The Aircraft Engine: an Historical Perspective of Engine Development Through World War I
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Aircraft Engine Performance Study Using Flight Data Recorder Archives
Aircraft Engine Performance Study Using Flight Data Recorder Archives Yashovardhan S. Chati∗ and Hamsa Balakrishnan y Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 - 223 is used to study the variation of normalized engine performance parameters with the altitude profile in all the phases of flight. A turbofan performance analysis model is employed to calculate the theoretical thrust and it is shown to be a good qualitative match to the FDR reported thrust. The operational thrust settings and the times in mode are found to differ significantly from the ICAO standard values in the LTO cycle. This difference can lead to errors in the calculation of aircraft emission inventories. This paper is the first step towards the accurate estimation of engine performance and emissions for different aircraft and engine types, given the trajectory of an aircraft. I. Introduction Aircraft emissions depend on engine characteristics, particularly on the fuel flow rate and the thrust. It is therefore, important to accurately assess engine performance and operational fuel burn. Traditionally, the estimation of fuel burn and emissions has been done using the ICAO Aircraft Engine Emissions Databank1. However, this method is approximate and the results have been shown to deviate from the measured values of emissions from aircraft in operation2,3. -
A Short History of the Royal Aeronautical Society
A SHORT HISTORY OF THE ROYAL AERONAUTICAL SOCIETY Royal Aeronautical Society Council Dinner at the Science Museum on 26 May 1932 with Guest of Honour Miss Amelia Earhart. Edited by Chris Male MRAeS Royal Aeronautical Society www.aerosociety.com Afterburner Society News RAeS 150th ANNIVERSARY www.aerosociety.com/150 The Royal Aeronautical Society: Part 1 – The early years The Beginning “At a meeting held at Argyll Lodge, Campden Hill, Right: The first Aeronautical on 12 January 1866, His Grace The Duke of Argyll Exhibition, Crystal Palace, 1868, showing the presiding; also present Mr James Glaisher, Dr Hugh Stringfellow Triplane model W. Diamond, Mr F.H. Wenham, Mr James Wm. Butler and other exhibits. No fewer and Mr F.W. Brearey. Mr Glaisher read the following than 77 exhibits were address: collected together, including ‘The first application of the Balloon as a means of engines, lighter- and heavier- than-air models, kites and ascending into the upper regions of the plans of projected machines. atmosphere has been almost within the recollection A special Juror’s Report on on ‘Aerial locomotion and the laws by which heavy of men now living but with the exception of some the exhibits was issued. bodies impelled through air are sustained’. of the early experimenters it has scarcely occupied Below: Frederick W Brearey, Wenham’s lecture is now one of the aeronautical Secretary of the the attention of scientific men, nor has the subject of Aeronautical Society of Great classics and was the beginning of the pattern of aeronautics been properly recognised as a distinct Britain, 1866-1896. -
View Sample Pages
Ebook Code REAU5044 SAMPLE Contents Teachers' Notes 4 Comprehension Activity 1 26 Curriculum Links 5 Comprehension Activity 2 27 Flights into Space 1 28 SECTION 1: LAND Flights into Space 2 29 Early Car Design Space Technology 30 The Innovations of Otto, Langen and Wankel 7 Space Activity 1 31 Comprehension Activity 8 Space Activity 2 32 Creative Activity 9 Space Activity 3 33 Modern Car Design Top Secret Space Plane 34 Piston Engines 10 Piston Engines Activity 11 SECTION 3: SEA Gears 12 Under the Water Gears Template 13 Submarines 36 Technology and the Environment 14 Submarine Activity 37 Technology and the Environment Activity 15 Diesel Electric and Nuclear Submarines 1 38 Diesel Electric and Nuclear Submarines 2 39 Cars of the Future Comparing Early and Modern Submarines 40 Future Designs 16 Comparing Early and Modern Submarines Future Designs Activity 17 Activity 41 Future Designs 2 18 Life in a Modern Submarine 1 42 Future Designs Activity 2 19 Life in a Modern Submarine 2 43 Nuclear Submarines and the Environment 44 SECTION 2: AIR SAMPLEOther Submarines 45 Aircraft Design Submarine Stories 46 Aerodynamic Forces 22 Build a Submarine 47 Aerodynamic Forces Activity 23 Examining Technological Leaps Answers 48 The Technological Innovations of the Wright Brothers 24 The Flyer and The Modern Day Airbus 25 3 Teachers’ Notes Fantastic Inventions examines how past, current The Air Section focuses on the Wright brothers’ and future inventions consistently affect our early plane. This method of transport is modes of transport, our lifestyles and the compared to the Boeing 747 and the new environment. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
Tethered Fixed-Wing Aircraft to Lift Payloads…
Tethered Fixed-Wing Aircraft to Lift Payloads: A Concept Enabled by Electric Propulsion David Rancourt Etienne Demers Bouchard Université de Sherbrooke Georgia Institute of Technology 3000 boul. Université – Pavillon P2 275 Ferst Drive NW Sherbrooke, QC Atlanta, GA CANADA USA [email protected] [email protected] Keywords: Electric propulsion, novel aircraft concept, VTOL, hybrid-electric powertrain ABSTRACT Helicopters have been essential to the military as they have been one of the only solutions for air-transporting substantial payloads with no need for complex mile-long runway infrastructures. However, they are fundamentally limited with high fuel consumption and reduced range. A disruptive concept to vertical lift uses tethered fixed-wing aircraft to lift a payload, where multiple aircraft collaborate and fly along a near circular flight path in hover. The Electric-Powered Reconfigurable Rotor concept (EPR2) leverages the recent progress in electric propulsion and modern controls to enable efficient load lifting using fixed-wing aircraft. The novel idea is to replace tethered manned aircraft (with onboard energy, fuel) with electric-powered fixed-wing aircraft with remote energy source to enable efficient collaborative load lifting. This paper presents the conceptual design of a heavy-lifting aircraft concept using electric-powered tethered fixed-wing aircraft for a ~30 metric ton lifting capability. A physics-based multidisciplinary design and simulation environment is used to predict the performance and optimize the aircraft flight path. It is demonstrated that this concept could hover with only 3.01 MW of power yet be able to translate to over 80 kts with minimal power increase by leveraging the benefits of complex non-circular flight paths. -
Wankel Powered Time to Climb World Record Attempt
Wankel powered time to climb world record attempt Presentation at Aero Expo, Friedrichshafen, Germany April 19th, 2018 by Paul Lamar Several years ago an American rotor head by the name of Russ MacFarlane living in Newcastle Australia decided to build a Mazda rotary powered world record attempt time to climb aircraft. Russ was a long time subscriber to the Rotary Engine News Letter. A used flying Harmon Rocket home built aircraft was purchased and the Lycoming engine and instruments were removed and sold. The aircraft is very similar to a Van's RV4 with longer landing gear and shorter wings. Dan Grey, owner of Aviation FX in Santa Paula California was chosen to finish the project and get it flying. I was the project engineer. Dan is a 787 captain for UAL. The Wankel rotary has a much better power to weight ratio and power to size ratio than any automotive piston engine. It is also far more robust and will withstand ungodly amounts of turbo boost with out structural failure. Up to 100 inches of Mercury manifold pressure is possible. That translates to almost 1000 HP for an all aluminum turbo two rotor weighing less than 200 pounds. That is about four HP per pound of engine weight. Most aircraft engines are about one HP per pound of weight or worse. Any piston engine operating at aircraft power levels has a limited life. That is the reason for a TBO. The moving parts are magnafluxed for cracks at TBO. The cracks are caused by reversing stress on the crankshaft, connecting rods, pistons and valve parts. -
History of Solar Flight July 2008
History of Solar Flight July 2008 solar airplane aircraft continuous sustainable flight solar-powered solar cells mppt helios Sky-Sailor sun-powered HALE platform solaire avion vol continu dévelopement durable énergie solaire cellules plateforme History of Solar flight André Noth, [email protected] Autonomous Systems Lab, Swiss Federal Institute of Technology Zürich 1. The conjunction of two pioneer fields, electric flight and solar cells The use of electric power for flight vehicles propulsion is not new. The first one was the hydrogen- filled dirigible France in year 1884 that won a 10 km race around Villacoulbay and Medon. At this time, the electric system was superior to its only rival, the steam engine but then with the arrival of gasoline engines, work on electrical propulsion for air vehicles was abandoned and the field lay dormant for almost a century [2]. On the 30th June 1957, Colonel H. J. Taplin of the United Kingdom made the first officially recorded electric powered radio controlled flight with his model “Radio Queen”, which used a permanent-magnet motor and a silver-zinc battery. Unfortunately, he didn’t carry on these experiments. Further developments in the field came from the great German pioneer, Fred Militky, who first achieved a successful flight with a Radio Queen, 1957 free flight model in October 1957. Since this premises, electric flight continuously evolved with constant improvements in the fields of motors and batteries [12]. Three years before Taplin and Militky’s experiments, in 1954, photovoltaic technology was born at Bell Telephone Laboratories. Daryl Chapin, Calvin Fuller, and Gerald Pearson developed the first silicon photovoltaic cell capable of converting enough of the sun’s energy into power to run everyday electrical Gerald Pearson, Daryl Chapin equipment. -
Air-Breathing Engine Precooler Achieves Record-Breaking Mach 5 Performance 23 October 2019
Air-breathing engine precooler achieves record-breaking Mach 5 performance 23 October 2019 The Synergetic Air-Breathing Rocket Engine (SABRE) is uniquely designed to scoop up atmospheric air during the initial part of its ascent to space at up to five times the speed of sound. At about 25 km it would then switch to pure rocket mode for its final climb to orbit. In future SABRE could serve as the basis of a reusable launch vehicle that operates like an aircraft. Because the initial flight to Mach 5 uses the atmospheric air as one propellant it would carry much less heavy liquid oxygen on board. Such a system could deliver the same payload to orbit with a vehicle half the mass of current launchers, potentially offering a large reduction in cost and a higher launch rate. Reaction Engines' specially constructed facility at the Colorado Air and Space Port in the US, used for testing the innovative precooler of its air-breathing SABRE engine. Credit: Reaction Engines Ltd UK company Reaction Engines has tested its innovative precooler at airflow temperature conditions equivalent to Mach 5, or five times the speed of sound. This achievement marks a significant milestone in its ESA-supported Airflow through the precooler test item in the HTX heat exchanger test programme. UK company Reaction development of the air-breathing SABRE engine, Engines has tested its innovative precooler at airflow paving the way for a revolution in space access temperature conditions equivalent to Mach 5, or five and hypersonic flight. times the speed of sound. This achievement marks a significant milestone in the ESA-supported development The precooler heat exchanger is an essential of its air-breathing SABRE engine, paving the way for a SABRE element that cools the hot airstream revolution in hypersonic flight and space access. -
Winter 2016 Issue No 128
The Oily Rag! Photo Peter Nicholson Tony Newberry surrounded by some of the locos he has built at a celebration of his achievements at Coate Water Miniature Railwa y Peter Nicholson and Joshua Brinsford report WinterWinter 2016 Issue No 128 TheThe Taunton Model Engineers’ magazinemagazine 1 ContentsContents 3. From the Editor 3. Chairman’s Notes 5. News from Creech 7. Report from Vivary Park 9. Steam powered aircraf t By William Pickering Do you believe this? 14. Robin No. 6 By Tim Griffiths Would you like to be involved with rebuilding this loco? 16. “On the footplate” The art of stopping By Ray Rolt Ray brings his experiences on the S&DR to a halt. 20. Tony Newberry honoured at Coate Miniature Railway A report by Peter Nicholson and Joshua Brinsfo rd 23. “Tich 2.5” By John Pickering A new take on a classic design. 25. Little puffers way By Tim Griffiths Tim’s early days in South London 28. Of ships and things By Fireman M.N. retired Clean clothes and black smoke 2 From the Editor Tony Newberry is probably our most prolific model engineer. On the weekend of the 13th and 14th August an event was held at the North Wilts Model Engineering Society’s Coate Water Miniature Railway to celebrate his achievements. Peter Nicholson and Joshua Brinsford report on this event. This issue has nostalgia with pieces from Tim Griffiths and fireman MN retd. Ray Rolt complet es his series on driving on the S&DR. appropriately with the “art of stopping”. To fill the pages I was able to call on a source from beyond the grave. -
Design of a Micro-Aircraft Glider
Design of A Micro-Aircraft Glider Major Qualifying Project Report Submitted to the faculty of WORCESTER POLYTECHNIC INSTITUTE In partial fulfillment of the requirements for The Degree of Bachelor of Science Submitted by: ______________________ ______________________ Zaki Akhtar Ryan Fredette ___________________ ___________________ Phil O’Sullivan Daniel Rosado Approved by: ______________________ _____________________ Professor David Olinger Professor Simon Evans 2 Certain materials are included under the fair use exemption of the U.S. Copyright Law and have been prepared according to the fair use guidelines and are restricted from further use. 3 Abstract The goal of this project was to design an aircraft to compete in the micro-class of the 2013 SAE Aero Design West competition. The competition scores are based on empty weight and payload fraction. The team chose to construct a glider, which reduces empty weight by not employing a propulsion system. Thus, a launching system was designed to launch the micro- aircraft to a sufficient height to allow the aircraft to complete the required flight by gliding. The rules state that all parts of the aircraft and launcher must be contained in a 24” x 18” x 8” box. This glider concept was unique because the team implemented fabric wings to save substantial weight and integrated the launcher into the box to allow as much space as possible for the aircraft components. The empty weight of the aircraft is 0.35 lb, while also carrying a payload weight of about 0.35 lb. Ultimately, the aircraft was not able to complete the required flight because the team achieved 50% of its desired altitude during tests. -
An Ancient Air – John Stringfellow
AnAirlife CLASSIC AN ANCIENT AIR The invention all admired and each how he To be the inventor missed; so easy it seemed Once found, which yet unfound Most would have thought impossible. Milton BIOGRAPHY (JL THE VICTORIAN AERONAUTICAL HARALD PEMRUbfc AnAirlife CLASSIC Copyright © 1988 Harald Penrose First published in the UK in 1988 by Airlife Publishing Ltd This edition published 2000 British Library Cataloguing-in-Publication Data A catalogue record for this book is available from the British Library ISBN 1840371846 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. Printed in England by St Edmundsbury Press Ltd, Bury St Edmunds, Suffolk Airlife Publishing Ltd 101 Longden Road, Shrewsbury, SYS 9EB, England E-mail: [email protected] Website: www.airlifebooks.com Contents Acknowledgements Chronology Foreword 9 Chapter 1 Age of Industrial Development 17 Chapter 2 Days of the Reform Bill 23 Chapters Scheming a Powered Flyer 31 Chapter 4 Publicity Manoeuvring 55 Chapter 5 Trial and Tribulation 63 Chapter 6 Epochal Independent Success 70 Chapter 7 Continuing Development 76 Chapter 8 The Great Exhibition 94 Chapter 9 A Valued Friendship 122 Chapter 10 A Wonderful Old Gentleman 135 Chapter 11 His Son Continues the Quest 154 Chapter 12 An End and a Beginning 168 Index 179 Acknowledgements Introducing some of the many who assisted The route to a biography is long and tortuous and requires the help of many people. -
Ammonia Powered Engine
Ammonia Powered Engine A Major Qualifying Project Submitted to the faculty of Worcester Polytechnic Institute In partial fulfillment of the requirements for the Degree in Bachelor of Science In Mechanical Engineering By: ___________________________ Alexander James Baldino ___________________________ Brendan Walter Gallagher ___________________________ Hayden George Furcolo Date: 5/18/2020 Project Advisor ___________________________ Professor Robert Daniello Acknowledgements We would like to thank our project advisor Professor Robert Daniello for his knowledge and guidance throughout our entire MQP process. We would also like to thank Barbara Fuhrman of the Mechanical Engineering Office for her help in acquiring material for our project and her dedication to our success. Additionally, we would like to thank Ian Anderson and James Loiselle, as well as the entirety of the Washburn Shops staff, for their help during our manufacturing processes. 1 | P a g e Abstract Cars are a significant source of carbon emissions into the atmosphere and with a growing number of cars on the road, this is negatively affecting the atmosphere. The carbon emissions cars emit comes from the gasoline being burned in the engine. While battery/electrics provide one solution, energy density and speed of refueling are favorable with internal combustion engines. A potential candidate for replacing hydrocarbons as the fuel for combustion engines is ammonia. A molecule of ammonia is composed of one nitrogen atom and three hydrogen atoms producing nitrogen gas and water upon combustion. Neither product of combustion is harmful to our environment and the ammonia itself can be produced through “green” renewable energy processes. Using a small engine from a snow blower, we aimed to modify the engine to run off of ammonia as the fuel source.