Control Valve Sizing Theory, Cavitation, Flashing Noise, Flashing and Cavitation Valve Pressure Recovery Factor
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The Role of MHD Turbulence in Magnetic Self-Excitation in The
THE ROLE OF MHD TURBULENCE IN MAGNETIC SELF-EXCITATION: A STUDY OF THE MADISON DYNAMO EXPERIMENT by Mark D. Nornberg A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Physics) at the UNIVERSITY OF WISCONSIN–MADISON 2006 °c Copyright by Mark D. Nornberg 2006 All Rights Reserved i For my parents who supported me throughout college and for my wife who supported me throughout graduate school. The rest of my life I dedicate to my daughter Margaret. ii ACKNOWLEDGMENTS I would like to thank my adviser Cary Forest for his guidance and support in the completion of this dissertation. His high expectations and persistence helped drive the work presented in this thesis. I am indebted to him for the many opportunities he provided me to connect with the world-wide dynamo community. I would also like to thank Roch Kendrick for leading the design, construction, and operation of the experiment. He taught me how to do science using nothing but duct tape, Sharpies, and Scotch-Brite. He also raised my appreciation for the artistry of engineer- ing. My thanks also go to the many undergraduate students who assisted in the construction of the experiment, especially Craig Jacobson who performed graduate-level work. My research partner, Erik Spence, deserves particular thanks for his tireless efforts in modeling the experiment. His persnickety emendations were especially appreciated as we entered the publi- cation stage of the experiment. The conversations during our morning commute to the lab will be sorely missed. I never imagined forging such a strong friendship with a colleague, and I hope our families remain close despite great distance. -
New Developments in Pneumatic Valve Technology for Packaging Applications
TechnicalPaper New developments in pneumatic valve technology for packaging applications Pneumatics is widely used in many packaging machines to drive motion and actuate machine sequences. It is a clean, reliable, compact and lightweight technology that provides a cost-effective solution to help packaging machine designers create innovative systems while staying competitive. Advances in pneumatic valves enable packaging machines like this Manifold valve technology plays a central role in the performance and cartoner to use pneumatics more efficiently and help machine builders effectiveness of pneumatic systems. Recent developments in this create innovative folding configurations to satisfy market needs. technology have increased their flexibility, their modularity and their ability to integrate with and be controlled by the advanced communication bus architectures that are preferred by leading Several factors continue to make pneumatics broadly appealing to packaging machine OEMs and end users, enhancing the application machine builders in the packaging industry. One is cost of ownership: value pneumatic technology supplies. Not only are most pneumatic components relatively low-cost to begin Pneumatics-driven packaging applications Pneumatics can be particularly effective for any kind of machine motion that combines or includes high-speed, point-to-point movement AVENTICS AV valve system – of the types of products with the weight and size dimensions typically found in packaging machines. This includes indexing, sorting and advantages at -
Poppet Valve
POPPET VALVE A poppet valve is a valve consisting of a hole, usually round or oval, and a tapered plug, usually a disk shape on the end of a shaft also called a valve stem. The shaft guides the plug portion by sliding through a valve guide. In most applications a pressure differential helps to seal the valve and in some applications also open it. Other types Presta and Schrader valves used on tires are examples of poppet valves. The Presta valve has no spring and relies on a pressure differential for opening and closing while being inflated. Uses Poppet valves are used in most piston engines to open and close the intake and exhaust ports. Poppet valves are also used in many industrial process from controlling the flow of rocket fuel to controlling the flow of milk[[1]]. The poppet valve was also used in a limited fashion in steam engines, particularly steam locomotives. Most steam locomotives used slide valves or piston valves, but these designs, although mechanically simpler and very rugged, were significantly less efficient than the poppet valve. A number of designs of locomotive poppet valve system were tried, the most popular being the Italian Caprotti valve gear[[2]], the British Caprotti valve gear[[3]] (an improvement of the Italian one), the German Lentz rotary-cam valve gear, and two American versions by Franklin, their oscillating-cam valve gear and rotary-cam valve gear. They were used with some success, but they were less ruggedly reliable than traditional valve gear and did not see widespread adoption. In internal combustion engine poppet valve The valve is usually a flat disk of metal with a long rod known as the valve stem out one end. -
Chapter 5 Dimensional Analysis and Similarity
Chapter 5 Dimensional Analysis and Similarity Motivation. In this chapter we discuss the planning, presentation, and interpretation of experimental data. We shall try to convince you that such data are best presented in dimensionless form. Experiments which might result in tables of output, or even mul- tiple volumes of tables, might be reduced to a single set of curves—or even a single curve—when suitably nondimensionalized. The technique for doing this is dimensional analysis. Chapter 3 presented gross control-volume balances of mass, momentum, and en- ergy which led to estimates of global parameters: mass flow, force, torque, total heat transfer. Chapter 4 presented infinitesimal balances which led to the basic partial dif- ferential equations of fluid flow and some particular solutions. These two chapters cov- ered analytical techniques, which are limited to fairly simple geometries and well- defined boundary conditions. Probably one-third of fluid-flow problems can be attacked in this analytical or theoretical manner. The other two-thirds of all fluid problems are too complex, both geometrically and physically, to be solved analytically. They must be tested by experiment. Their behav- ior is reported as experimental data. Such data are much more useful if they are ex- pressed in compact, economic form. Graphs are especially useful, since tabulated data cannot be absorbed, nor can the trends and rates of change be observed, by most en- gineering eyes. These are the motivations for dimensional analysis. The technique is traditional in fluid mechanics and is useful in all engineering and physical sciences, with notable uses also seen in the biological and social sciences. -
Low Pressure High Torque Quasi Turbine Rotary Air Engine
ISSN: 2319-8753 International Journal of Innovative Research in Science, Engineering and Technology (An ISO 3297: 2007 Certified Organization) Vol. 3, Issue 8, August 2014 Low Pressure High Torque Quasi Turbine Rotary Air Engine K.M. Jagadale 1, Prof V. R. Gambhire2 P.G. Student, Department of Mechanical Engineering, Tatyasaheb Kore Institute of Engineering and Technology, Warananagar, Maharashtra, India1 Associate Professor, Department of Mechanical Engineering, Tatyasaheb Kore Institute of Engineering and Technology, Warananagar, Maharashtra, India 2 ABSTRACT: This paper discusses concept of Quasi turbine (QT) engines and its application in industrial systems and new technologies which are improving their performance. The primary advantages of air engine use come from applications where current technologies are either not appropriate or cannot be scaled down in size, rather there are not such type of systems developed yet. One of the most important things is waste energy recovery in industrial field. As the natural resources are going to exhaust, energy recovery has great importance. This paper represents a quasi turbine rotary air engine having low rpm and works on low pressure and recovers waste energy may be in the form of any gas or steam. The quasi turbine machine is a pressure driven, continuous torque and having symmetrically deformable rotor. This report also focuses on its applications in industrial systems, its multi fuel mode. In this paper different alternative methods discussed to recover waste energy. The quasi turbine rotary air engine is designed and developed through this project work. KEYWORDS: Quasi turbine (QT), Positive displacement rotor, piston less Rotary Machine. I. INTRODUCTION A heat engine is required to convert the recovered heat energy into mechanical energy. -
Cavitation in Valves
VM‐CAV/WP White Paper Cavitation in Valves Table of Contents Introduction. 2 Cavitation Analysis. 2 Cavitation Data. 3 Valve Coefficient Data. 4 Example Application. .. 5 Conclusion & Recommendations . 5 References. 6 Val‐Matic Valve & Mfg. Corp. • www.valmatic.com • [email protected] • PH: 630‐941‐7600 Copyright © 2018 Val‐Matic Valve & Mfg. Corp. Cavitation in Valves INTRODUCTION Cavitation can occur in valves when used in throttling or modulating service. Cavitation is the sudden vaporization and violent condensation of a liquid downstream of the valve due to localized low pressure zones. When flow passes through a throttled valve, a localized low pressure zone forms immediately downstream of the valve. If the localized pressure falls below the vapor pressure of the fluid, the liquid vaporizes (boils) and forms a vapor pocket. As the vapor bubbles flow downstream, the pressure recovers, and the bubbles violently implode causing a popping or rumbling sound similar to tumbling rocks in a pipe. The sound of cavitation in a pipeline is unmistakable. The condensation of the bubbles not only produces a ringing sound, but also creates localized stresses in the pipe walls and valve body that can cause severe pitting. FIGURE 1. Cavitation Cavitation is a common occurrence in shutoff valves during the last few degrees of closure when the supply pressure is greater than about 100 psig. Valves can withstand limited durations of cavitation, but when the valve must be throttled or modulated in cavitating conditions for long periods of time, the life of the valve can be drastically reduced. Therefore, an analysis of flow conditions is needed when a valve is used for flow or pressure control. -
Air-Cooled Cylinders 2
Air-Cooled Aircraft Engine Cylinders An Evolutionary Odyssey by George Genevro Part 2 - Developments in the U.S. The Lawrance-Wright Era. In the U.S., almost the only proponent of the air-cooled engine during World War I was the Lawrance Aero Engine Company. This small New York City firm had produced the crude opposed twins that powered the Penguin trainers, which were supposed to be the stepping-stone to the Jenny for aspiring military pilots. The Penguins were not intended to fly but apparently could taxi at a speed that would provide some excitement for trainees as they tried to maintain directional control and develop some feel of what flight controls were all about. The Lawrance twins, which can be seen in many museums, had directly opposed air- cooled cylinders and a crankshaft with a single crankpin to which both connecting rods were attached. This arrangement resulted in an engine that shook violently at all speeds and was therefore essentially useless for normal powered flight. After World War I, some attempts were made, generally unsuccessful, to convert the Lawrance twins into usable engines for light aircraft by fitting a two-throw crankshaft and welding an offset section into the connecting rods. This proves that the desire to fly can be very strong indeed in some individuals. The hairpin valve springs pictured to the left were possibly pioneered by Salmson in 1911, and later used not only on British single-cylinder racing motorcycle engines, but also by Ferrari and others into the 1950s. This use was a response to the same problem that led to desmodromic valves at Ducati, Norton (test only) and Mercedes - namely the fatigue of coil springs from "ringing". -
Preparation of Papers in Two-Column Format
International Conference on Ideas, Impact and Innovation in Mechanical Engineering (ICIIIME 2017) ISSN: 2321-8169 Volume: 5 Issue: 6 1336 – 1341 __________________________________________________________________________________________ A Review on Application of the Quasiturbine Engine as a Replacement for the Standard Piston Engine Akash Ampat, Siddhant Gaidhani2,Sachin Yevale3, Prashant Kharche4 1Student,Department of Mechanical Engineering, Smt. Kashibai Navale College of Engineering, Pune;[email protected], 2Student,Department of Mechanical Engineering, Smt. Kashibai Navale College of Engineering, Pune; [email protected] ABSTRACT This paper reviews the concept of a Quasiturbine (also known as Qurbine) Engine and its potential as a replacement for the standard Piston Engine. The Quasiturbine Rotary Air Engine is a low rpm engine, working on low pressure. For this purpose, a binary system of Quasiturbines is also used. It also discusses the multi-fuel capability of Quasiturbine and how it can be used in vehicle propulsion systems. This piston-less rotary machine is intended to be used where the existing technologies are centuries old and have numerous insurmountable problems. It has been consistently observed that this engine provides a better efficiency, much smaller ratio of unit displacement to engine volume, extremely high power per cycle and reduced emissions. Key words: Quasiturbine, standard piston engine, piston-less rotary engine, deformable rotor. I. INTRODUCTION A. Need and Invention Dr. Gilles Saint-Hilaire, a thermonuclear physicist, after thoroughly studying the limitations of conventional engines, designed the Quasiturbine Engine. The Quasiturbine is a continuous Torque, symmetrically deformable spinning wheel. The Saint-Hilaire family used a modern computer based approach to map the conventional engine characteristics with optimum physical-chemical graphs. -
1/8” Poppet Valves
1/8” POPPET VALVES 1/8" POPPET TYPE-VALVES provide a complete line of economical, compact, trouble-free units. They are available in a wide variety of manually operated 2-way, 3-way and 4-way models. The valve bodies are corrosion resistant aluminum. All other parts are treated or plated to provide long service and resist corrosion. The poppet seal is Buna-N. Air flow capacity is 25 Cu. Ft. free air per minute at 100 P.S.I. Maximum operating pressure is 150 P.S.I. Maximum temperature range is 250°F. V2 TWO-WAY BUTTON VALVE Depressing button will permit flow. May be mounted on any one of three sides. V23 THREE-WAY BUTTON VALVE Depressing button will permit flow. Releasing button will permit exhaust flow through button stem. V2H TWO WAY TWO BUTTON VALVE One common inlet Two separate outlets. THREE-WAY VALVES During operation, air will not escape to atmosphere. Lever bearings are of hardened steel for long service. The utilizable exhaust port will accept our Bleed Control Valve PTV305 for controlling the exhaust. Can be mounted on either of two sides. LEVER OPERATED V3NC THREE-WAY NORMALLY CLOSED V3NO THREE-WAY NORMALLY OPEN HAND OPERATED HV3NC THREE-WAY NORMALLY CLOSED HV3NO THREE-WAY NORMALLY OPEN CAM OPERATED CV3NC THREE-WAY NORMALLY CLOSED CV3NO THREE-WAY NORMALLY OPEN FOOT OPERATED FT300NC THREE-WAY NORMALLY CLOSED FT300NO THREE-WAY NORMALLY OPEN PILOT TIMER VALVE PTV3NC THREE-WAY NORMALLY CLOSED PTV3NO THREE-WAY NORMALLY OPEN Valve consists of a diaphragm pilot chamber which operates the 3-way valve section. -
Eulerian–Lagrangian Method for Simulation of Cloud Cavitation ∗ Kazuki Maeda , Tim Colonius
Journal of Computational Physics 371 (2018) 994–1017 Contents lists available at ScienceDirect Journal of Computational Physics www.elsevier.com/locate/jcp Eulerian–Lagrangian method for simulation of cloud cavitation ∗ Kazuki Maeda , Tim Colonius Division of Engineering and Applied Science, California Institute of Technology, 1200 East California Boulevard, Pasadena, CA 91125, USA a r t i c l e i n f o a b s t r a c t Article history: We present a coupled Eulerian–Lagrangian method to simulate cloud cavitation in a Received 3 December 2017 compressible liquid. The method is designed to capture the strong, volumetric oscillations Received in revised form 10 April 2018 of each bubble and the bubble-scattered acoustics. The dynamics of the bubbly mixture Accepted 16 May 2018 is formulated using volume-averaged equations of motion. The continuous phase is Available online 18 May 2018 discretized on an Eulerian grid and integrated using a high-order, finite-volume weighted Keywords: essentially non-oscillatory (WENO) scheme, while the gas phase is modeled as spherical, Bubble dynamics Lagrangian point-bubbles at the sub-grid scale, each of whose radial evolution is tracked Cavitation by solving the Keller–Miksis equation. The volume of bubbles is mapped onto the Eulerian Eulerian–Lagrangian method grid as the void fraction by using a regularization (smearing) kernel. In the most general Compressible multiphase flows case, where the bubble distribution is arbitrary, three-dimensional Cartesian grids are used Multiscale modeling for spatial discretization. In order to reduce the computational cost for problems possessing Reduced-order modeling translational or rotational homogeneities, we spatially average the governing equations along the direction of symmetry and discretize the continuous phase on two-dimensional or axi-symmetric grids, respectively. -
A Numerical Algorithm for MHD of Free Surface Flows at Low Magnetic Reynolds Numbers
A Numerical Algorithm for MHD of Free Surface Flows at Low Magnetic Reynolds Numbers Roman Samulyak1, Jian Du2, James Glimm1;2, Zhiliang Xu1 1Computational Science Center, Brookhaven National Laboratory, Upton, NY 11973 2 Department of Applied Mathematics and Statistics, SUNY at Stony Brook, Stony Brook, NY 11794, USA November 7, 2005 Abstract We have developed a numerical algorithm and computational soft- ware for the study of magnetohydrodynamics (MHD) of free surface flows at low magnetic Reynolds numbers. The governing system of equations is a coupled hyperbolic/elliptic system in moving and ge- ometrically complex domains. The numerical algorithm employs the method of front tracking for material interfaces, high resolution hy- perbolic solvers, and the embedded boundary method for the elliptic problem in complex domains. The numerical algorithm has been imple- mented as an MHD extension of FronTier, a hydrodynamic code with free interface support. The code is applicable for numerical simulations of free surface conductive liquids or flows of weakly ionized plasmas. Numerical simulations of the Muon Collider/Neutrino Factory target have been discussed. 1 Introduction Computational magnetohydrodynamics, greatly inspired over the last decades by the magnetic confinement fusion and astrophysics problems, has achieved significant results. However the major research effort has been in the area of highly ionized plasmas. Numerical methods and computational software for MHD of weakly conducting materials such as liquid metals or weakly ionized plasmas have not been developed to such an extent despite the need 1 for fusion research and industrial technologies. Liquid metal MHD, driven by potential applications of flowing liquid metals or electrically conducting liquid salts as coolant in magnetic confinement fusion reactors as well as some industrial problems, has attracted broad theoretical, computational, and experimental studies (see [16, 17, 18] and references therein). -
Quasiturbine Rotor Development Optimization
Quasiturbine Rotor Development Optimization MOHAMMED AKRAM MOHAMMED A thesis submitted in fulfillment of the requirement for the award of the Degree of Master in Mechanical Engineering Faculty of Mechanical and Manufacturing Engineering Universiti Tun Hussein Onn Malaysia June 2014 v ABSTRACT The Quasiturbine compressor is still in developing level and its have more advantages if compare with wankel and reciprocating compressors. Quasiturbine was separated in two main important components which they are housing and rotor .Quasiturbine rotor contains a number of parts such as blades, seal, support plate and mechanism .This research focus on modeling and simulation for Quasiturbine seal to improve it and reduce the wear by using motion analysis tool and simulation tool box in Solidworks 2014 software .This study has simulated the existing design and proposed design of seal with use Aluminum (1060 alloy ) as a material of seal for both cases . In addition it has been simulated three different materials for the proposed design of seal (Aluminum, ductile iron , steel ) .The proposed design of seal was selected as better design than the existing one when compared the distribution of von Mises stress and the percentage of deformation for both cases . According to the results of the three mateials that tested by simulation for the proposed design , ductile iron is the most suitable materials from the three tested materials for Quasiturbine seal . vi CONTENTS TITLE i DECLARATION ii DEDICATION iii ACKNOWLEDGEMENT iv ABSTRACT v CONTENTS vi LIST