflussung instationärer und stationärer Effekte zu untersuchen und zum grundlegenden Verständnis der instationären Schaufelinteraktion beizutragen. Dazu wurden über 2000 Leitgitterkonfigurationen vermessen, so dass der Einfluss von Clocking auf den Wirkungsgrad entlang der Kennlinie bei Auslegungsdrehzahl, auf die Schaufelgrenzschichten und auf die Betriebsgrenzen untersucht und dokumentiert werden konnte. Vor allem wurde so eine erhebliche Beeinflussung der Pumpgrenze gefunden, während das Grenzschichtverhalten auf den Schaufeln und der Wirkungsgrad im praktisch relevanten Bereich der Kennlinie kaum verändert wurden. Hauptgegenstand der Untersuchungen war aber der Einfluss von Stator-Clocking auf die instationären Druckverteilungen und die resultierenden instationären Erregerkräfte an den Lauf- und Leitschaufeln. Die Vermessung der Auswirkungen der Positionierung jedes einzelnen Leitgitters wurde genutzt, um durch eine einfache Optimierung zwei geometrische Konfigurationen aller Leitgitter zu entwickeln. Die eine Konfiguration führte zu geringen aerodynamischen Erregerkräften an den Laufschaufeln aller Stufen, während die andere Konfiguration eine gleichmäßig hohe instationäre Anregung zur Folge hatte. Die Unterschiede der instationären Erregerkräfte zwischen den Konfigurationen waren erheblich und über weite Bereiche der Kennlinie unabhängig vom Betriebspunkt, ohne das die Konfiguration der Leitgitter geändert wurde. Für eine umfassende Analyse der periodisch instationären, aerodynamischen Schaufelinteraktion wurden sowohl die Schaufeldruckverteilungen, als auch das Strömungsfeld in den axialen Schaufelzwischenräumen im Mittelschnitt der Beschaufelung für beide Clocking-Konfigurationen zeitgenau vermessen und vergleichend ausgewertet. Aus diesen Analysen konnte mithilfe der Wellenmechanik eine einfache analytische Beschreibung der instationären Interaktion der Potentialfelder der Beschaufelung entwickelt werden. Für eine einzelne Stufe wurde mit diesem Modell die experimentell bestimmte Phasendifferenz der Druckschwankungen auf Druck- und Saugseite auf sehr einfache Weise nachgewiesen. Damit liegt ein einfaches, analytisches Modell für die Beschreibung der komplexen Überlagerung der sich relativ zueinander bewegenden Druckfelder der Beschaufelung axialer Turbomaschinen vor, das für das physikalische Verständnis der instationären Schaufelinteraktion einen wertvollen Beitrag liefert.

Ziel dieser Arbeit war, die Auswirkungen von Clocking der Leitreihen eines mehrstufigen Axialverdichters auf Potentiale hinsichtlich der Beeinflussung instationärer und stationärer Effekte zu untersuchen und zum grundlegenden Verständnis der instationären Schaufelinteraktion beizutragen. Dazu wurden über 2000 Leitgitterkonfigurationen vermessen, so dass der Einfluss von Clocking auf den Wirkungsgrad entlang der Kennlinie bei Auslegungsdrehzahl, auf die Schaufelgrenzschichten und auf die Betriebsgrenzen untersucht und dokumentiert werden konnte. Vor allem wurde so eine erhebliche Beeinflussung der Pumpgrenze gefunden, während das Grenzschichtverhalten auf den Schaufeln und der Wirkungsgrad im praktisch relevanten Bereich der Kennlinie kaum verändert wurden. Hauptgegenstand der Untersuchungen war aber der Einfluss von Stator-Clocking auf die instationären Druckverteilungen und die resultierenden instationären Erregerkräfte an den Lauf- und Leitschaufeln. Die Vermessung der Auswirkungen der Positionierung jedes einzelnen Leitgitters wurde genutzt, um durch eine einfache Optimierung zwei geometrische Konfigurationen aller Leitgitter zu entwickeln. Die eine Konfiguration führte zu geringen aerodynamischen Erregerkräften an den Laufschaufeln aller Stufen, während die andere Konfiguration eine gleichmäßig hohe instationäre Anregung zur Folge hatte. Die Unterschiede der instationären Erregerkräfte zwischen den Konfigurationen waren erheblich und über weite Bereiche der Kennlinie unabhängig vom Betriebspunkt, ohne das die Konfiguration der Leitgitter geändert wurde. Für eine umfassende Analyse der periodisch instationären, aerodynamischen Schaufelinteraktion wurden sowohl die Schaufeldruckverteilungen, als auch das Strömungsfeld in den axialen Schaufelzwischenräumen im Mittelschnitt der Beschaufelung für beide Clocking-Konfigurationen zeitgenau vermessen und vergleichend ausgewertet. Aus diesen Analysen konnte mithilfe der Wellenmechanik eine einfache analytische Beschreibung der instationären Interaktion der Potentialfelder der Beschaufelung entwickelt werden. Für eine einzelne Stufe wurde mit diesem Modell die experimentell bestimmte Phasendifferenz der Druckschwankungen auf Druck- und Saugseite auf sehr einfache Weise nachgewiesen. Damit liegt ein einfaches, analytisches Modell für die Beschreibung der komplexen Überlagerung der sich relativ zueinander bewegenden Druckfelder der Beschaufelung axialer Turbomaschinen vor, das für das physikalische Verständnis der instationären Schaufelinteraktion einen wertvollen Beitrag liefert.