Torque Meter Table of Contents Volumes 1 - 7 (2002 - 2008) Compiled by James Strobeck
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Pegasus Vectored-Thrust Turbofan Engine
Pegasus Vectored-thrust Turbofan Engine Matador Harrier Sea Harrier AV-8A International Historic Mechanical Engineering Landmark 24 July 1993 International Air Tattoo '93 RAF Fairford The American Society of Mechanical Engineers I MECH E I NTERNATIONAL H ISTORIC M ECHANICAL E NGINEERING L ANDMARK PEGASUS V ECTORED-THRUST T URBOFAN ENGINE 1960 T HE B RISTOL AERO-ENGINES (ROLLS-R OYCE) PEGASUS ENGINE POWERED THE WORLD'S FIRST PRACTICAL VERTICAL/SHORT-TAKEOFF-AND-LANDING JET AIRCRAFT , THE H AWKER P. 1127 K ESTREL. USING FOUR ROTATABLE NOZZLES, ITS THRUST COULD BE DIRECTED DOWNWARD TO LIFT THE AIRCRAFT, REARWARD FOR WINGBORNE FLIGHT, OR IN BETWEEN TO ENABLE TRANSITION BETWEEN THE TWO FLIGHT REGIMES. T HIS ENGINE, SERIAL NUMBER BS 916, WAS PART OF THE DEVELOPMENT PROGRAM AND IS THE EARLIEST KNOWN SURVIVOR. PEGASUS ENGINE REMAIN IN PRODUCTION FOR THE H ARRIER II AIRCRAFT. T HE AMERICAN SOCIETY OF M ECHANICAL ENGINEERS T HE INSTITUTION OF M ECHANICAL ENGINEERS 1993 Evolution of the Pegasus Vectored-thrust Engine Introduction cern resulted in a perceived need trol and stability problems associ- The Pegasus vectored for combat runways for takeoff and ated with the transition from hover thrust engine provides the power landing, and which could, if re- to wing-borne flight. for the first operational vertical quired, be dispersed for operation The concepts examined and short takeoff and landing jet from unprepared and concealed and pursued to full-flight demon- aircraft. The Harrier entered ser- sites. Naval interest focused on a stration included "tail sitting" types vice with the Royal Air Force (RAF) similar objective to enable ship- exemplified by the Convair XFY-1 in 1969, followed by the similar borne combat aircraft to operate and mounted jet engines, while oth- AV-8A with the United States Ma- from helicopter-size platforms and ers used jet augmentation by means rine Corps in 1971. -
The New Whittle Laboratory Decarbonising Propulsion and Power
The New Whittle Laboratory Decarbonising Propulsion and Power The impressive work undertaken by the Whittle Laboratory, through the National Centre for Propulsion “and Power project, demonstrates the University’s leadership in addressing the fundamental challenges of climate change. The development of new technologies, allowing us to decarbonise air travel and power generation, will be central to our efforts to create a carbon neutral future. Professor Stephen Toope, Vice-Chancellor of the University of Cambridge ” 2 The New Whittle Laboratory Summary Cambridge has a long tradition of excellence in the propulsion and power sectors, which underpin aviation and energy generation. From 1934 to 1937, Frank Whittle studied engineering in Cambridge as a member of Peterhouse. During this time he was able to advance his revolutionary idea for aircraft propulsion and founded ‘Power Jets Ltd’, the company that would go on to develop the jet engine. Prior to this, in 1884 Charles Parsons of St John’s College developed the first practical steam turbine, a technology that today generates more than half of the world’s electrical power.* Over the last 50 years the Whittle Laboratory has built on this heritage, playing a crucial role in shaping the propulsion and power sectors through industry partnerships with Rolls-Royce, Mitsubishi Heavy Industries and Siemens. The Whittle Laboratory is also the world’s most academically successful propulsion and power research institution, winning nine of the last 13 Gas Turbine Awards, the most prestigious prize in the field, awarded once a year since 1963. Aviation and power generation have brought many benefits – connecting people across the world and providing safe, reliable electricity to billions – but decarbonisation of these sectors is now one of society’s greatest challenges. -
The Aircraft Propulsion the Aircraft Propulsion
THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section - -
The Connection
The Connection ROYAL AIR FORCE HISTORICAL SOCIETY 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. Copyright 2011: Royal Air Force Historical Society First published in the UK in 2011 by the Royal Air Force Historical Society All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. ISBN 978-0-,010120-2-1 Printed by 3indrush 4roup 3indrush House Avenue Two Station 5ane 3itney O72. 273 1 ROYAL AIR FORCE HISTORICAL SOCIETY President 8arshal of the Royal Air Force Sir 8ichael Beetham 4CB CBE DFC AFC Vice-President Air 8arshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-8arshal N B Baldwin CB CBE FRAeS Vice-Chairman 4roup Captain J D Heron OBE Secretary 4roup Captain K J Dearman 8embership Secretary Dr Jack Dunham PhD CPsychol A8RAeS Treasurer J Boyes TD CA 8embers Air Commodore 4 R Pitchfork 8BE BA FRAes 3ing Commander C Cummings *J S Cox Esq BA 8A *AV8 P Dye OBE BSc(Eng) CEng AC4I 8RAeS *4roup Captain A J Byford 8A 8A RAF *3ing Commander C Hunter 88DS RAF Editor A Publications 3ing Commander C 4 Jefford 8BE BA 8anager *Ex Officio 2 CONTENTS THE BE4INNIN4 B THE 3HITE FA8I5C by Sir 4eorge 10 3hite BEFORE AND DURIN4 THE FIRST 3OR5D 3AR by Prof 1D Duncan 4reenman THE BRISTO5 F5CIN4 SCHOO5S by Bill 8organ 2, BRISTO5ES -
The Raf Harrier Story
THE RAF HARRIER STORY ROYAL AIR FORCE HISTORICAL SOCIETY 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. Copyright 2006: Royal Air Force Historical Society First published in the UK in 2006 by the Royal Air Force Historical Society All rights reserved. No part of this book may be reproduced or transmitted in any form or by any means, electronic or mechanical including photocopying, recording or by any information storage and retrieval system, without permission from the Publisher in writing. ISBN 0-9530345-2-6 Printed by Advance Book Printing Unit 9 Northmoor Park Church Road Northmoor OX29 5UH 3 ROYAL AIR FORCE HISTORICAL SOCIETY President Marshal of the Royal Air Force Sir Michael Beetham GCB CBE DFC AFC Vice-President Air Marshal Sir Frederick Sowrey KCB CBE AFC Committee Chairman Air Vice-Marshal N B Baldwin CB CBE FRAeS Vice-Chairman Group Captain J D Heron OBE Secretary Group Captain K J Dearman Membership Secretary Dr Jack Dunham PhD CPsychol AMRAeS Treasurer J Boyes TD CA Members Air Commodore H A Probert MBE MA *J S Cox Esq BA MA *Dr M A Fopp MA FMA FIMgt *Group Captain N Parton BSc (Hons) MA MDA MPhil CEng FRAeS RAF *Wing Commander D Robertson RAF Wing Commander C Cummings Editor & Publications Wing Commander C G Jefford MBE BA Manager *Ex Officio 4 CONTENTS EARLY HISTORICAL PERSPECTIVES AND EMERGING 8 STAFF TARGETS by Air Chf Mshl Sir Patrick Hine JET LIFT by Prof John F Coplin 14 EVOLUTION OF THE PEGASUS VECTORED -
The Power for Flight: NASA's Contributions To
The Power Power The forFlight NASA’s Contributions to Aircraft Propulsion for for Flight Jeremy R. Kinney ThePower for NASA’s Contributions to Aircraft Propulsion Flight Jeremy R. Kinney Library of Congress Cataloging-in-Publication Data Names: Kinney, Jeremy R., author. Title: The power for flight : NASA’s contributions to aircraft propulsion / Jeremy R. Kinney. Description: Washington, DC : National Aeronautics and Space Administration, [2017] | Includes bibliographical references and index. Identifiers: LCCN 2017027182 (print) | LCCN 2017028761 (ebook) | ISBN 9781626830387 (Epub) | ISBN 9781626830370 (hardcover) ) | ISBN 9781626830394 (softcover) Subjects: LCSH: United States. National Aeronautics and Space Administration– Research–History. | Airplanes–Jet propulsion–Research–United States– History. | Airplanes–Motors–Research–United States–History. Classification: LCC TL521.312 (ebook) | LCC TL521.312 .K47 2017 (print) | DDC 629.134/35072073–dc23 LC record available at https://lccn.loc.gov/2017027182 Copyright © 2017 by the National Aeronautics and Space Administration. The opinions expressed in this volume are those of the authors and do not necessarily reflect the official positions of the United States Government or of the National Aeronautics and Space Administration. This publication is available as a free download at http://www.nasa.gov/ebooks National Aeronautics and Space Administration Washington, DC Table of Contents Dedication v Acknowledgments vi Foreword vii Chapter 1: The NACA and Aircraft Propulsion, 1915–1958.................................1 Chapter 2: NASA Gets to Work, 1958–1975 ..................................................... 49 Chapter 3: The Shift Toward Commercial Aviation, 1966–1975 ...................... 73 Chapter 4: The Quest for Propulsive Efficiency, 1976–1989 ......................... 103 Chapter 5: Propulsion Control Enters the Computer Era, 1976–1998 ........... 139 Chapter 6: Transiting to a New Century, 1990–2008 .................................... -
AEROMOTIVE Part 2
AEROMOTIVE Part 2 What is an aircraft engine? A child might answer, "an engine that's on an aeroplane." Foolish youth! If we skip the radials, rotarys, sleeve valvers, two strokes, diesels, turbines, jets, and rockets, we're left with . the four cycle, internal combustion, spark ignited, piston reciprocating, poppet valvers, in only; aircooled, liquid cooled, inline, opposed, vee, naturally aspirated, and supercharged gasoline consuming variations. These qualifications squeeze the answer into a set of characteristics that appears remarkably like an automotive engine to enthusiastic people. Back To The Basics: We can attempt to equate engine performance in a variety of ways. However, horsepower still seems to be the best method if it is qualified by an accompanying RPM (revolutions/minute). Power output in HP/CID (horsepower/cubic inch displacement) is a standard for most engine nerds but it doesn't reveal much about the drivability (torque) or personality (horsepower curve) of the engine. Torque and horsepower are intimately related even though they are often spoken of as if they were separate entities. I have taught a private engine design and building course for 21 years and it has always been a challenge to get my students to understand the relationship between torque and horsepower. This doesn't surprise me because these two parameters, ostensibly simple, are in fact tricky to relate. I am reluctant to rehash the whole horsepower/torque issue. But, based on conversations I have had with aircraft folks - and automotive folks, for that matter - I perceive the need to establish basic terms. We (“we” meaning us at Sunset Engine Development) are often asked, "what do I want, torque or horsepower?" Trying to explain such abstract concepts on the telephone cannot do the subject justice. -
Napier Sabre Engines Will Be Found on Page L75
STAITDARDIZRD DATA PAGES FOR RECIPROCATIITG EITCTI\ES Standardized data pages are used to present the specifieations of the basic aircraft engines and airhorne auxiliary units described and illustrated in the followirg section of the book. The arrangeme'nt of the data on the standardi zed" data pages is as f ollows : First, there is a concise description of the engine, its construe tion and the major accessories with which it is equipped. Then, in tabular form, there are items such as bore, stroke, displacement (swept vol- ume), compression ratio, overall dimensions, frontal areae total weight and weight per maximum horsepolyer. F'uel and lubricating oiX eonsumptions at cruising output are given in units of weight. The fuel grade and the viscosity of the lubricating oil at 210o F" (100o C) also are specified. Efficiency figures such as maximum power output per unit of dis- placement, maximum polver output per unit of piston area) maximum piston speed and maximum brake mean effective pressure have been ealculated for comparative purposes. Finally, the various horsepower ratings of the engine are given, such as; Take-off rating, or the maxinrum horsepower which it is per- missibil to ,ruJ at sea level and at low altitrdes. flrlilitary (combat) rating, or the maximum horsepower which it is perrnissib]e to use for military purposes at various alti- tudes. fVorrual rating,, or the ntaximum horsepower which the engine can deliver continuously for climh without undue stress" Cruising ratirug, or the maximum horsepo\,ver recommended for continuous operation consistent with reasonable fuel econ- omy. Ern,ergerlcy rating, or the marximum horsepower which it is permissible use a _ to for short period of time in an ernergency. -
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. -
ENGINEERS' WALK in BRISTOL (Blue Plaques)
Supplement to the Histelect News No. S75 August 2020 ENGINEERS’ WALK IN BRISTOL (Blue Plaques) - Part 1 by John Coneybeare There were three reasons why I suggested that the Retired Professional Engineers Club (now sadly closed) should set this up. a) In Sydney I saw the recently commenced series of pavement mounted plaques, celebrating famous Australian Writers at Circular Quay. b) The Retired Chartered Engineer’s Club in Exeter had already erected wall mounted plaques in their city and kindly showed me around. c) Bristol was planning to celebrate the bi-centenary of Isambard Kingdom Brunel’s birth in 2006. There are now 15 plaques erected on walls belonging to a science museum in Bristol called ‘We the Curious’. We are indebted to this museum for their great support. The following are mini biographies but you can see more by visiting engineerswalk.co.uk. _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ Samuel Plimsoll (1824 – 1898) Mr John Chambers, of a mine owning family, gave him another chance. Following the Plimsoll was born in Bristol but by his teens dismissal of corrupt staff there was the family lived in Sheffield. He wanted to be cooperation between GNR and Plimsoll. a coal merchant exporting coal to Kings Plimsoll designed and built a revolutionary Cross, London by rail. -
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. -
Napier Sabre VII
55° FLIGHT Napier Sabre VII Over 3,000 b.h.p. for Take-off tLowest Specific Weight of Any Pro- duction Piston Engine EGULAR readers of Flight may remember that a octane fuel are no longer burned to produce only hot water, detailed description of the Sabre engine was given which is immediately cooled again; by using regenerative R in the March 23rd, 1944, issue, together with a good dynamometers the power output is used to produce elec- many illustrations, including a special cut-away drawing; tricity for the factory and outside supply, and an example but the subject of that description was the Mk. II, whereas of the output is that if a Sabre is running on a Sunday the latest Sabre is the Mk. VII. (when the factory is not working) the electricity generated Series II engines were developed in three guises, the II, by a single engine is sufficient to supply the entire demand IIA and IIB, in which the boost pressures were progressively from the whole Willesden area and still leave sufficient increased and the power outputs stepped-up from 2,090 over for feeding into the national grid system. to 2,220 and then to 2,420 b.h.p. Weight had also in- creased, but not proportionally, so that specific weight Teetliing Troubles Cured went down respectively from 1.12 to 1.06 until, with the As with all engines developed at high pressure during IIB, it dropped below unity with the value of 0.981b. /b.h.p. the war, teething troubles were experienced with the Sabre.