10. First 50 Years of Aircraft Engines
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Turbocompound Reheat Gas Turbine Combined Cycle 2015
INFRASTRUCTURE MINING & METALS NUCLEAR, SECURITY & ENVIRONMENTAL OIL, GAS & CHEMICALS Turbocompound Reheat Gas Turbine Combined Cycle 2015 Turbocompound Reheat Gas Turbine Combined Cycle S. Can Gülen Mark S. Boulden Bechtel Infrastructure Power POWER-GEN INTERNATIONAL 2015 December 8 - 10, 2015 Las Vegas Convention Center Las Vegas, NV USA ABSTRACT This paper discusses a new power generation cycle based on the fundamental thermodynamic concepts of constant volume combustion and reheat. The turbo- compound reheat gas turbine combined cycle (TC-RHT GTCC) comprises three pieces of rotating equipment: A turbo-compressor and two prime movers, i.e., a reciprocating gas engine and an industrial (heavy duty) gas turbine. Ideally, the cycle is proposed as the foundation of a customized power plant design of a given size and performance by combining different prime movers with new "from the blank sheet" designs. Nevertheless, a compact power plant based on the TC-RHT cycle can also be constructed by combining off-the-shelf equipment with modifications for immediate implementation. The paper describes the underlying thermodynamic principles, representative cycle calculations and value proposition as well as requisite modifications to the existing hardware. The operational philosophy governing plant start-up, shut-down and loading is described in detail. Also included in the paper is a 110 MW reference power block concept with 57+% net efficiency. The concept has been developed using a pre-engineered standard block approach and is amenable to simple “module-by-module” construction including easy shipment of individual components. POWER-GEN INTERNATIONAL 2015 Page 1 OF 26 INTRODUCTION Brief History Internal combustion engines can be classified into two major categories based on the heat addition portion of their respective thermodynamic cycles: “constant volume” and “constant pressure” heat addition engines (cycles) [1]. -
The TSR-2: a BRITISH STORY with an AUSTRALIAN CHAPTER
RAAF Radschool Association Magazine – Vol 32 Page 15 The TSR-2: A BRITISH STORY WITH AN AUSTRALIAN CHAPTER With the era of the F-111 coming to a close, it is timely to reflect on the development of this aircraft and the rivals that existed at the time of its selection. The principal competitor was the British Aircraft Corporation’s Tactical Strike and Reconnaissance (TSR-2) aircraft. However, as indicated by Sir Sydney Camm’s comment, the development and subsequent abrupt cancellation of the project in 1965 was politically charged. While it was suggested at the time that Australia played a key role in the demise of the TSR-2, there appears to have been many other contributors to its downfall. From the mid 1950s, the RAF and subsequently the RAAF identified the need to replace the Canberra bomber, focusing on a nuclear-capable aircraft. Given the rapid advances in anti-aircraft weaponry capability, having supersonic strike aircraft that could slip under radar surveillance was seen as a priority. The development of the TSR-2 was also the result of the British Government’s focus in the late 1950s on rationalising the eight main British aircraft manufacturers that then existed. On New Year’s Day 1959, Vickers-Armstrong and English Electric, amalgamated as the new British Aircraft Corporation (BAC), were awarded the contract to combine their earlier individual designs into the TSR-2. Later that year Bristol- Siddeley were awarded the contract for development of the Olympus engines which were to power the aircraft. Like the development of any aircraft, the TSR-2 had its technical problems. -
Los Motores Aeroespaciales, A-Z
Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales. -
Rolls-Royce, Oberursel - Summary
Group 1: Joseph Höfler, Ronan Bernard, Leonard Franke Thermal Turbomachines – Excursion 2015 Day 1: Rolls-Royce, Oberursel - Summary The Rolls-Royce Holding plc is a multinational company headquartered in the City of Westminster, London (UK). Its business segments include design, manufacturing, distribution and maintenance in the field of civil aero engines (53%), military aero engines (20%), marine propulsion systems (18%) and power generation equipment (9%). Rolls-Royce employs worldwide around 54,100 (2014) employees of which 15,500 (2014) are engineers. The underlying group revenue for 2014 is £14.588bn and a profit of £1.617bn. A direct subsidiary of the Rolls-Royce Holding plc is Rolls- Royce Deutschland with two facilities at Dahlewitz outside Berlin and Oberursel near to Frankfurt am Main combined with 3300 employees operating mainly in the field of civil and military aero engines. While in Dahlewitz the design and final assembly of the aero engines is located the sight at Oberursel focuses on production and maintenance. Today Rolls-Royce Deutschland is the only official licensed aero engine manufacturer in Germany operating in the field of design, production and maintenance of modern civil and military turbo jet engines. In the course of this excursion we were able to visit the facility in Oberursel on Tuesday the 26th of May 2015. Two former RR employees gave us an insight view on the production site. Besides visiting the actual production and maintenance lines a key focus lay also on the historical development of the factory site Oberursel therefor our visit started at the in-house factory museum (Prof. -
Electric Boosting and Energy Recovery Systems for Engine Downsizing
energies Review Electric Boosting and Energy Recovery Systems for Engine Downsizing Mamdouh Alshammari 1,2, Fuhaid Alshammari 2 and Apostolos Pesyridis 1,* 1 Centre of Advanced Powertrain and Fuels (CAPF), Department of Mechanical, Aerospace and Civil Engineering, Brunel University London, Middlesex UB8 3PH, UK; [email protected] 2 Department of Mechanical Engineering, University of Hai’l, Hail 55476, Saudi Arabia; [email protected] * Correspondence: [email protected] Received: 31 October 2019; Accepted: 4 December 2019; Published: 6 December 2019 Abstract: Due to the increasing demand for better fuel economy and increasingly stringent emissions regulations, engine manufacturers have paid attention towards engine downsizing as the most suitable technology to meet these requirements. This study sheds light on the technology currently available or under development that enables engine downsizing in passenger cars. Pros and cons, and any recently published literature of these systems, will be considered. The study clearly shows that no certain boosting method is superior. Selection of the best boosting method depends largely on the application and complexity of the system. Keywords: engine downsizing; electrically assisted turbocharger; electric supercharger; e-turbo; waste heat recovery; turbocharging; supercharging; turbocompounding; organic Rankine cycle 1. Introduction Although internal combustion engines are getting more efficient nowadays, still the major part of fuel energy is transformed into wasted heat. In terms of harmful exhaust emissions, the transportation sector is responsible for the one-third of CO2 emissions worldwide and approximately 15% of the overall greenhouse gas emissions [1]. Moreover, owing to the limited amount of fossil fuels, prices fluctuate significantly, with consistent general rising trends, resulting in economic issues in non-oil-producing countries. -
19FFL-0023 2-Stroke Engine Options for Automotive Use: a Fundamental Comparison of Different Potential Scavenging Arrangements for Medium-Duty Truck Applications
Citation for published version: Turner, J, Head, RA, Chang, J, Engineer, N, Wijetunge, RS, Blundell, DW & Burke, P 2019, '2-Stroke Engine Options for Automotive Use: A Fundamental Comparison of Different Potential Scavenging Arrangements for Medium-Duty Truck Applications', SAE Technical Paper Series, pp. 1-21. https://doi.org/10.4271/2019-01-0071 DOI: 10.4271/2019-01-0071 Publication date: 2019 Document Version Peer reviewed version Link to publication The final publication is available at SAE Mobilus via https://doi.org/10.4271/2019-01-0071 University of Bath Alternative formats If you require this document in an alternative format, please contact: [email protected] General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. Take down policy If you believe that this document breaches copyright please contact us providing details, and we will remove access to the work immediately and investigate your claim. Download date: 27. Sep. 2021 Paper Offer 19FFL-0023 2-Stroke Engine Options for Automotive Use: A Fundamental Comparison of Different Potential Scavenging Arrangements for Medium-Duty Truck Applications Author, co-author (Do NOT enter this information. It will be pulled from participant tab in MyTechZone) Affiliation (Do NOT enter this information. It will be pulled from participant tab in MyTechZone) Abstract For the opposed-piston engine, once the port timing obtained by the optimizer had been established, a supplementary study was conducted looking at the effect of relative phasing of the crankshafts The work presented here seeks to compare different means of on performance and economy. -
Constant Volume Combustion: the Ultimate Gas Turbine Cycle
INFRASTRUCTURE MINING & METALS NUCLEAR, SECURITY & ENVIRONMENTAL OIL, GAS & CHEMICALS Constant volume combustion: the ultimate gas turbine cycle About Bechtel Bechtel is among the most respected engineering, project management, and construction companies in the world. We stand apart for our ability to get the job done right—no matter how big, how complex, or how remote. Bechtel operates through four global business units that specialize in infrastructure; mining and metals; nuclear, security and environmental; and oil, gas, and chemicals. Since its founding in 1898, Bechtel has worked on more than 25,000 projects in 160 countries on all seven continents. Today, our 58,000 colleagues team with customers, partners, and suppliers on diverse projects in nearly 40 countries. Guest Feature Also in this section Constant volume combustion: 00 DARPA-funded CVC projects the ultimate gas turbine cycle 00 Power cycle thermodynamics 00 History of CVC engineering By S. C. Gülen, PhD, PE; Principal Engineer, Bechtel Power Pulse detonation combustion holds the key to 45% simple cycle and close to 65% combined cycle efficiencies at today’s 1400-1500°C gas turbine firing temperatures. The Kelvin-Planck statement of the Second Law of Thermo- Why constant volume combustion? dynamics leaves no room for doubt: the maximum efficiency In a modern gas turbine with an approximately constant pres- of a heat engine operating in a thermodynamic cycle cannot sure combustor, the compressor section consumes close to exceed the efficiency of a Carnot cycle operating between 50% of gas turbine power output. the same hot and cold temperature reservoirs. Assume one could devise a combustion system where All practical heat engine cycles are attempts to approxi- energy added to the working fluid (i.e. -
N O T I C E This Document Has Been Reproduced From
N O T I C E THIS DOCUMENT HAS BEEN REPRODUCED FROM MICROFICHE. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE CONTRACTORS REPORT NO. 995 NASA CR•165,170 LIGHTWEIGHT DIESEL ENGINE DESIGNS FOR COMMUTER TYPE AIRCRAFT (NASA-C8-165470) LIG BINEIGHT DIESEL ENGINE DiS1VNS FOR C ONMUTEi T y kE N82-11066 Coatiuenta^ AIRCRAFT (TelEdyne 10t0rs, nuskeyon, Micu^) 7U P hC: A04/&F A01 CSCL 21c Uncla., G3/J7 u8165 Alex P. Brouwers Teledyne Continental Motors General Products Division 76 Getty Street Muskegon, Michigan 49442 JULY 1981 ^^ NGV1S81 RECEIVED NASA Sn FACSftx Acm 01 PREPARED FOR: AMM NATIONAL AERONAUTICS AND SPACE ADMINISTRATION LEWIS RESEARCH CENTER 21000 BROOKPARK ROAD CLEVELAND, OHIO 44135 CONTRACT NAS3.22149 CONTRACTORS REPORT NO. 995 NASA CR•165470 LIGHTWEIGHT DIESEL ENGINE DESIGNS FOR COMMUTER TYPE AIRCRAFT Alex P. Bromers Teledyne Continental Motors General Products Division 76 Getty Street Muskegon, Michigan 49442 JULY 1981 PREPARED FOR: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION LEWIS RESEARCH CENTER 21000 BROOKPARK ROAD CLEVELAND, OHIO 44135 CONTRACT NAS3.22149 .xTELEDYNE C *ff1NEN1AL Mc7 M. General Products Wslon 4244J7-81 U, TABLE OF CONTENTS Papa No. 1.0 Summary ................................................................1 2.0 Introduction .............................................................3 2.1 Purpose of the Study ..................................................3 2.2 Previous Large Aircraft Diesel Engines -
Aircraft Propulsion C Fayette Taylor
SMITHSONIAN ANNALS OF FLIGHT AIRCRAFT PROPULSION C FAYETTE TAYLOR %L~^» ^ 0 *.». "itfnm^t.P *7 "•SI if' 9 #s$j?M | _•*• *• r " 12 H' .—• K- ZZZT "^ '! « 1 OOKfc —•II • • ~ Ifrfil K. • ««• ••arTT ' ,^IfimmP\ IS T A Review of the Evolution of Aircraft Piston Engines Volume 1, Number 4 (End of Volume) NATIONAL AIR AND SPACE MUSEUM 0/\ SMITHSONIAN INSTITUTION SMITHSONIAN INSTITUTION NATIONAL AIR AND SPACE MUSEUM SMITHSONIAN ANNALS OF FLIGHT VOLUME 1 . NUMBER 4 . (END OF VOLUME) AIRCRAFT PROPULSION A Review of the Evolution 0£ Aircraft Piston Engines C. FAYETTE TAYLOR Professor of Automotive Engineering Emeritus Massachusetts Institute of Technology SMITHSONIAN INSTITUTION PRESS CITY OF WASHINGTON • 1971 Smithsonian Annals of Flight Numbers 1-4 constitute volume one of Smithsonian Annals of Flight. Subsequent numbers will not bear a volume designation, which has been dropped. The following earlier numbers of Smithsonian Annals of Flight are available from the Superintendent of Documents as indicated below: 1. The First Nonstop Coast-to-Coast Flight and the Historic T-2 Airplane, by Louis S. Casey, 1964. 90 pages, 43 figures, appendix, bibliography. Price 60ff. 2. The First Airplane Diesel Engine: Packard Model DR-980 of 1928, by Robert B. Meyer. 1964. 48 pages, 37 figures, appendix, bibliography. Price 60^. 3. The Liberty Engine 1918-1942, by Philip S. Dickey. 1968. 110 pages, 20 figures, appendix, bibliography. Price 75jf. The following numbers are in press: 5. The Wright Brothers Engines and Their Design, by Leonard S. Hobbs. 6. Langley's Aero Engine of 1903, by Robert B. Meyer. 7. The Curtiss D-12 Aero Engine, by Hugo Byttebier. -
150 and 300 Kw Lightweight Diesel Aircraft Engine Design Study
https://ntrs.nasa.gov/search.jsp?R=19800011788 2020-03-21T19:51:36+00:00Z NASA Contractor Report 3260 150 and 300 kW Lightweight Diesel Aircraft Engine Design Study Alex P. Brouwers Teledyne Continental Motors Muskegon, Michigan Prepared for Lewis Research Center under Contract NAS3-20830 N/ /X National Aeronautics and Space Administration Scientific and Technical Information Office 1980 TABLE OF CONTENTS PageNo. 1.0 Summary ...................................................... 1 2.0 Introduction ................................................... 4 2.1 Advantages of the Diesel Engine .................................. 4 2.2 Previous Aircraft Diesel Engines .................................. 5 2.3 Scope of the Project ............................................. 7 2.4 Relative Merit of this Project to the General Field .................... 7 2.5 Significance of the Project ....................................... 7 3.0 Engine Design Study ............................................. 8 3.1 Technology Analysis ............................................ 8 3.1.1 Literature Search ............................................... 8 3.1.2 Definition of the Technology Base ................................. 8 3.1.3 Definition of the Design Approaches ............................... 16 3.1.4 Criteria Attributes ............................................... 17 3.1.5 Ranking Priorities ................................................ 18 3.1.6 Rating of Criteria ............................................... 19 3.1.7 Logic of Ranking ............................................... -
The Oberursel Rotary Engine - 100 Years of Fighter Aircraft
Geschichtskreis Motorenfabrik Oberursel e. V. Helmut Hujer The Oberursel Rotary Engine - 100 Years of Fighter Aircraft Special print of an article contributed by Helmut Hujer to the JOURNAL of The Rolls-Royce Heritage Trust, Issue 3 and 4 in 2015 © All rights reserved The author of this article has published in 2017 a comprehensive book about the 125 years of history of the Motorenfabrik Oberursel in German language. Some more information about this book is given on the following page. Zum Autor und dessen Buch „125 Jahre Motorenfabrik Oberursel“ Der Autor des Aufsatzes hat, beginnend mit einer Werkzeugmacher-Lehre 1961 und nach dem anschließenden Maschinenbau-Studium, sein gesamtes Berufsleben in der „Motorenfabrik Ober- ursel“ gearbeitet. Anschließend hat er wesentlich mitgewirkt an der Gründung des „Geschichts- kreis Motorenfabrik Oberursel“ im Jahr 2010, und zugleich hat er sich an die Erforschung der Werksgeschichte gemacht. Das Ergebnis ist sein im Jahr 2017 herausgegebenes Buch „125 Jahre Motorenfabrik Oberursel - 1892 bis 2017“. Dieses Buch, mit 896 reich bebilderten Seiten im Format A4, kann im Vortaunusmuseum in Ober- ursel eingesehen und erworben werden (50 €), im Werksmuseum bei Rolls-Royce Deutschland o- der direkt beim Autor, Kontakt: hujer.helmut@t- online.de, Tel. 06081/3611 und 0170 4375 178. Das Inhaltsverzeichnis sowie das Repertorium, mit Personen-Register und chronologischen Pro- dukte-Wegweiser, können auf den Webseiten www.gkmo.net und www.ursella.info als digitale und per Schlagwort durchsuchbare Dokumente eingesehen und kostenlos ausgedruckt werden. Die Motorenfabrik Oberursel, im Jahr 1892 gegründet und seit dem Jahr 2000 ein Standort der Firma Rolls-Royce Deutschland, gilt als die älteste noch in Betrieb befindliche Flugmotorenfabrik der Welt. -
National Air & Space Museum Technical Reference Files: Propulsion
National Air & Space Museum Technical Reference Files: Propulsion NASM Staff 2017 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Scope and Contents........................................................................................................ 1 Accessories...................................................................................................................... 1 Engines............................................................................................................................ 1 Propellers ........................................................................................................................ 2 Space Propulsion ............................................................................................................ 2 Container Listing ............................................................................................................. 3 Series B3: Propulsion: Accessories, by Manufacturer............................................. 3 Series B4: Propulsion: Accessories, General........................................................ 47 Series B: Propulsion: Engines, by Manufacturer.................................................... 71 Series B2: Propulsion: Engines, General............................................................