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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. -
Ivchenko Progress
® AdvancedAdvanced turboprop,turboprop, propfanpropfan andand turbojetturbojet bypassbypass enginesengines forfor GAGA andand lightlight airplanesairplanes S. DMYTRIYEV 23.11.09 ® HISTORY ZAPOROZHYE MACHINE-BUILDING DESIGN BUREAU PROGRESS STATE ENTERPRISE NAMED AFTER ACADEMICIAN A.G. IVCHENKO (SE IVCHENKO-PROGRESS) Foundation date: May 5, 1945 Over a whole past period, engine manufacturing plants have produced more than 80 , 000 aircraft gas turbine and piston engines, turbostarters and industrial plants. Today, the engines designed by SE IVCHENKO-PROGRESS power 57 types of flying vehicle in 109 countries. Over the years, SE IVCHENKO-PROGRESS engines logged more than 300 million flight hours. © SE Ivchenko-Progress, 2009 2 ® HISTORY D-27 propfan , ÒV3-117 VÌÀ- SBÌ1 turboprop , D-436 turbofan , AI -22 turbofan , AI -222 turbofan , AI -450 turboshaft , 4-th stage AI -450 turboprop , SPM-21 turbofan Turbofans with high power and thrust : 3- rd stage D-136, D-18Ò Turbofans : AI -25, AI -25ÒË, D-36 2-nd stage APUs: AI -9, AI -9 V Turboprops : AI -20, AI -24 1- st stage APU: AI -8 Piston engines: AI -26 , AI-14, AI-4 © SE Ivchenko-Progress, 2009 3 ® DIRECTIONS OF ACTIVITY CIVIL AVIATION: commercial aircraft and helicopters Ìè-2Ì Àí-140 Àí-14 8 STATE AVIATION : trainers and combat trainers, military transport aircraft and helicopters , multipurpose aircraft ßê-18Ò Àí-70 Ìè-26Ò ßê-130 Áe-200 Àí-124 © SE Ivchenko-Progress, 2009 4 ® THE BASIC SPHERES OF ACTIVITIES DESIGN MANUFACTURE OVERHAUL TEST AND DEVELOPMENT PUTTING IN SERIES PRODUCTION AND IMPROVEMENT OF CONSUMER'S CHARACTERISTICS © SE Ivchenko-Progress, 2009 5 INTERNATIONAL RECOGNITION OF ® CERTIFICATION AUTHORITIES Totally 60 certificates of various types European Aviation Safety Agency (Germany) Certificate No. -
Robust Gas Turbine and Airframe System Design in Light of Uncertain
Robust Gas Turbine and Airframe System Design in Light of Uncertain Fuel and CO2 Prices Stephan Langmaak1, James Scanlan2, and András Sóbester3 University of Southampton, Southampton, SO16 7QF, United Kingdom This paper presents a study that numerically investigated which cruise speed the next generation of short-haul aircraft with 150 seats should y at and whether a con- ventional two- or three-shaft turbofan, a geared turbofan, a turboprop, or an open rotor should be employed in order to make the aircraft's direct operating cost robust to uncertain fuel and carbon (CO2) prices in the Year 2030, taking the aircraft pro- ductivity, the passenger value of time, and the modal shift into account. To answer this question, an optimization loop was set up in MATLAB consisting of nine modules covering gas turbine and airframe design and performance, ight and aircraft eet sim- ulation, operating cost, and optimization. If the passenger value of time is included, the most robust aircraft design is powered by geared turbofan engines and cruises at Mach 0.80. If the value of time is ignored, however, then a turboprop aircraft ying at Mach 0.70 is the optimum solution. This demonstrates that the most fuel-ecient option, the open rotor, is not automatically the most cost-ecient solution because of the relatively high engine and airframe costs. 1 Research Engineer, Computational Engineering and Design 2 Professor of Aerospace Design, Computational Engineering and Design, AIAA member 3 Associate Professor in Aircraft Engineering, Computational Engineering and Design, AIAA member 1 I. Introduction A. Background IT takes around 5 years to develop a gas turbine engine, which then usually remains in pro- duction for more than two decades [1, 2]. -
Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
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. -
A Clean Slate Airbus Pivots to Hydrogen For
November 2020 HOW NOT TO DEVELOP DEVELOP TO NOT HOW FIGHTERYOUR OWN SPACE THREATS SPACE AIR GETSCARGO LIFT A A CLEAN SLATE AIRBUS HYDROGEN TO PIVOTS FOR ZERO-CARBON ‘MOONSHOT’ www.aerosociety.com AEROSPACE November 2020 Volume 47 Number 11 Royal Aeronautical Society 11–15 & 19–21 JANUARY 2021 | ONLINE REIMAGINED The 2021 AIAA SciTech Forum, the world’s largest event for aerospace research and development, will be a comprehensive virtual experience spread over eight days. More than 2,500 papers will be presented across 50 technical areas including fluid dynamics; applied aerodynamics; guidance, navigation, and control; and structural dynamics. The high-level sessions will explore how the diversification of teams, industry sectors, technologies, design cycles, and perspectives can all be leveraged toward innovation. Hear from high-profile industry leaders including: Eileen Drake, CEO, Aerojet Rocketdyne Richard French, Director, Business Development and Strategy, Space Systems, Rocket Lab Jaiwon Shin, Executive Vice President, Urban Air Mobility Division, Hyundai Steven Walker, Vice President and CTO, Lockheed Martin Corporation Join fellow innovators in a shared mission of collaboration and discovery. SPONSORS: As of October 2020 REGISTER NOW aiaa.org/2021SciTech SciTech_Nov_AEROSPACE PRESS.indd 1 16/10/2020 14:03 Volume 47 Number 11 November 2020 EDITORIAL Contents Drone wars are here Regulars 4 Radome 12 Transmission What happens when ‘precision effects’ from the air are available to everyone? The latest aviation and Your letters, emails, tweets aeronautical intelligence, and social media feedback. Nagorno-Karabakh is now the latest conflict where a new way of remote analysis and comment. war is evolving with cheap persistent UAVs, micro-munitions and loitering 58 The Last Word anti-radar drones, striking tanks, vehicles, artillery pieces and even SAM 11 Pushing the Envelope Keith Hayward considers sites with lethal precision. -
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. -
Signature Redacted Department of Civil and Envirnmental Engineering, MIT Sloan School of Management May 11,2018
Next Generation Commercial Aircraft Engine Maintenance, Repair, and Overhaul Capacity Planning and Gap Analysis by Amanda J. Knight B. S. Mechanical Engineering, The University of Texas at Austin, 2006 M.S. Aerospace Engineering, The University of Southern California, 2011 Submitted to the MIT Sloan School of Management and the Department of Civil and Environmental Engineering in Partial Fulfillment of the Requirements for the Degrees of Master of Business Administration and Master of Science in Civil and Environmental Engineering In conjunction with the Leaders for Global Operations Program at the Massachusetts Institute of Technology June 2018 2018 Amanda J. Knight. All rights reserved. The author hereby grants MIT permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part in any medium now known or hereafter created. Signature of Author: Signature redacted Department of Civil and Envirnmental Engineering, MIT Sloan School of Management May 11,2018 Certified by: Signature redacted __ DI Roy Welsch, Thesis Supervisor Professor of Statistics and Engineering Systems Certified by: Signature redacted Dr. Daniel Wh The i Supervisor Senior Research ScientisU/Eyneritust Lecturer, IVVT Leaders for obal Operations Certified by: _____Signature redacted _ _ _ _ _ _ Dr. David Simchi-Levi, Thesis Supervisor Prof"or,9 C ppdEnvironmental Engineering Accepted by: Signature redacted____ Jesse H. Kroll Profesor of Civil and Environmental Engineering Chair, Graduate Program Committee Accepted by: Signature redacted MHro MASSACHUSETTS INSTITUTE ' M PM ManuraHerson OF TECHNOLOGY co Director, MBA Program, MIT Sloan School of Management JUN 0 7 2018 LIBRARIES This page has been intentionally left blank Page | 2 Next Generation Commercial Aircraft Engine Maintenance, Repair, and Overhaul Capacity Planning and Gap Analysis by Amanda J. -
A Fond Farewell to Ve Fantastic Eets
NEWS RELEASE A fond farewell to ve fantastic eets 4/30/2020 Last month, American Airlines announced plans to accelerate the retirement of some older, less fuel-ecient aircraft from its eet sooner than originally planned. As ying schedules and aircraft needs are ne-tuned during this period of record low demand, American will take the unique step of retiring a total of ve aircraft types. American has ocially retired the Embraer E190 and Boeing 767 eets, which were originally scheduled to retire by the end of 2020. The airline has also accelerated the retirement of its Boeing 757s and Airbus A330-300s. Additionally, American is retiring 19 Bombardier CRJ200 aircraft operated by PSA Airlines. These changes remove operating complexity and will bring forward cost savings and eciencies associated with operating fewer aircraft types. It will also help American focus on ying more advanced aircraft as we continue receiving new deliveries of the Airbus A321neo and the Boeing 737 MAX and 787 family. American’s narrowbody eet also becomes more simplied with just two cockpit types – the Airbus A320 and the Boeing 737 families. This benets American’s operational performance through training eciency and streamlined maintenance. American continues to evaluate its schedule and remains committed to caring for customers on life’s journey. These changes will help American continue to provide a reliable travel experience around the world, even during these uncertain times. Here’s a snapshot of the aircraft exiting American’s eet: Airbus A330-300 — Blue Sky News/Pittsburgh International AirportAirbus A330-300 1 Joined the US Airways eet in 2000 prior to joining American’s eet in 2013. -
SP's Aviation June 2011
SP’s AN SP GUIDE PUBLICATION ED BUYER ONLY) ED BUYER AS -B A NDI I News Flies. We Gather Intelligence. Every Month. From India. 75.00 ( ` Aviationwww.spsaviation.net JUNE • 2011 ENGINE POWERPAGE 18 Regional Aviation FBO Services in India Interview with CAS No Slowdown in Indo-US Relationship LENG/2008/24199 Interview: Pratt & Whitney EBACE 2011 RNI NUMBER: DELENG/2008/24199 DE Show Report Our jets aren’t built tO airline standards. FOr which Our custOmers thank us daily. some manufacturers tout the merits of building business jets to airline standards. we build to an even higher standard: our own. consider the citation mustang. its airframe service life is rated at 37,500 cycles, exceeding that of competing airframes built to “airline standards.” in fact, it’s equivalent to 140 years of typical use. excessive? no. just one of the many ways we go beyond what’s required to do what’s expected of the world’s leading maker of business aircraft. CALL US TODAY. DEMO A CITATION MUSTANG TOMORROW. 000-800-100-3829 | WWW.AvIATOR.CESSNA.COM The Citation MUSTANG Cessna102804 Mustang Airline SP Av.indd 1 12/22/10 12:57 PM BAILEY LAUERMAN Cessna Cessna102804 Mustang Airline SP Av Cessna102804 Pub: SP’s Aviation Color: 4-color Size: Trim 210mm x 267mm, Bleed 277mm x 220mm SP’s AN SP GUIDE PUBLICATION TABLE of CONTENTS News Flies. We Gather Intelligence. Every Month. From India. AviationIssue 6 • 2011 Dassault Rafale along with EurofighterT yphoon were found 25 Indo-US Relationship compliant with the IAF requirements of a medium multi-role No Slowdown -
Optimisation of Flight Movements in Europe
Faculty of Economics and Business Administration Optimisation of Flight Movements in Europe Alexander Nollau Friedrich Thießen Chemnitz Economic Papers, No. 029, January 2019 Chemnitz University of Technology Faculty of Economics and Business Administration Thüringer Weg 7 09107 Chemnitz, Germany Phone +49 (0)371 531 26000 Fax +49 (0371) 531 26019 https://www.tu-chemnitz.de/wirtschaft/index.php.en [email protected] Professur für Finanzwirtschaft und Bankbetriebslehre Fakultät für Wirtschaftswissenschaften Optimisation of Flight Movements in Europe Possibilities for reducing the number of flight movements in Europe, taking the quality of the connections into account Alexander Nollau, Friedrich Thießen Aviation Working Group TU Chemnitz Prof. Dr. Friedrich Thießen [email protected] Tel. 0371-531-34174 January 2019 Optimisation of Flight Movements in Europe Possibilities for reducing the number of flight movements in Europe, taking the quality of the connections into account 1 Abstract Many current problems in air traffic are related to the number of aircraft movements. Overcrowding in the airspace, difficult coordination at airports, high emissions of noise and pollutants as well as complexity of airlines are side effects of too many aircraft movements. This study examines the extent to which the number of flight movements in Europe can be reduced without change in transport performance. For this purpose, the number of flight movement for a European network of the 140 most frequently flown serviced routes will be optimised. The reference date is November 17th, 2017. It shows that with the same passenger transport performance, the number of flight movements can be re- duced to 1/3 of the current level (from 2.040 flights per day to 738 flights per day). -
It's No American Dream: Pratt & Whitney GTF Engine Now a Reality
A D D E N D U M It’s No American Dream: Pratt & Whitney GTF Engine Now a Reality... and chosen in Time's November issue one of "The 50 Best Inventions of the Year" In the August try-tasked capabilities. 2008 issue of Gear For those who can’t Technology, we ran recall how the GTF a story (“Gearbox works, here’s a piece Speed Reducer Helps lifted from the 2008 Fan Technology for Gear Technology arti- ‘Greener” Jet Fuel cle explaining—with Efficiency’) on the help from Robert Saia, then ongoing, extreme- Pratt & Whitney vice ly challenging and pro- president, next-gener- tracted development ation products—what of Pratt & Whitney’s makes it leading edge: geared turbofan (GTF) (What’s unique) jet engine. If success- is the addition of a ful, the engine would reduction gear box— provide a 20 percent or transmission sys- reduction in carbon tem—comprised of a emissions and fuel star gear system with burn and up to 50 per- five stationary gears. cent in general noise As Saia explains, the reduction. The targeted The long-awaited Pratt & Whitney GTF (PurePower PW1000G) jet gear box decouples the market and application engine is now a reality, with customer orders now in production (cour- fan from the turbine so for the engine was the tesy Pratt & Whitney). that each component narrow-body commer- can turn at its optimum cial airline industry—until now a dormant market for P&W— speed while also allowing for a lighter, more efficient turbine to which had long demanded a total plane package that would turn at a higher speed in driving a much larger, slower-turning achieve reduced maintenance, lower emissions, better fuel burn, fan.