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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 -
MTU-Museum Triebwerksgeschichte – Gestern, Heute Und Morgen MTU Museum 07 2009 01.Qxd 27.08.2009 13:47 Uhr Seite 4
MTU_Museum_07_2009_01.qxd 27.08.2009 13:47 Uhr Seite 3 MTU-Museum Triebwerksgeschichte – gestern, heute und morgen MTU_Museum_07_2009_01.qxd 27.08.2009 13:47 Uhr Seite 4 Inhaltsverzeichnis Vorwort 3 Unternehmen mit Tradition und Zukunft 4 Bewegte Geschichte 5 GP7000 – Antrieb für den Mega-Airbus 8 PW6000 – Antrieb des kleinen Airbus A318 8 EJ200 – Schub für den Eurofighter 9 PW4000 – Triebwerk der Boeing B777-200 10 MTR390 – Triebwerk des Tigers 10 V2500 – Antrieb für den Airbus A320 11 PW500 – Antrieb für Geschäftsreiseflugzeuge 12 RR250-C20 – Antrieb für Hubschrauber 12 RB199 – Antrieb des Tornado 13 CF6 – Power für Großraumflugzeuge 14 Lycoming GO-480-B1A6 – Lizenzfertigung bei BMW 15 MTU7042 – Erprobung einer LKW-Gasturbine 15 T64-MTU-7 – Lizenzbau in Deutschland 16 RB145R – Antrieb des VJ101C 16 RB193-12 – Antrieb für Senkrechtstarter 17 RB153 – Antrieb des VJ101E 17 J79 – Triebwerk des Starfighters 18 Tyne – Antrieb der Transall 19 BMW 6022 – Antrieb für den Bo105 19 DB 720 – Daimler-Nachkriegsära beginnt 20 BMW 801 – erster deutscher Doppelsternmotor 20 BMW 114 – Diesel-Flugmotor 21 BMW 003E – Schub für den Volksjäger 22 Riedel-Anlasser – Starter für Strahltriebwerke 23 BRAMO 323 R-1 „Fafnir“ – erfolgreichster BRAMO-Flugmotor 23 Daimler-Benz DB 605 – der „kleine“ Mercedes-Benz-Flugmotor 24 BMW 132 – Nachfolger des Hornet-Motors 25 Sh14A – erfolgreichster Siemens-Flugmotor 26 BMW VI – Erfolgsmotor der 1920er-Jahre 26 Daimler-Benz F4A – Vorläufer der DB 600-Familie 27 Daimler D IIIa – Ära der Kolbenflugmotoren beginnt 27 Exponate 28 Chirurg der Motoren 31 2 MTU_Museum_07_2009_01.qxd 27.08.2009 13:47 Uhr Seite 5 Vorwort Die Museumswelt wird nicht nur von großen Ausstellungen und Kunstgalerien jeder Couleur geprägt, sondern auch von technischen Samm- lungen, wie etwa dem Deutschen Museum in München. -
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. -
Lifetime Excellence Lifetime Excellence | 3 Power for the World
MTU Aero Engines AG The full range of engine expertise Firmly established worldwide balanced portfolio, the company is represented in all thrust and power categories for commercial engines. Highpres MTU Aero Engines is Germany’s leading engine manufacturer sure compressors, lowpressure turbines and turbine center and a firmly established player in the international aviation frames “made by MTU” rank among the best in their class. industry. The company designs, develops, manufactures, markets and supports commercial and military propulsion In commercial engine maintenance, MTU Maintenance systems for aircraft and helicopters, and stationary gas tur sets global standards with its comprehensive services and bines, and offers full system capability in engine construction. innovative repair techniques. MTU Power offers compelling intelligent maintenance solutions for industrial gas turbines. MTU is the industrial lead company for almost all engines operated by the German Armed Forces and plays a key role High power density in major European military engine programs. MTU offers solutions for the entire engine lifecycle—from development to production to maintenance. With its well 2 | Lifetime Excellence Lifetime Excellence | 3 Power for the world MTU Maintenance Lease Services SMBC Aero Engine Lease MTU Maintenance Hannover MTU Maintenance Berlin-Brandenburg MTU Maintenance Canada Pratt & Whitney Canada Customer Service Centre Europe MTU Aero Engines North America EME Aero MTU Aero Engines Polska MTU Aero Engines, Headquarters MTU Maintenance Dallas For MTU Aero Engines, Aerospace Embedded Solutions customer proximity is key. Ceramic Coating Center This is delivered by around MTU Maintenance Zhuhai 10,000 employees from over 60 nations at 15 locations worldwide. Through its sub- sidiaries and joint ventures, Major locations and participations MTU is present in all key IGT Service Centers regions and markets. -
NPA 2018-13 Table of Contents
European Aviation Safety Agency Notice of Proposed Amendment 2018-13 Appendix I to AMC to Annex III (Part-66) Aircraft type ratings for Part-66 aircraft maintenance licences RMT.0541 (66.024) EXECUTIVE SUMMARY This Notice of Proposed Amendment (NPA) addresses a regulatory coordination issue related to aircraft type ratings. According to the AMC to Annex III (Part-66), type ratings should be endorsed on an aircraft maintenance licence (AML) in accordance with Appendix I to AMC to Part-66 ‘List of type ratings’. An NPA is issued regularly to amend this list, after assessing feedback received from the industry, and to add new aircraft types or to remove aircraft types whose type certificate (TC) has been revoked or surrendered. This NPA adds also the tables of the new Group as a consequence of the introduction of the ‘L’ licence subcategories by Commission Regulation (EU) 2018/1142. The main objective is to ensure a common standard throughout the Member States. Action area: Regular updates/review of rules Affected rules: AMC/GM to Annex III (Part-66) to Commission Regulation (EU) No 1321/2014 Affected stakeholders: Maintenance certifying staff; maintenance training organisations; maintenance organisations; competent authorities Driver: Efficiency/proportionality Rulemaking group: No Impact assessment: None Rulemaking Procedure: Standard 12.5.2009 5.12.2018 2019/Q2 TE.RPRO.00034-008 © European Aviation Safety Agency. All rights reserved. ISO 9001 certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA intranet/internet. Page 1 of 186 An agency of the European Union European Aviation Safety Agency NPA 2018-13 Table of contents Table of contents 1. -
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. -
MTU Annual Report 2006
Ready for the Future Annual Report 2006 Selected Consolidated Financial Information and Key Figures 2006 2005*) Key income statement figures in € million Revenues 2,416.2 2,182.7 Research and development expenses 64.5 45.7 Earnings before interest and tax (EBIT) 183.8 131.2 Earnings before interest, tax, depreciation and amortization (EBITDA) 335.6 295.3 Earnings before tax (EBT) 150.5 58.6 Income taxes 61. 4 25.8 Net profit 89.1 32.8 Key income statement figures in € million (adjusted) Earnings before interest, tax, depreciation and amortization (EBITDA) 318.2 238.7 Earnings before tax (EBT) 204.4 89.1 Net profit 121.8 53.1 Key balance sheet figures in € million Equity 562.3 528.0 Total assets 3,112.2 2,850.7 Fixed assets 1,739.5 1,795.4 Non-current financial liabilities (excluding deferred tax liabilities) 1,184.9 1,048.7 Number of employees at year end By market segment Commercial and Military Engine Business 4,740 4,805 Commercial Maintenance Business 2,337 2,125 7,077 6,930 Key figures in % Gross margin 14.6 13.2 EBITDA-margin 13.9 13.5 EBIT-margin 7. 6 6.0 Post-tax return on sales 3.7 1.5 Return on equity 16.3 8.8 Equity ratio 18.1 18.5 Cash flow in € million Cash flow from operating activites 209.8 291.7 Cash flow from investing activities -94.1 -83.9 Free cash flow 115.7 207.8 Share values Basic (undiluted) earnings per share in € 1.64 0.60 Basic (undiluted) earnings per share in € (adjusted) 2.25 0.97 Diluted earnings per share in € 1.64 0.60 Free cash flow per share in € 2.13 3.78 Equity per share in € 10.37 9.60 *) MTU Maintenance Zhuhai Co. -
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 .................................... -
Aip Supplement 012/2019 United Kingdom
AIP SUPPLEMENT 012/2019 UNITED KINGDOM Date Of Publication 14 Mar 2019 UK Aeronautical Information Services Notes NATS Swanwick (a) All times are UTC. Room 3115 (b) References are to the UK AIP. Sopwith Way (c) Information, where applicable, Southampton SO31 7AY [email protected] should also be used to amend http://www.ais.org.uk appropriate charts. 07469-441832 (Content - DfT/Aviation Policy Division) 0191-203 2329 (Distribution - Communisis UK) LONDON HEATHROW, LONDON GATWICK AND LONDON STANSTED AIRPORTS NOISE RESTRICTIONS NOTICE 2019 (Published on behalf of the Department for Transport) Whereas: a) By virtue of the Civil Aviation (Designation of Aerodromes) Order 1981(a) Heathrow Airport - London, Gatwick Airport - London and Stansted Airport - London (‘the London Airports’) are designated aerodromes for the purposes of Section 78 of the Civil Aviation Act 1982 (‘the Act’)(b); b) Pursuant to the powers set out in section 78 of the Act, the Secretary of State considers it appropriate, for the purpose of avoiding, limiting or mitigating the effect of noise and vibration connected with the taking-off or landing of aircraft at the London Airports, to prohibit aircraft of specified descriptions from taking off or landing and to limit the number of occasions on which other aircraft may take off or land at those aerodromes during periods specified in this Notice throughout the period specified as the summer season 2019 in this Notice; c) For the purposes of Section 78(4)(a) of the Act, the circumstances under which a particular occasion or series of occasions on which aircraft take off or land at the London Airports will be disregarded for the purposes of this Notice are specified in paragraph 11 of this Notice. -
The Market for Aviation Turbofan Engines
The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7