Something About the Balancing of Thermal Motors
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Fluctuations in the Energetic Properties of a Spark-Ignition Engine Model with Variability
Entropy 2013, 15, 3277-3296; doi:10.3390/e15083367 OPEN ACCESS entropy ISSN 1099-4300 www.mdpi.com/journal/entropy Article Fluctuations in the Energetic Properties of a Spark-Ignition Engine Model with Variability Pedro L. Curto-Risso 1, Alejandro Medina 2, Antonio Calvo-Hernandez´ 3, Lev Guzman-Vargas´ 4;* and Fernando Angulo-Brown 5 1 Instituto de Ingenier´ıa Mecanica´ y Produccion´ Industrial, Universidad de la Republica,´ Montevideo 11300, Uruguay; E-Mail: pcurto@fing.edu.uy 2 Departamento de F´ısica Aplicada, Universidad de Salamanca, Salamanca 37008, Spain; E-Mail: [email protected] 3 Departamento de F´ısica Aplicada and IUFFYM, Universidad de Salamanca, Salamanca 37008, Spain; E-Mail: [email protected] 4 Unidad Profesional Interdisciplinaria en Ingenier´ıa y Tecnolog´ıas Avanzadas, Instituto Politecnico´ Nacional, Av. IPN 2580, L. Ticoman,´ Mexico D.F. 07340, Mexico 5 Departamento de F´ısica, Escuela Superior de F´ısica y Matematicas,´ Instituto Politecnico´ Nacional, Edif. No. 9 U.P. Zacatenco, Mexico D. F. 07738, Mexico; E-Mail: [email protected] * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel.: +52-55-57296000 ext. 56873; Fax: +52-55-57529318. Received: 8 June 2013; in revised form: 30 July 2013 / Accepted: 13 August 2013 / Published: 19 August 2013 Abstract: We study the energetic functions obtained in a simulated spark-ignited engine that incorporates cyclic variability through a quasi-dimensional combustion model. Our analyses are focused on the effects of the fuel-air equivalence ratio of the mixture simultaneously over the cycle-to-cycle fluctuations of heat release (QR) and the performance outputs, such as the power (P ) and the efficiency (η). -
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. -
Intellectual Property Center, 28 Upper Mckinley Rd. Mckinley Hill Town Center, Fort Bonifacio, Taguig City 1634, Philippines Tel
Intellectual Property Center, 28 Upper McKinley Rd. McKinley Hill Town Center, Fort Bonifacio, Taguig City 1634, Philippines Tel. No. 238-6300 Website: http://www.ipophil.gov.ph e-mail: [email protected] Publication Date: August 10, 2015 1 ALLOWED MARKS PUBLISHED FOR OPPOSITION ............................................................................................... 2 1.1 ALLOWED NATIONAL MARKS ....................................................................................................................................... 2 Intellectual Property Center, 28 Upper McKinley Rd. McKinley Hill Town Center, Fort Bonifacio, Taguig City 1634, Philippines Tel. No. 238-6300 Website: http://www.ipophil.gov.ph e-mail: [email protected] Publication Date: August 10, 2015 1 ALLOWED MARKS PUBLISHED FOR OPPOSITION 1.1 Allowed national marks Application No. Filing Date Mark Applicant Nice class(es) Number 25 June 1 4/2010/00006843 AIR21 GLOBAL AIR21 GLOBAL, INC. [PH] 35 and39 2010 20 2 4/2012/00011594 September AAA SUNQUAN LU [PH] 19 2012 11 May 3 4/2012/00501163 CACATIAN, LEUGIM D [PH] 25 2012 24 4 4/2012/00740257 September MIX N` MAGIC MICHAELA A TAN [PH] 30 2012 11 June NEUROGENESIS 5 4/2013/00006764 LBI BRANDS, INC. [CA] 32 2013 HAPPY WATER BABAYLAN SPA AND ALLIED 6 4/2013/00007633 1 July 2013 BABAYLAN 44 INC. [PH] 12 July OAKS HOTELS & M&H MANAGEMENT 7 4/2013/00008241 43 2013 RESORTS LIMITED [MU] 25 July DAIWA HOUSE INDUSTRY 8 4/2013/00008867 DAIWA HOUSE 36; 37 and42 2013 CO., LTD. [JP] 16 August ELLEBASY MEDICALE ELLEBASY MEDICALE 9 4/2013/00009840 35 2013 TRADING TRADING [PH] 9 THE PROCTER & GAMBLE 10 4/2013/00010788 September UNSTOPABLES 3 COMPANY [US] 2013 9 October BELL-KENZ PHARMA INC. -
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. -
Scope of Quasi Turbine:A Review Analysis Pranjal Yadav, Amit Tiwari, Anuj Gupta, Sushant Verma, Sandeep Kumar Singh Department of Mechanical Engineering, G
Scope of Quasi Turbine:A Review Analysis Pranjal Yadav, Amit Tiwari, Anuj Gupta, Sushant Verma, Sandeep Kumar Singh Department of Mechanical Engineering, G. L. Bajaj Institute of Technology and Management, India ABSTRACT Piston engine is the main power supply of all kinds of mobile equipment’s, and its power density directly affects the performance of mobile equipment. Compared with electric motor and gas turbine power, the piston engine has a smaller volume, simpler structure, and larger power density etc., therefore it becomes the most common source of power. Present paper provides the review analysis for the Quasi Turbine including its comparison, design analysis and future scope of work. Keywords – Quasiturbine, Rotory Engine I INTRODUCTION Rotary piston engines have the basic characteristics different from traditional piston engine which is that under pressure torque, its piston rotates around the output shaft instead of reciprocating motion in the cylinder. The working process of the cylinders, although in some points it has its own characteristics, is almost simile as the original reciprocating work cycle in nature. On the one hand, it is freed of the reciprocating inertia force for the privilege of high speed, and on the other hand, to a certain extent, it keeps the economy of traditional piston engine. So, its emergence is the major technological changes on the structure of internal combustion engine [1]. Over the years, like this rotational structure, many kinds of solutions were put forward. By now in addition to Wankel rotary engine, others did not become a formal product 1.1. About Quasi Turbine The QT (QT) is the most compact and efficient tool currently available for compression and expansion of most working fluids. -
Numerical Analysis on Combustion Characteristic of Leaf Spring Rotary Engine
Energies 2015, 8, 8086-8109; doi:10.3390/en8088086 OPEN ACCESS energies ISSN 1996-1073 www.mdpi.com/journal/energies Article Numerical Analysis on Combustion Characteristic of Leaf Spring Rotary Engine Yan Zhang, Zhengxing Zuo and Jinxiang Liu * School of Mechanical Engineering, Beijing Institute of Technology, Beijing 100081, China; E-Mails: [email protected] (Y.Z.); [email protected] (Z.Z.) * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel./Fax: +86-10-6891-1392. Academic Editors: Paul Stewart and Chris Bingham Received: 19 March 2015 / Accepted: 17 July 2015 / Published: 4 August 2015 Abstract: The purpose of this paper is to investigate combustion characteristics for rotary engine via numerical studies. A 3D numerical model was developed to study the influence of several operative parameters on combustion characteristics. A novel rotary engine called, “Leaf Spring Rotary Engine”, was used to illustrate the structure and principle of the engine. The aims are to (1) improve the understanding of combustion process, and (2) quantify the influence of rotational speed, excess air ratio, initial pressure and temperature on combustion characteristics. The chamber space changed with crankshaft rotation. Due to the complexity of chamber volume, an equivalent modeling method was presented to simulate the chamber space variation. The numerical simulations were performed by solving the incompressible, multiphase Unsteady Reynolds-Averaged Navier–Stokes Equations via the commercial code FLUENT using a transport equation-based combustion model; a realizable turbulence model and finite-rate/eddy-dissipation model were used to account for the effect of local factors on the combustion characteristics. -
RT Rondelle PDF Specimen
RAZZIATYPE RT Rondelle RAZZIATYPE RT RONDELLE FAMILY Thin Rondelle Thin Italic Rondelle Extralight Rondelle Extralight Italic Rondelle Light Rondelle Light Italic Rondelle Book Rondelle Book Italic Rondelle Regular Rondelle Regular Italic Rondelle Medium Rondelle Medium Italic Rondelle Bold Rondelle Bold Italic Rondelle Black Rondelle Black Italic Rondelle RAZZIATYPE TYPEFACE INFORMATION About RT Rondelle is the result of an exploration into public transport signage typefa- ces. While building on this foundation it incorporates the distinctive characteri- stics of a highly specialized genre to become a versatile grotesque family with a balanced geometrical touch. RT Rondelle embarks on a new life of its own, lea- ving behind the restrictions of its heritage to form a consistent and independent type family. Suited for a wide range of applications www.rt-rondelle.com Supported languages Afrikaans, Albanian, Basque, Bosnian, Breton, Catalan, Croatian, Czech, Danish, Dutch, English, Esperanto, Estonian, Faroese, Fijian, Finnish, Flemish, French, Frisian, German, Greenlandic, Hawaiian, Hungarian, Icelandic, Indonesian, Irish, Italian, Latin, Latvian, Lithuanian, Malay, Maltese, Maori, Moldavian, Norwegian, Polish, Portuguese, Provençal, Romanian, Romany, Sámi (Inari), Sámi (Luli), Sámi (Northern), Sámi (Southern), Samoan, Scottish Gaelic, Slovak, Slovenian, Sorbian, Spa- nish, Swahili, Swedish, Tagalog, Turkish, Welsh File formats Desktop: OTF Web: WOFF2, WOFF App: OTF Available licenses Desktop license Web license App license Further licensing -
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 -
Review of Quasi-Turbine Engine
ISSN(Online) : 2319-8753 ISSN (Print) : 2347-6710 International Journal of Innovative Research in Science, Engineering and Technology (An ISO 3297: 2007 Certified Organization) Vol. 5, Issue 10, October 2016 Review of Quasi-Turbine Engine Yogesh Khedkar1, Prof.Sushant Pande2 P.G. Student, Department of Mechanical Engineering, D Y Patil College of Engineering, Akurdi, Pune, India1 Assistant Professor, Department of Mechanical Engineering, D Y Patil College of Engineering, Akurdi, Pune, India2 ABSTRACT: The Quasi turbine engine is a multi-fuel, continuous torque rotary engine.It a next step in the world of Engine research is to run engine on air or any other fuel. Turbine characteristics help achieving this goal. The quasi turbine turbo-machine is a pressure driven, continuous torque and symmetrically deformable spinning wheel. The Quasi turbine is a compact, low weight and high torque machine with top efficiency, especially in power modulation applications. 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. A quasi turbine rotary air engine having low rpm and works on low pressure recovers waste energy may be in the form of any gas or steam. This paper discusses concept of quasi turbine air and combustion engines also the comparison between the quasi turbine engine and the other engines. KEYWORDS: Quasi turbine (QT), Positive displacement rotor, piston less Rotary Machine. I. INTRODUCTION The Quasi-turbine is a new engine technology that was invented in 1990 and patented in 1996.The concept of quasi turbine rotary air engine was first introduced by Gilles Saint-Hilaire and etal. -
On Cycle-To-Cycle Heat Release Variations in a Simulated Spark Ignition Heat Engine
On cycle-to-cycle heat release variations in a simulated spark ignition heat engine P.L. Curto-Risso 1 Departamento de F´ısica Aplicada, Universidad de Salamanca, 37008 Salamanca, Spain A. Medina ∗;2 Departamento de F´ısica Aplicada, Universidad de Salamanca, 37008 Salamanca, Spain A. Calvo Hern´andez 3 Departamento de F´ısica Aplicada, Universidad de Salamanca, 37008 Salamanca, Spain L. Guzm´an-Vargas Unidad Profesional Interdisciplinaria en Ingenier´ıay Tecnolog´ıasAvanzadas, Instituto Polit´ecnico Nacional, Av. IPN No. 2580, L. Ticom´an,M´exico D.F. 07340, M´exico F. Angulo-Brown Departamento de F´ısica, Escuela Superior de F´ısica y Matem´aticas, Instituto Polit´ecnico Nacional, Edif. No. 9 U.P. Zacatenco, M´exico D.F. 07738, M´exico Abstract The cycle-by-cycle variations in heat release for a simulated spark-ignited engine are analyzed within a turbulent combustion model in terms of some basic parameters: the characteristic length of the unburned eddies entrained within the flame front, a arXiv:1005.5410v1 [physics.class-ph] 28 May 2010 characteristic turbulent speed, and the location of the ignition kernel. The evolution of the simulated time series with the fuel-air equivalence ratio, φ, from lean mixtures to over stoichiometric conditions, is examined and compared with previous experi- ments. Fluctuations on the characteristic length of unburned eddies are found to be essential to simulate heat release cycle-to-cycle variations and recover experimental results. Relative to the non-linear analysis of the system, it is remarkable that at fuel ratios around φ ' 0:65, embedding and surrogate procedures show that the dimensionality of the system is small. -
The Earliest Locomotives and Railways
The Earl i est Rai l ways The first railroads in Britain were in the 18th century coal mines, where horses pulled mine carts from the pits to the factories along wooden tracks. Later, in 1807, the first railway to carry passengers was opened. It was called the Oystermouth Railway and horses pulled carriages along tracks from Swansea to Oystermouth in South Wales. The Earl i est Rai l ways Thomas Saver y Thomas Savery (1650 – 1715) invented and made one of the f irst ever st eam engines in 1698. This engine was used to pump water out of the coal mines, but unfortunately it had a number of problems and did not work as well as everyone hoped. However, t his early st eam engine design helped other engineers and inventors to develop more successful engines in the future. The Earl i est Rai l ways James Watt James Watt (1736 – 1819) was a Scottish engineer who worked to improve the earliest steam engines like that of Thomas Savery. Watt’s desi gns and i deas were ver y successf ul . Af t er Wat t ret ired in 1800, many ot her engineers and inventors continued to work on and improve on this early steam engine design. The power of the steam engine was soon about to completely change travel and transport in the United Kingdom and around the world. Did you K now ? The unit of enery ‘the watt’ was named after James Wat t and he invent ed t he t erm ‘horsepower ’. The Fi rst St eam Engi ne Locomotives locomotive Soon engineers were creating train steam engine locomotives using new steam engine technologies which were quickly developing. -
ENRESO WORLD - Ilab
ENRESO WORLD - ILab Different Car Engine Types Istas René Graduated in Automotive Technologies 1-1-2019 1 4 - STROKE ENGINE A four-stroke (also four-cycle) engine is an internal combustion (IC) engine in which the piston completes four separate strokes while turning the crankshaft. A stroke refers to the full travel of the piston along the cylinder, in either direction. The four separate strokes are termed: 1. Intake: Also known as induction or suction. This stroke of the piston begins at top dead center (T.D.C.) and ends at bottom dead center (B.D.C.). In this stroke the intake valve must be in the open position while the piston pulls an air-fuel mixture into the cylinder by producing vacuum pressure into the cylinder through its downward motion. The piston is moving down as air is being sucked in by the downward motion against the piston. 2. Compression: This stroke begins at B.D.C, or just at the end of the suction stroke, and ends at T.D.C. In this stroke the piston compresses the air-fuel mixture in preparation for ignition during the power stroke (below). Both the intake and exhaust valves are closed during this stage. 3. Combustion: Also known as power or ignition. This is the start of the second revolution of the four stroke cycle. At this point the crankshaft has completed a full 360 degree revolution. While the piston is at T.D.C. (the end of the compression stroke) the compressed air-fuel mixture is ignited by a spark plug (in a gasoline engine) or by heat generated by high compression (diesel engines), forcefully returning the piston to B.D.C.