N Sulf, S SS 323 Š2S ŽS2% 26

Total Page:16

File Type:pdf, Size:1020Kb

N Sulf, S SS 323 Š2S ŽS2% 26 USOO7762219B2 (12) United States Patent (10) Patent No.: US 7.762,219 B2 Shuttleworth (45) Date of Patent: Jul. 27, 2010 (54) RECIRCULATION SYSTEM FOR MOTOR 5,647.309 A 7/1997 Avery 5,782,226 A 7/1998 Gartner (75) Inventor: Richard Jack Shuttleworth, Nelson 6,386,154 B1* 5/2002 Hellman et al. ............ 123,588 (NZ) 6.427,644 B1 8, 2002 Dabadie et al. 6,431,128 B1 8, 2002 Dabadie (73) Assignee: Shuttleworth Axial Motor Company, Nelson (NZ) FOREIGN PATENT DOCUMENTS (*) Notice: Subject to any disclaimer, the term of this EP O682743 11, 1995 patent is extended or adjusted under 35 EP O953745 11, 1999 U.S.C. 154(b) by 576 days. 2.E. 2. (21) Appl. No.: 10/590,337 W s 12 (22) PCT Filed: Feb. 7, 2005 W S. :3. (86). PCT No.: PCT/NZ2OOS/OOOO11 * cited by examiner S371 (c)(1), (2), (4) Date: Jun. 22, 2007 Primary Examiner Noah Kamen (74) Attorney, Agent, or Firm—Dann, Dorfman, Herrell and (87) PCT Pub. No.: WO2005/080781 Skillman, P.C. PCT Pub. Date: Sep. 1, 2005 (57) ABSTRACT (65) Prior Publication Data A motor has an engine block with cylinders arranged to fire in US 2007/O295OO8A1 Dec. 27, 2007 a firing order. Arecirculation system delivers combusted mix s ture from a cylinder which has just fired to at least partly mix (30) Foreign Application Priority Data with fuel for the next cylinder in the firing order. Injector bodies (401-405) are associated with each cylinder. Each Feb. 23, 2004 (NZ) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 531314 injector body (401-405) has an internal chamber (424) in communication with a fuel inlet port (426) for delivering fuel (51) Int. Cl. into the internal chamber, a fuel outlet port (428) for deliver F02B 75/20 (2006.01) ing fuel under pressure from the chamber into the associated (52) U.S. Cl. .......................................... 123/58.8 cylinder and a combusted mixture out-let port (442). The (58) Field of Classification Search ................. 123/58.8 combusted mixture outlet port (442) of each injector body See application file for complete search history. (401–405) is fluidly connected to the combusted mixture inlet port (438) of the next cylinder in the firing order. Alterna (56) References Cited tively, the recirculation system is arranged Substantially inter U.S. PATENT DOCUMENTS nally within the cylinder head. 4.475,524 A 10, 1984 Eckert et al. 4,787,343 A 1 1/1988 Tuckey 34 Claims, 7 Drawing Sheets S. 7.an 101 3.x. N. f N Sulf, S SS 323 Š2S ŽS2% 26 22 22 7 E. U.S. Patent Jul. 27, 2010 Sheet 1 of 7 US 7,762.219 B2 FIGURE 1 U.S. Patent Jul. 27, 2010 Sheet 2 of 7 US 7,762.219 B2 FIGURE 2 U.S. Patent Jul. 27, 2010 Sheet 3 of 7 US 7,762.219 B2 N yé 2 Š it.ÉIN%.2%NsŽ E3N N 2 SY27 7 1/ &2See N FIGURE 3 U.S. Patent Jul. 27, 2010 Sheet 4 of 7 US 7,762.219 B2 FIGURE 4 U.S. Patent US 7,762.219 B2 FIGURES U.S. Patent Jul. 27, 2010 Sheet 6 of 7 US 7,762.219 B2 U.S. Patent Jul. 27, 2010 Sheet 7 of 7 US 7,762.219 B2 % | % 94,9|| 22 (HIRI[10][HL NZZ (Z ||89 US 7,762,219 B2 1. 2 RECIRCULATION SYSTEM FOR MOTOR plurality of cylinders arranged to fire with a firing order, and a recirculation system configured to deliver combusted mix FIELD OF THE INVENTION ture under combustion pressure and temperature from a cyl inder which has just fired to at least partly mix with fuel for the The present invention relates to a recirculation system for a 5 next cylinder in the firing order to improve the combustion motor or engine and to a motor or engine incorporating the properties of the fuel. recirculation system. While the invention has application for It should be noted that where reference herein is made to axial motors, it also has applications for other motors. The “combusted mixture under combustion temperature and pres term “motor is used interchangeably with “engine'. Sure', that need not mean that the temperature and pressure 10 will be at the same levels as at the time of combustion, as BACKGROUND TO THE INVENTION pressure and temperature losses will occur during transfer of the mixture. However, the mixture will be at a significantly Over the years engine manufacturers have been working to elevated temperature and pressure relative to any combustible improve the weight, size efficiency and manufacturing costs mixture in the next cylinder in the firing order. of engines. In part this has lead to the development of axial 15 motors. An axial motor includes an engine block in which the The term comprising as used in this specification and cylinders are spaced evenly in a circular configuration about claims means consisting at least in part of, that is to say an axis of the engine block, rather than in the inline, “V” or when interpreting statements in this specification and claims horizontally opposed configurations of traditional engines. which include that term, the features prefaced by that term in The reciprocal motion of the pistons in an axial motor can be each statement all need to be present but other features can transferred to rotational motion of an output shaft by way of also be present. a wobble plate configuration, such as that disclosed in NZ In accordance with a second aspect of the present inven 221336. tion, there is provided a motor comprising: an engine block Generally, as with conventional internal combustion with a plurality of cylinders arranged to fire with a firing engines, the compression ratio and therefore power output of 25 order; and a recirculation system comprising fluid transfer the axial motor is at least in part limited by the quality of the paths which are arranged to provide a fluid connection fuel being burnt. If poor quality fuel is used, a lower com between cylinders sequentially in the firing order of the pression ratio must be used in the motor or else “knocking’ or motor, the motor configured Such that combustion in a cylin auto-igniting will occur, which ultimately could damage der creates a combusted mixture having a combustion pres components of the motor. Some higher density fuels (“heavy' 30 Sure, which combustion pressure forces some of that com fuels) such as diesel hydrocarbon fuel exhibit poor combus busted mixture to at least partly mix with fuel for the next tion properties as they are difficult to atomise prior to com cylinder in the firing order to improve the combustion prop bustion, compared to lower density fuels (“light' fuels) such erties of the fuel. as petrol. In one embodiment, each cylinder has an injector body A number of internal combustion engines are configured to 35 associated therewith, with each injector body having an inter deliver exhaust gas under relatively low pressure to cylinders nal chamber in communication with a fuel inlet port for to go some way towards improving combustion properties delivering fuel into the internal chamber, a fuel outlet port for and/or reducing emissions. Such engines are described in delivering fuel under pressure from the chamber into the U.S. Pat. No. 6,427,644; U.S. Pat. No. 5,782,226; U.S. Pat. associated cylinder, a mixture inlet port and a mixture outlet No. 4,475,524 and EP 0682743. 40 port, with the mixture inlet port of each injector body in fluid WO 03/008785 and WO 03/040530 to Scuderi describe communication with the mixture outlet port of an injector four stroke split cycle internal combustion engines. The body associated with the immediately preceding cylinder in engines have a compression cylinder containing a compres the firing order of the motor, the motor configured to deliver sion piston and a power cylinder containing a power piston. combusted mixture under combustion pressure and tempera The compression piston performs the intake and compression 45 ture from an outlet port of an injector body associated with a strokes of a four stroke cycle, and the power piston performs cylinder that has just fired to an inlet port of an injector body the power and exhaust strokes of the same four stroke cycle. associated with the next cylinder in the firing order of the A fresh air/fuel mixture is compressed in the compression motor to at least partly mix with fliel in the internal chamber cylinder and is delivered via a gas passage to the combustion of the injector body associated with said next cylinder in the cylinder for combustion, and then exhausted from the engine. 50 firing order to improve the combustion properties of the fuel. The two pistons are provided so that the power piston can be The fuel inlet port of each injector body is preferably offset to align the maximum combustion pressure with the configured for receipt of a respective fuel injector. maximum torque applied to the crank shaft, and so that the Advantageously, each mixture inlet port comprises a non compression piston can be offset to align the maximum com return valve which allows the mixture to travel into the inter pression with the maximum torque applied from the crank 55 shaft. The Scuderi systems do not address compression ratio nal chamber through the port but not out of the internal issues. Only fresh compressed mixture is shared between chamber through the port. cylinders. Preferably, each mixture outlet port comprises a non-return It is an object of the present invention to provide a recircu valve which allows mixture to travel out of the internal cham lation system for a motor which is operable to improve com 60 berthrough the port but not into the internal chamber through bustion properties and improve performance and/or which at the port.
Recommended publications
  • Conseil International
    Prof. Günter Elsbett: Controlled shift-liners for optimized scavenging, improved thermal efficiency and multi- stroke capability for opposed piston engines and conventional engines Page 2 Prof. Günter Elsbett: Controlled shift-liners for optimized scavenging, improved thermal efficiency and multi- stroke capability for opposed piston engines and conventional engines INTRODUCTION they are guided and supported by the surrounding cylinder material, leading to Opposed Piston Engines (OPEs) are low oscillating liner masses during shifting. looking back to 120 years of history and have been produced as Otto and Diesel engines, offering a promising challenge in specific output and thermal efficiency. Diesel-OPEs have been used regularly for commercial aircraft due to excellent power/weight ratio, but powering also merchant ships with big engines of several thousands of kW. Already 75 years ago a brake efficiency of more than 40% could be achieved. In recent decades these Fig.1 Cross-section of the 4SOPE engines seem to be forgotten while the research and development engineers put The presented experimental-OPE was just their main focus on emission improvement. created demonstrating the functions of the Conventional OPE-technology is known for hydraulically shifted liners in a fired engine. emission problems, especially caused by The parts are machined from full pieces of scraping lubrication oil into in- and outlet material. This OPE is applied with a simple ports, as common OPEs scavenging is mechanical fuel injection system, single- limited for use in 2-stroke engines only. hole pintle-nozzles and electric governor. Any emission treatment is not applied. Now some new developments in OPE- Data: Single-cylinder, 4-stroke, natural technology show their relevance to future aspirated, 108mm bore, 2x118mm stroke, power-train challenges.
    [Show full text]
  • The “Michell” Crankless Engine – Why Was It Not a Commercial Success?
    The Piston Engine Revolution The “Michell” Crankless Engine – Why was it not a commercial success? John A. Anning At the beginning of the twentieth century, when the internal combustion engine was being developed for automobiles and aircraft, some designers arranged for the cylinders to be parallel to the output shaft. These became known as axial or barrel engines. They utilised either the swash plate or wobbleplate principles. The most promising was the Michell Crankless Engine, which was patented in 1917. AGM Michell FRS (1870-1959) was an Australian engineer best known for the design of the “Michell” tilting pad thrust bearing, patented in the UK and Australia in 1905. By the end of WWI Michell was a wealthy man from royalties and applied the tilting pad principle to an axial engine. The principle was first applied to compressors and by 1920 the first IC engine was made. An advantage is that perfect primary and secondary balance can be achieved at all rotational speeds. Michell formed Crankless Engines (Australia) Pty Ltd. A number of engines were built and installed in existing production vehicles. He realised that for the future commercialisation an overseas involvement was essential so offices were opened in London and New York. The Michell crankless principle still remains the most efficient method of converting linear into rotary motion. By the late 1920s with the world depression the Australian company was forced into receivership. A business analysis is given as to the possible reasons for its failure to achieve commercial success. It deserves its place in the panoply of IC engine history.
    [Show full text]
  • Military Vehicle Options Arising from the Barrel Type Piston Engine
    Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes.
    [Show full text]
  • Re'search Memorandum
    c~~ififf$\? --A- CANC&LLtk, -j&$&+u 7&Czte-/ - &St , Au / 7 B ‘@. El4 3 5 is RE’SEARCH MEMORANDUM STUDY OF COMPRESSOR SYSTEMS FOR A GAS-GENERATOR ENGINE c .-? By Bernard I. Sather and Max J. Tauschek I I Lewis Flight Propulsion Laboratory i I’; Cleveland, Ohio Th~5oxulxa- -Lb-I EiE?ia p$g$p~gyg”~ym”& n&dmccdaat*Lnuj-mr. mM.a~-y yn 1L ,rO.Lblt.d m Irr. -wb!me sty I p.r.*ll. In th mm&y md mnl mwrvb.althabEd~.~ Ct*Ur omM~~~mycmarra~~ . SC- M*. aml Lil --.2iHmMMkDZD= L?hudd!szatl:r*d-munba NATIONAL ADVISORY COM M FOR AERONAUTICS WASHINGTON April 13, 1949 viJ!=s-! $ AC .c 3mkuy - --m!sv Awcf+AlrlliAL -km --L \ WV F-a-3 VI - --- --S~~l~~~~~~~lll~ NACA RM No. RCA28 ._..-___- -- .-.--- NATIONAL ADvIsaaY colNEEE Fak AERo~mIcs ByBernardI.SatheramdMaxJ.T'auschek Various methods of providing omessor-capacity and pressure- ratio control in the gas-generatm type of compound engine over a range of altitudes frcm sea level to 50,000 feet ax8 presented. The analythal results indicated that the best method of con- trol is that in which the first stage cf compression is carried out in a variable-speed supercharger driven by a hydmulio slip coupling. The second stage of oc~apression oould be either a rotazy constant-pressure-ratio-type cmpressor or a piston-type ccaspressor, both driven at oonstant speed. The a.n3lysis also iradioatedthat the variation Crp the value of the load coefficient for the first and second stages cd? the rotary constant-pressure-tgpe cqessor combination was within reasonable limits and that the valve timing .
    [Show full text]
  • “Design and Fabrication of Arc Engine”
    PROJECT REPORT [AUT84] On “DESIGN AND FABRICATION OF ARC ENGINE” Submitted by RISHAV CHHABRA (1NH15AU038) MOHAMMED TAMKEEN (1NH15AU029) In partial fulfillment of the requirement for award of Degree in Bachelor of Engineering (DEPARTMENT OF AUTOMOBILE ENGINEERING) Under The Guidance of Ms. Smitha B S Asst. Professor, Department of Automobile Engineering DEPARTMENT OF AUTOMOBILE ENGINEERING CERTIFICATE This is to certify that the Project [AUT84] On “DESIGN AND FABRICATION OF ARC ENGINE” Is a bonafide work carried out by Rishav Chhabra [1NH15AU038] Mohammed Tamkeen [1NH15AU029] Bonafide students of New Horizon College of Engineering in partial fulfilment for the award of Bachelor of Engineering in Automobile Engineering of the Visveswaraya Technological University, Belgaum during the year 2018-2019. It is certified that all corrections/suggestions indicated for Internal Assessment have been incorporated in the Report deposited in the department library. The project report has been approved as it satisfies the academic requirements in respect of Project work prescribed for the said Degree. Signature of HOD Signature of Principal Signature of Internal Guide Dr. Shridhar Kurse Dr. Manjunatha Prof. Smitha B S External Viva Name of the Examiners 1. Signature with Date 2. ACKNOWLEDGEMENT We express our heartfelt thanks to Dr. Mohan Manghnani, Chairman, New Horizon Educational Institutions for providing this endeavor. We would also like to thank Dr. Shridhar Kurse, Head of Department, Department of Automobile Engineering, NHCE and Dr. Manjunatha, Principal of NHCE who has given us a constant support with motivation in completion of the project. We sincerely thank Dr. Shridhar Kurse, HOD and Professor, Department of Automobile Engineering, NHCE who has guided us throughout in completion of the project.
    [Show full text]
  • Master's Thesis
    Potential Future Engine Cycles for Improved Thermal Efficiency Analysis of Various Internal Waste Heat Recovery Cycles with Minimal Deviation From Common Engine Architectures MICHAEL J. DENNY Department of Applied Mechanics Combustion Division Chalmers University of Technology Gothenburg, Sweden 2014 Master's Thesis 2014:32 Potential Future Engine Cycles for Improved Thermal Efficiency Analysis of Various Internal Waste Heat Recovery Cycles with Minimal Deviation From Common Engine Architectures MICHAEL J. DENNY © MICHAEL J. DENNY, 2014 Master's Thesis 2014:32 ISSN 1652-8557 Department of Applied Mechanics Combustion Division Chalmers University of Technology SE-412 96 G¨oteborg Sweden Telephone: + 46 (0)31-772 1000 Thesis performed at: Volvo Car Corporation Advanced Engine Engineering Dept. 97624 PO Box PV4B SE-405 31 G¨oteborg Sweden Printed by: Chalmers Reposervice G¨oteborg, Sweden 2014 Abstract A comparative 1-D analysis is undertaken between a baseline internal combustion engine (ICE) and several ICE operating cycle concepts which are intended to produce higher brake efficiencies than the baseline which runs on an Otto cycle. The baseline is a spark ignition gasoline engine representative of modern naturally aspirated automotive engines in its architecture and implemented technologies. Engine models are created and compared in the 1-D engine simulation software program GT-Power created by Gamma Technologies. After calibrating the performance of each model with the same resolution and tuning strategies, the result is that all of the concepts are less efficient than the base- line engine. Each engine concept requires additional hardware to separate the processes of the cycle within the engine. These components add to the mechanical friction, flow, and heat losses within the engine, and in some cases manage only to transfer exergy into different forms, not reduce it in a positive way.
    [Show full text]
  • IS 7879-8 (1987): Glossary of Aeronautical and Astronautical Terms, Part 8 Power Plant [TED 14: Aircraft and Space Vehicles]
    इंटरनेट मानक Disclosure to Promote the Right To Information Whereas the Parliament of India has set out to provide a practical regime of right to information for citizens to secure access to information under the control of public authorities, in order to promote transparency and accountability in the working of every public authority, and whereas the attached publication of the Bureau of Indian Standards is of particular interest to the public, particularly disadvantaged communities and those engaged in the pursuit of education and knowledge, the attached public safety standard is made available to promote the timely dissemination of this information in an accurate manner to the public. “जान का अधकार, जी का अधकार” “परा को छोड न 5 तरफ” Mazdoor Kisan Shakti Sangathan Jawaharlal Nehru “The Right to Information, The Right to Live” “Step Out From the Old to the New” IS 7879-8 (1987): Glossary of aeronautical and astronautical terms, Part 8 Power plant [TED 14: Aircraft and Space Vehicles] “ान $ एक न भारत का नमण” Satyanarayan Gangaram Pitroda “Invent a New India Using Knowledge” “ान एक ऐसा खजाना > जो कभी चराया नह जा सकताह ै”ै Bhartṛhari—Nītiśatakam “Knowledge is such a treasure which cannot be stolen” Jlf4+z qw(” “RE-AFFlRM ED 1997’ UDC 001’4 : 629’73/‘78’036 IS : 7879 [ Part 8 I- 1987 \ i‘y- ” -..i-:\, -La m qic:R_ ‘_ i Indian Standard XL \. , > % GLOSSARY OF AERONAUTICAL AND ASTRONA”Tl&i$iii’/~~ ._ PART 8 POWER PLANT 1. scope - Covers terms and definitions relating to power plant for aerospace applications.
    [Show full text]
  • Potentials of Coconut Oil As Diesel Substitute in Pacific Island Countries
    Rheinisch-Westfälische Technische Hochschule Aachen Fakultät für Maschinenwesen Lehrstuhl für Reaktorsicherheit und -technik Univ.-Prof. Dr.-Ing. Kurt Kugeler Diplomarbeit Potentials of Coconut Oil as Diesel Substitute in Pacific Island Countries vorgelegt von: cand. ing. Daniel Fürstenwerth betreut von: Dr.-Ing. Inga Maren Tragsdorf (RWTH Aachen) Dipl.-Ing. Gerhard Zieroth ( Executive Summary i Executive Summary The use of coconut oil as a substitute for diesel fuel is attracting increasing interest. This MSc thesis enhances the understanding of this technology and points out directions for its future application in the Republic of the Marshall Islands (RMI) as well as other Pacific Island Countries. The research work was undertaken by the PIEPSAP project in cooperation with RWTH University in Aachen and it is based on a literature review and field data obtained in RMI and Fiji. The use of straight vegetable oil in standard diesel engines leads to certain adverse technical and consequently financial effects. The extent of these depends on factors related to the (i) engine, (ii) oil and, equally important, (iii) utilisation and maintenance pattern. In principle, all adverse technical effects known from other vegetable oils occur when coconut oil is used. Important findings are that (i) “simply” replacing diesel fuel with coconut oil can by no means be recommended; (ii) blending of coconut oil with other fuels or the use of additives may decrease the rate but not prevent adverse technical effects; (iii) use of adaptation technology is a prerequisite, but no guarantee for a successful application of straight coconut oil. Before using coconut oil, a case-by-case analysis of the specific application is necessary, including the engine used and expected utilisation pattern.
    [Show full text]
  • The Potential of Wobble Plate Opposed Piston Axial Engines for Increased Efficiency
    energies Article The Potential of Wobble Plate Opposed Piston Axial Engines for Increased Efficiency Paweł Mazuro and Barbara Makarewicz * Department of Aircraft Engines, Faculty of Power and Aeronautical Engineering, Warsaw University of Technology, 00-665 Warsaw, Poland; [email protected] * Correspondence: [email protected] Received: 29 September 2020; Accepted: 22 October 2020; Published: 26 October 2020 Abstract: Recent announcements regarding the phase out of internal combustion engines indicate the need to make major changes in the automotive industry. Bearing in mind this innovation trend, the article proposes a new approach to the engine design. The aim of this paper is to shed a new light on the forgotten concept of axial engines with wobble plate mechanism. One of their most important advantages is the ease of use of the opposed piston layout, which has recently received much attention. Based on several years of research, the features determining the increase in mechanical efficiency, lower heat losses and the best scavenging efficiency were indicated. Thanks to the applied Variable Compression Ratio (VCR), Variable Angle Shift (VAS) and Variable Port Area (VPA) systems, the engine can operate on various fuels in each of the Spark Ignition (SI), Compression Ignition (CI) and Homogeneous Charge Compression Ignition (HCCI)/Controlled Auto Ignition (CAI) modes. In order to quantify the potential of the proposed design, an initial research of the newest PAMAR 4 engine was presented to calculate the torque curve at low rotational speeds. The achieved torque of 500 Nm at 500 rpm is 65% greater than the maximum torque of the OM 651 engine of the same 1.8 L capacity.
    [Show full text]
  • 81 Numerical Investigation of Pressure Reactive Piston Technology in a Spark Ignition Engine
    20056083 81 NUMERICAL INVESTIGATION OF PRESSURE REACTIVE PISTON TECHNOLOGY IN A SPARK IGNITION ENGINE Wooheum Cho Hyundai Motor Company, Korea Dohoy Jung, and Dennis Assanis W. E. Lay Automotive Laboratory, The University of Michigan, Ann Arbor, Michigan The novel, two-piece Pressure Reactive Piston technology providing the advantages of Variable Compression Ratio and rapid response to cylinder pressure changes was developed and numerically simulated in order to investigate its dynamic behavior and effects on fuel efficiency and emissions. The analytical model for flame-combustion chamber interaction was newly developed incorporating the VCR feature of the PRP engine and implemented into the engine cycle simulation program. The cycle simulation was subsequently used to explore the potential of the PRP engine over the full operating range and to investigate the effect of the PRP spring set characteristics on engine performance and emissions. Keywords: Variable Compression Ratio, Pressure Reactive Piston, Brake Specific Fuel Consumption Introduction sensitive to disturbances or wear to be used in production applications. Evenmore, many VCR technologies require In a typical Spark Ignition (SI) engine, better new engine architecture to implement, which require efficiency and higher performance can be achieved with significant investment to produce. Brevick patented the higher Compression Ratio (CR). However, higher Pressure Reactive Piston (PRP) technology (Patent cylinder pressure associated with higher CR can increase #5,755,192), which is two-piece piston with a spring set the end gas temperature and cause knocking at high load. between the upper and lower pistons. This mechanism In an effort to achieve higher CR while still avoiding with acceptable cost and complexity effectively limits the knocking, various types of Variable Compression Ratio peak cylinder pressures at high loads, while allowing the (VCR) technologies have been developed.
    [Show full text]
  • A Novel Reciprocating Sleeve Axial Diesel Engine, “The Shepherd
    A Novel Reciprocating Sleeve Axial Diesel Engine, “The Shepherd Engine” Adjunct Professor Stephen F Johnston PhD ME GCHE FIEAust CPEng Applied Technology Institute, Unitec NZ Abstract The paper outlines key features and explores some of the potential benefits of a novel axial, reciprocating sleeve, two stroke diesel engine design being developed by New Zealand inventor and innovator Gray Shepherd, with support from Unitec NZ. A proof of concept model has been demonstrated, and current work is on developing an engine which could meet global and European emission standards required by years 2008 - 2015. The Applied Technology Institute at Unitec is providing facilities and support. The paper discusses earlier engine designs and patents with broad similarities to Shepherd’s. The Shepherd engine dispenses with many of the components in a conventional engine, including connecting rods, crankshaft and valve drive train. Other design features significantly increase engine efficiency and power-to-weight ratio. The paper describes the advantages of the design, particularly its mechanical simplicity and its reduced number of working parts. Some of the issues in the commercialisation of new kinds of engine technologies are explored in the context of the experience of the Powell Engine Company. The paper concludes with suggestions on possible development paths for the engine. Its commercial prospects appear to be enhanced by concerns about fuel security and global climate change. Keywords Axial engines, ceramics, crankless engines, design and development, diesel engines, patents, invention, innovation, Shepherd, Unitec. Introduction In a diesel engine the fuel is injected into a combustion chamber, where it is ignited by the elevated temperature of the compressed air and burns at essentially constant pressure.
    [Show full text]
  • Royal Air Force Historical Society Journal 53
    ROYAL AIR FORCE HISTORICAL SOCIETY JOURNAL 53 2 The opinions expressed in this publication are those of the contributors concerned and are not necessarily those held by the Royal Air Force Historical Society. First published in the UK in 2012 by the Royal Air Force Historical Society All ri hts reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical includin photocopyin , recordin or by any information stora e and retrieval system, without permission from the Publisher in writin . ISSN 1361 4231 Printed by ,indrush -roup ,indrush House Avenue Two Station .ane ,itney O021 40, 3 ROYAL AIR FORCE HISTORICAL SOCIETY President 2arshal of the Royal Air Force Sir 2ichael 3eetham -C3 C3E DFC AFC 7ice8President Air 2arshal Sir Frederick Sowrey KC3 C3E AFC Committee Chairman Air 7ice82arshal N 3 3aldwin C3 C3E 7ice8Chairman -roup Captain 9 D Heron O3E Secretary -roup Captain K 9 Dearman FRAeS 2embership Secretary Dr 9ack Dunham PhD CPsychol A2RAeS Treasurer 9 3oyes TD CA 2embers Air Commodore - R Pitchfork 23E 3A FRAes ,in Commander C Cummin s :9 S Cox Esq 3A 2A :A72 P Dye O3E 3Sc(En ) CEn AC-I 2RAeS :-roup Captain P 9 2 Squires O3E 2A 3En RAF :,in Commander S Hayler 2A 3Sc RAF Editor & Publications ,in Commander C - 9efford 23E 3A 2ana er :Ex Officio 4 CONTENTS THE ,OR.D?S FIRST 9ET EN-INES: THE SERIOUS 7 PURSUIT OF INNO7ATION IN 2I.ITARA A7IATION, 19368194C byDr Hermione Giffard E&A SESSION 22 3RITAIN?S EAR.A 9ET AIRCRAFT by Captain Eric 3rown 21 DISCUSSION 3C THE 9ET INTO RAF SEUADRON SER7ICE by Air Cdre 31 -raham Pitchfork FIT FOR SER7ICE F THE RO.E OF SER7ICE TEST PI.OTS C0 by A72 Alan 2erriman THE A7RO 7U.CAN F 2AKIN- IT ,ORK by Tony 66 3lackman THE CO2ET IN TRANSPORT CO22AND by , Cdr 3asil 79 DGOliveira THE INTRODUCTION OF RAF 9ET AIRCRAFT F 96 EN-INEERIN- AND SUPP.A ISSUES by A72 -raham Skinner SUPP.E2ENTARA PAPERS THE .INCO.N THESEUS E0PERI2ENTA.
    [Show full text]