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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. -
04Aug00-Ieee-Spaceshipone
News Analysis IEEE Spectrum magazine August 2004 A Giant Leap For Commercial Space Travel Pioneering aerospace designer Burt Rutan claims early lead in race for Ansari X Prize Looking like something out of a Japanese sci-fi cartoon, the futuristic space plane dropped from its mother ship 14 kilometers above Edwards Air Force Base, east of Mojave, Calif., and lit its rocket engine. The winged craft shot straight up, up, and still up, marked by a milky white smoke trail. It didn't curve toward any horizon, the way most rockets do, as they head toward a stable orbit as quickly as possible. More than 30 000 viewers in the desert tilted their heads back farther and farther, mouths agape, necks starting to ache, for the 76 seconds that pilot Michael W. Melvill let the engine burn. It was the most momentous suborbital hop since Alan Shepard rode his Freedom 7 capsule to an altitude of 187.4 km in 1961. IEEE Spectrum was on hand at Mojave Airport in California on 21 June for the launch of the unusual privately funded space plane, SpaceShipOne, which was designed by Burt Rutan and his team at Scaled Composites LLC in Mojave. Paul Allen, Microsoft Corp.'s cofounder, funded Rutan's project, ostensibly to win the US $10 million Ansari X Prize for the first workable "space tourist" vehicle. But Rutan and Allen's gaze was directed far beyond that prize. Considering they spent more than twice as much money as they could win, clearly they were looking to participate in a future of commercial space travel for ordinary—albeit rich—people. -
PRESS RELEASE Safran Appointments
PRESS RELEASE Safran appointments June 28, 2021 Two appointments to Safran's Executive Committee Effective July 1, 2021, Stéphane Cueille is named CEO of Safran Electrical & Power. He takes over from Alain Sauret, who is retiring. Olivier Andriès, CEO of Safran, said, “I would like to sincerely thank Alain Sauret, who joined the Group almost 40 years ago at our legacy company, Labinal. He went on to transform the company into a world-class center of electrical system excellence. Safran Electrical & Power is today a cornerstone of our decarbonized aviation roadmap.” Holding the rank of Ingénieur de l’Armement (defense scientist), Stéphane Cueille was seconded to Snecma1 from 1998 to 2001 to work on ceramic matrix composites (CMC). He returned to the French defense procurement agency DGA in 2001, taking various management positions in the aircraft propulsion sector. In 2005 he was placed in charge of the Missiles-Space unit in the industrial affairs department (S2IE). In 2008, he returned to Snecma, starting in the turbine blade quality department at the Gennevilliers plant. He was subsequently named repair general manager in Snecma’s Military Engine division, then director of the turbine blade center of excellence. / Safran Mereis / Capa/ Safran/ MereisCapa/ Safran / In May 2013 he was appointed Managing Director of Aircelle Ltd, the UK subsidiary of Aircelle2 based in Burnley. In January 2015 he was named head of Safran Tech, the Stéphanie Group's Research & Technology (R&T) center, and then in 2016 was appointed Senior Executive Vice President R&T and Christophe Innovation, also becoming a member of the Safran Executive © Committee. -
Where Every Child Thrives 2012 Annual Report 1 2 3 Annual Giving 2012 Fiscal Year Ending August 31, 2012
Where every child thrives 2012 Annual Report 1 2 3 ANNUAL GIVING 2012 Fiscal Year Ending August 31, 2012 Individuals ........................$599, 532 Corporations, Foundations, Organizations and Government ...................$1,746,059 Event..................................$495,163 Gifts In Kind .......................$201,478 Legacies and Bequests .....$78, 893 Total ...............................$3,121,125 Thank you to Meeting Street’s special circle of friends Gifts and support received in fiscal year 2012 (September 1, 2011 – August 31, 2012) Individual Giving Mr. and Mrs. Michael J. Angelakis Ms. Carol A. Peterson Mrs. Lucille A. Cavan Mr. and Mrs. David Sluter Premier Circle $50,000+ Mr. and Mrs. Arnold B. Chace, Jr. One donor wished to remain anonymous The Carter Family Charitable Trust Malcolm G. Chace, Jr. *denotes deceased One donor wished to remain anonymous John and Karen Galvin Bryce and Gloria Hall Touching Hearts Circle $1,000+ Majestic Circle $25,000+ Mr. and Mrs. James Joy, II Ms. Ellen J. Alexander Frank Decedric Charitable Trust Mr. John M. Kelly Mr. Edward A. Allsop Mr. and Mrs. Thomas M. Ryan The John Marshall Family Mr. Steven Alves Estate of Wiacheslav A. O. Thompson Adelaide and Paul Nicholson Mr. and Mrs. Arthur H. Audette Estate of Dorothy E. Wolstenholm Dr. Michael A. Rocchio Mrs. Lynne Burke One donor wished to remain anonymous Estate of W.E. Thompson Daniel C. Bryant and Elizabeth Burke Bryant Three donors wished to remain anonymous Mr. and Mrs. Thomas G. Carmody Helping Hands Circle $10,000+ The Honorable David N. Cicilline Estate of Loretta Beauvais Goucher Changing Lives Circle $2,500+ Mrs. Monika I. Clark Rena Burney Fund Jill and John Andy Ms. -
Chemical Engineering Education Graduate Education in Chemical Engineering
I • N • D • E • X GRADUATE EDUCATION ADVERTISEMENTS Akron, Uni versity of. .......... , .... ... .................. 321 Iowa State Uni versity .................. ... ....... ....... 360 Pensylvania State Uni versity ........................ 395 Alabama, University of ................................ 322 Johns Hopkins University .... .... .. .... .... .......... 361 Pittsburgh, University of .............................. 396 Alabama, Huntsville; Uni versity of.. .... .. ..... 323 Kansas, University of ............................... .... 362 Polytechnic University .. .... ... .... ........... .. ..... .. 397 Alberta, Uni versity of .. ........ .... .. .... ... ..... ..... .. 324 Kansas State University ............... ... ...... ........ 363 Princeton University ....................... .......... .. .. 398 Arizona, University of ....... .. .... .. .... ... .. ... ....... 325 Kentucky, Uni versity of ........................ .. ..... 364 Purdue University .. ........... ... ... ....... ... .... .... ... 399 Arizona State University ..... .. ... ...... ..... ......... 326 Lamar University .. ... ..... ..... ......... ........... .. ..... 430 Rensselaer Polytechnic Institute .... ...... .... ... .. 400 Auburn Uni versity .. ..... .. ... ..... .. .............. .... ... 327 Laval Universite ...................... ........... ...... .. .. 365 Rhode Island, University of.. .... ..... .. ... ..... .. ... 435 Bri gham Young Uni versity .............. ... .. ..... ... 427 Lehigh University .................................. .... ... 366 Rice University -
Safran Aircraft Engines Download
SAFRAN AIRCRAFT ENGINES This is a multi-site certificate, additional site details are listed in the appendix to this certificate 10 ALLEE DU BREVENT - COURCOURONNES 91019 EVRY CEDEX - FRANCE Bureau Veritas Certification certify that the Management System of the above organisation has been audited in accordance with the relevant Aerospace Supplier Quality system Certification Scheme EN 9104-001:2013 and found to be in accordance with the requirements of the management system standard detailed below: Standard EN 9100:2018 AS 9100:D - JISQ 9100:2016 Scope of certification DESIGN, DEVELOPMENT, PRODUCTION, DISTRIBUTION, TEST AND SERVICING OF CIVIL AND MILITARY AIRCRAFT ENGINES - DESIGN, DEVELOPMENT, PRODUCTION, DISTRIBUTION, TEST AND SERVICING SATELLITE AND SPACECRAFT PROPULSION SYSTEMS - ASSOCIATED SERVICES PROVIDED TO CIVIL AND MILITARY CUSTOMERS. Certification structure : Campus Certification Issue date: 15 September 2018 Subject to the continued satisfactory operation of the organization’s Management System, this certificate expires on (Certification Expiry date): 14 September 2021 Original certification date: 15 July 2004 Certificate : 7098050-Rev0 Date: 06 September 2018 File number : FR044707-1 Jacques Matillon – Managing DIrector Bureau Veritas Certification France 60, avenue du Général de Gaulle – Immeuble Le Guillaumet - 92046 Paris La Défense Further clarifications regarding the scope of this certificate the applicability of the management system requirements may be obtained by consulting the organization. To check this certificate validity, please call + 33(0) 1 41 97 00 60. APPENDIX SAFRAN AIRCRAFT ENGINES Standard EN 9100:2018 AS 9100:D - JISQ 9100:2016 Scope of certification Site Address Scope 10 ALLEE DU BREVENT COURCOURONNES SIEGE CENTRAL FUNCTIONS 91019 EVRY CEDEX, France RUE HENRI AUGUSTE INDUSTRIALIZATION AND MANUFACTURING OF PARTS AND EVRY-CORBEIL DESBRUÈRES - BP 81 COMPONENTS FOR AIRCRAFT ENGINES. -
Sheepshead Bay, Brooklyn, NY 11235
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Aviation Week & Space Technology
$14.95 JUNE 29-JULY 12, 2020 Quest for Speed BOOM XB-1 TAKES SHAPE RICH MEDIA EXCLUSIVE Europe’s Hydrogen- Powered Aircraft Push PRIME TIME FOR How Safe Are HYPERSONICS Aircraft Cabins? Canada’s Fighter RICH MEDIA EXCLUSIVE Strategy Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa. -
Flight International – July 2021.Pdf
FlightGlobal.com July 2021 RISE of the open rotor Airbus, Boeing cool subsidies feud p12 Home US Air Force studies advantage resupply rockets p28 MC-21 leads Russian renaissance p44 9 770015 371327 £4.99 Sonic gloom Ton up Investors A400M gets pull plug a lift with on Aerion 100th delivery 07 p30 p26 Comment All together now Green shoots Irina Lavrishcheva/Shutterstock While CFM International has set out its plan to deliver a 20% fuel saving from its next engine, only the entire aviation ecosystem working in concert can speed up decarbonisation ohn Slattery, the GE Aviation restrictions, the RISE launch event governments have a key role to chief executive, has many un- was the first time that Slattery and play here through incentivising the doubted skills, but perhaps his Safran counterpart, Olivier An- production and use of SAF; avia- the least heralded is his abil- dries, had met face to face since tion must influence policy, he said. Jity to speak in soundbites while they took up their new positions. It He also noted that the engine simultaneously sounding natural. was also just a week before what manufacturers cannot do it alone: It is a talent that politicians yearn would have been the first day of airframers must also drive through for, but which few can master; the Paris air show – the likely launch aerodynamic and efficiency im- frequently the individual simply venue for the RISE programme. provements for their next-genera- sounds stilted, as though they were However, out of the havoc tion products. reading from an autocue. -
Getting Shipshape
AER October 2020 OSPACE DOES AEROSPACE HAVE A RACE PROBLEM? SECRETS FROM THE FALKLANDS AIR WAR POWERING UP ELECTRIC FLIGHT www.aerosociety.com October 2020 GETTING SHIPSHAPE Volume 47 Number 10 Volume UK F-35B FORCE GETS READY FOR FIRST OPERATIONAL CARRIER DEPLOYMENT Royal AeronauticaSociety OCTOBER 2020 AEROSPACE COVER FINAL.indd 1 18/09/2020 14:59 RAeS 2020 Virtual Conference Programme Join us from wherever you are in the world to experience high quality, informative content. Book early for our special introductory offer rates. STRUCTURES & MATERIALS UAS / ROTORCRAFT / AIR TRANSPORT GREENER BY DESIGN 7th Aircraft Structural Urban Air Mobility RAeS Climate Change Design Conference Conference 2020 Conference 2020 DATE NEW DATE DATE 8 October 22 - 23 October 3 - 4 November TIME TIME TIME 14:00 - 17:00 13:00 - 18:00 13:00 - 18:00 SCAN USING SCAN USING SCAN USING YOUR PHONE YOUR PHONE YOUR PHONE FOR MORE INFO FOR MORE INFO FOR MORE INFO Embark on your virtual learning journey with the RAeS Connect and interact with our speakers and ask questions live Engage and network with other professionals from across the world Meet our sponsors at our virtual exhibitor booths Access content post-event to continue your professional development For the full virtual conference programme and further details on what to expect visit aerosociety.com/VCP Volume 47 Number 10 October 2020 EDITORIAL Contents When global rules unravel Regulars 4 Radome 12 Transmission What price global standards, rules and regulations? Pre-pandemic there were The latest aviation and Your letters, emails, tweets aeronautical intelligence, and social media feedback. -
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. -
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.