Propulsione Aeronautica 2020/2021 Francesco Barato
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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 -
A Study of Technology Used and Comparison Between Traditional and Hf120 (Advanced Aero Engine)
International Journal of Recent Technology and Engineering (IJRTE) ISSN: 2277-3878, Volume-4 Issue-4, September 2015 A Study of Technology Used and Comparison Between Traditional and Hf120 (Advanced Aero Engine) Vivek Kumar, Rajeshwar Prasad Singh, Vikash Kumar Abstract- Paper includes detailed study of the HF120 turbofan The two companies began talks in 2003 with the goal of engine, which is the first product from GE Honda Aero providing durable and economical engines for business Engines. This paper is to showcase state of art technology aviation. The idea was to combine the strengths of each involved in gas turbine engines and to bring out various aspects and future trends in field of propulsion technology. parent company in technology leadership, manufacturing Paper also includes development in gas turbine engine that have expertise, and performance engine tradition to provide helped to achieve great fuel efficiency and less noise, increased modern business aviation engines with the performance power, thrust and also advancements made in the field of and availability of large commercial engines. A strategic materials have contributed in a major way in gas turbine in alliance between the two companies lead to planning of accordance to the future trends that have come up in recent 50/50 project intended to develop, certify and market the years. The paper reviews the evolutionary process that has taken place over the years with reference to the different design Honda engine. The HF120, product from GE Honda Aero concepts used for aero engines. At General Electric, the official Engines, utilizes Honda's world-renowned expertise in corporate slogan is “Imagination at work.” At Honda, it’s “The manufacturing, research and development and GE's power of dreams.” Two of the world's most respected names in experience in aerospace technology, durability, and propulsion have come together to design and manufacture certification. -
6. Chemical-Nuclear Propulsion MAE 342 2016
2/12/20 Chemical/Nuclear Propulsion Space System Design, MAE 342, Princeton University Robert Stengel • Thermal rockets • Performance parameters • Propellants and propellant storage Copyright 2016 by Robert Stengel. All rights reserved. For educational use only. http://www.princeton.edu/~stengel/MAE342.html 1 1 Chemical (Thermal) Rockets • Liquid/Gas Propellant –Monopropellant • Cold gas • Catalytic decomposition –Bipropellant • Separate oxidizer and fuel • Hypergolic (spontaneous) • Solid Propellant ignition –Mixed oxidizer and fuel • External ignition –External ignition • Storage –Burn to completion – Ambient temperature and pressure • Hybrid Propellant – Cryogenic –Liquid oxidizer, solid fuel – Pressurized tank –Throttlable –Throttlable –Start/stop cycling –Start/stop cycling 2 2 1 2/12/20 Cold Gas Thruster (used with inert gas) Moog Divert/Attitude Thruster and Valve 3 3 Monopropellant Hydrazine Thruster Aerojet Rocketdyne • Catalytic decomposition produces thrust • Reliable • Low performance • Toxic 4 4 2 2/12/20 Bi-Propellant Rocket Motor Thrust / Motor Weight ~ 70:1 5 5 Hypergolic, Storable Liquid- Propellant Thruster Titan 2 • Spontaneous combustion • Reliable • Corrosive, toxic 6 6 3 2/12/20 Pressure-Fed and Turbopump Engine Cycles Pressure-Fed Gas-Generator Rocket Rocket Cycle Cycle, with Nozzle Cooling 7 7 Staged Combustion Engine Cycles Staged Combustion Full-Flow Staged Rocket Cycle Combustion Rocket Cycle 8 8 4 2/12/20 German V-2 Rocket Motor, Fuel Injectors, and Turbopump 9 9 Combustion Chamber Injectors 10 10 5 2/12/20 -
Enhancement of Volumetric Specific Impulse in HTPB/Ammonium Nitrate Mixed
Utah State University DigitalCommons@USU All Graduate Plan B and other Reports Graduate Studies 12-2016 Enhancement of Volumetric Specific Impulse in TPB/H Ammonium Nitrate Mixed Hybrid Rocket Systems Jacob Ward Forsyth Utah State University Follow this and additional works at: https://digitalcommons.usu.edu/gradreports Part of the Propulsion and Power Commons Recommended Citation Forsyth, Jacob Ward, "Enhancement of Volumetric Specific Impulse in TPB/AmmoniumH Nitrate Mixed Hybrid Rocket Systems" (2016). All Graduate Plan B and other Reports. 876. https://digitalcommons.usu.edu/gradreports/876 This Report is brought to you for free and open access by the Graduate Studies at DigitalCommons@USU. It has been accepted for inclusion in All Graduate Plan B and other Reports by an authorized administrator of DigitalCommons@USU. For more information, please contact [email protected]. ENHANCEMENT OF VOLUMETRIC SPECIFIC IMPULSE IN HTPB/AMMONIUM NITRATE MIXED HYBRID ROCKET SYSTEMS by Jacob W. Forsyth A report submitted in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE in Aerospace Engineering Approved: ______________________ ____________________ Stephen A. Whitmore Ph.D. David Geller Ph.D. Major Professor Committee Member ______________________ Rees Fullmer Ph.D. Committee Member UTAH STATE UNIVERSITY Logan, Utah 2016 ii Copyright © Jacob W. Forsyth 2016 All Rights Reserved iii ABSTRACT Enhancement of Volumetric Specific Impulse in HTPB/Ammonium Nitrate Mixed Hybrid Rocket Systems by Jacob W. Forsyth, Master of Science Utah State University, 2016 Major Professor: Dr. Stephen A. Whitmore Department: Mechanical and Aerospace Engineering Hybrid rocket systems are safer and have higher specific impulse than solid rockets. However, due to large oxidizer tanks and low regression rates, hybrid rockets have low volumetric efficiency and very long longitudinal profiles, which limit many of the applications for which hybrids can be used. -
Records Fall at Farnborough As Sales Pass $135 Billion
ISSN 1718-7966 JULY 21, 2014 / VOL. 448 WEEKLY AVIATION HEADLINES Read by thousands of aviation professionals and technical decision-makers every week www.avitrader.com WORLD NEWS More Malaysia Airlines grief The Airbus A350 XWB The US stock market fell sharply was a guest on fears of renewed hostilities of honour at after the news that a Malaysian Farnborough Airlines flight was allegedly shot (left) last week down over eastern Ukraine, with as it nears its service all 298 people on board reported entry date dead. US vice president Joe Biden with Qatar said the plane was “blown out of Airways later the sky”, apparently by a surface- this year. to-air missile as the Boeing 777 Airbus jet cruised at 33,000 feet, some 1,000 feet above a closed section of airspace. Ukraine has accused Records fall at Farnborough as sales pass $135 billion pro-Russian “terrorists” of shoot- Airbus, CFM International beat forecasts with new highs at UK show ing the plane down with a Soviet- era SA-11 missile as it flew from The 2014 Farnborough Interna- Farnborough International Airshow: Major orders* tional Airshow closed its doors Amsterdam to Kuala Lumpur. Airframer Customer Order Value¹ last week safe in the knowledge Boeing 777 Qatar Airways 50 777-9X $19bn Record show for CFM Int’l that it had broken records on many fronts - not least on total Boeing 777, 737 Air Lease 6 777-300ER, 20 737 MAX $3.9bn CFM International, the 50/50 orders and commitments for Air- Airbus A320 family SMBC 110 A320neo, 5 A320 ceo $11.8bn joint company between Snec- bus and Boeing aircraft, which ma (Safran) and GE, celebrated Airbus A320 family Air Lease 60 A321neo $7.23bn hit a combined $115.5bn at list record sales worth some $21.4bn Embraer E-Jet Trans States 50 E175 E2 $2.4bn prices for 697 aircraft - over 60% at Farnborough. -
ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics
National Research University Higher School of Economics Institute for Statistical Studies and Economics of Knowledge Big Data Augmented Horizon Scanning: Combination of Quantitative and Qualitative Methods for Strategic and Marketing Analytics [email protected] [email protected] XIX April International Academic Conference on Economic and Social Development Moscow, 11 April 2018 Outline - Role of artificial intelligence and big data in modern analytics - System of Intelligent Foresight Analytics iFORA - Combined quantitative and qualitative analysis methodology and software solutions - Use cases - Conclusion and discussion 2 Growing interest in Artificial Intelligence, Big Data and Machine Learning International analytical reports & news feed 12000 10000 8000 Artificial Intelligence 6000 Big Data Machine Learning 4000 2000 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 Russian analytical reports & news feed 800 700 600 500 Artificial Intelligence 400 Big Data 300 Machine Learning 200 100 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 3 Source: System of Intelligent Foresight Analytics iFORA™ (ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics AI-related tasks Tracking latest and challenges trends, technologies, drivers, barriers Market forecasting Trend analysis Understanding S&T modern skills and Instruments for Customers Market Intelligence competences analysis feedback knowledge discovery HR policy Vacancy Feedback mining -
An Investigation of the Performance Potential of A
AN INVESTIGATION OF THE PERFORMANCE POTENTIAL OF A LIQUID OXYGEN EXPANDER CYCLE ROCKET ENGINE by DYLAN THOMAS STAPP RICHARD D. BRANAM, COMMITTEE CHAIR SEMIH M. OLCMEN AJAY K. AGRAWAL A THESIS Submitted in partial fulfillment of the requirements for the degree of Master of Science in the Department of Aerospace Engineering and Mechanics in the Graduate School of The University of Alabama TUSCALOOSA, ALABAMA 2016 Copyright Dylan Thomas Stapp 2016 ALL RIGHTS RESERVED ABSTRACT This research effort sought to examine the performance potential of a dual-expander cycle liquid oxygen-hydrogen engine with a conventional bell nozzle geometry. The analysis was performed using the NASA Numerical Propulsion System Simulation (NPSS) software to develop a full steady-state model of the engine concept. Validation for the theoretical engine model was completed using the same methodology to build a steady-state model of an RL10A-3- 3A single expander cycle rocket engine with corroborating data from a similar modeling project performed at the NASA Glenn Research Center. Previous research performed at NASA and the Air Force Institute of Technology (AFIT) has identified the potential of dual-expander cycle technology to specifically improve the efficiency and capability of upper-stage liquid rocket engines. Dual-expander cycles also eliminate critical failure modes and design limitations present for single-expander cycle engines. This research seeks to identify potential LOX Expander Cycle (LEC) engine designs that exceed the performance of the current state of the art RL10B-2 engine flown on Centaur upper-stages. Results of this research found that the LEC engine concept achieved a 21.2% increase in engine thrust with a decrease in engine length and diameter of 52.0% and 15.8% respectively compared to the RL10B-2 engine. -
Vysoké Učení Technické V Brně
VYSOKÉ UČENÍ TECHNICKÉ V BRNĚ BRNO UNIVERSITY OF TECHNOLOGY FAKULTA STROJNÍHO INŽENÝRSTVÍ ÚSTAV AUTOMOBILNÍHO A DOPRAVNÍHO INZENYRSTVÍ FACULTY OF MECHANICAL ENGINEERING INSTITUTE OF AUTOMOTIVE ENGINEERING ZLEPSOVANI BRAYTONOVA OBEHU LETECKYCH PLYNOVYCH TURBIN Improving of Brayton Cycle For Aero Gas Engine BAKALÁŘSKÁ PRÁCE BACHELOR´S THESIS AUTOR PRÁCE RODRIGO ACEVEDO AUTHOR VEDOUCÍ PRÁCE ING. MIROSLAV ŠPLÍCHAL SUPERVISOR BRNO 2012 1 Vysoké učení technické v Brně, Fakulta strojního inženýrství Ústav automobilního a dopravního inženýrství Akademický rok: 2011/2012 ZADÁNÍ BAKALÁŘSKÉ PRÁCE student(ka): Rodrigo Acevedo který/která studuje v bakalářském studijním programu obor: Stavba strojů a zařízení (2302R016) Ředitel ústavu Vám v souladu se zákonem č.111/1998 o vysokých školách a se Studijním a zkušebním řádem VUT v Brně určuje následující téma bakalářské práce: Zlepšování Braytonova oběhu leteckých plynových turbín v anglickém jazyce: Improving of Brayton cycle for aero gas turbine Stručná charakteristika problematiky úkolu: Popsat ideální a skutečný oběh leteckých plynových turbín. Rozbor vlivu zařazení mezistupňového chlazení a regenerace. Popis realizace zlepšení parametrů oběhu u leteckých turbín. Cíle bakalářské práce: Rešerše parametrů oběhu aktuálně používaných leteckých plynových turbín. Rozbor termické účinnosti oběhu leteckých plynových turbín a návrh možných zlepšení. 2 Seznam odborné literatury: OTT, Adolf. Pohon letadel. první. Brno : Nakladatelství Vysokého učení technického v Brně, 1993. 168 s. ISBN 80-214-0522-8. ADAMEC, Josef; KOCÁB, Jindřich. Letadlové motory. Vyd. 2. Praha : Corona, 2008. ISBN 978-808-6116-549 WARD, Thomas A.; Aerospace propulsion systems, Sinagaporse : John Wiley & Sons, 2010, ISBN 978-0-470-82497-9 Vedoucí bakalářské práce: Ing. Miroslav Šplíchal Termín odevzdání bakalářské práce je stanoven časovým plánem akademického roku 2011/2012. -
We Want to Continue Innovating, Finding Newer Ways to Delight Our Customers and Redefine Air Travel.” — LESLIE THNG, CHIEF EXECUTIVE OFFICER, VISTARA
FIRST BIOFUEL CIVIL AIRCRAFT SHOW POWERED FLIGHT MANUFACTURING REPORT: IN INDIA IN INDIA FIA 2018 P 11 P 16 P 22 AUGUST-SEPTEMBER 2018 `100.00 (INDIA-BASED BUYER ONLY) VOLUME 11 • ISSUE 4 WWW.SPSAIRBUZ.COM ANAIRBUZ EXCLUSIVE MAGAZINE ON CIVIL AVIATION FROM INDIA EXCLUSIVE PAGE 8 “we wANT TO CONTINUE INNOVATING, FINDING NEWER WAYS TO DELIGHT OUR CUSTOMERS AND REDEFINE AIR TRAvel.” — LESLIE THNG, CHIEF EXECUTIVE OFFICER, VISTARA AN SP GUIDE PUBLICATION RNI NUMBER: DELENG/2008/24198 TABLE OF CONTENTS EXCLUSIVE COVER STORY / INTERVIEW P8 “we’re not chasing the COMPETITION, BUT CREATING A Cover: FIRST BIOFUEL CIVIL AIRCRAFT SHOW “Vistara has naturally inherited POWERED FLIGHT MANUFACTURING REPORT: IN INDIA IN INDIA FIA 2018 UNIQUE SPACE FOR OURSELVES IN P 11 P 16 P 22 very strong values and stands the market” AUGUST-SEPTEMBER 2018 `100.00 (INDIA-BASED BUYER ONLY) VOLUME 11 • ISSUE 4 committed to delivering WWW.SPSAIRBUZ.COM ANAIRBUZ EXCLUSIVE MAGAZINE ON CIVIL AVIATION FROM INDIA EXCLUSIVE In an exclusive interview with Jayant customer-centricity at every PAGE 8 “WE WANT touchpoint,”says Leslie Thng, TO CONTINUE Baranwal, Editor-in-Chief of SP’s INNOVATING, FINDING CEO, Vistara, in an exclusive NEWER WAYS AirBuz, Leslie Thng, Chief Executive TO DELIGHT OUR CUSTOMERS with SP’s AirBuz. AND REDEFINE AIR TRAVEL.” Officer of Vistara shares his optimism — LESLIE THNG, CHIEF EXECUTIVE OFFICER, Cover Photograph: VISTARA AN SP GUIDE PUBLICATION and outlines his vision and plans for Vistara RNI NUMBER: DELENG/2008/24198 the future growth of the airlines. SP's AirBuz Cover 4-2018.indd 1 18/09/18 4:43 PM POLICY / AIR INDIA P14 AIR INDIA DISINVESTMENT Debate on Air India disinvestment though, has been on for over two decades and the failed attempt at disinvestment earlier this year, was an anticlimactic episode in the ongoing saga. -
SP's Aviation 03-09
SP’s AN SP GUIDE PUBLICATION News Flies. We Gather Intelligence. Every Month. From India. ISSUE 3 • 2009 WWW.SPSAVIATION.NET Aviation Lockheed Martin’s VP, Business Embraer’s VP, S&M José Development Orville Prins spells out Eduardo Costas elaborates on combat capabilities of the F-16IN strengths of Phenom 100 PAGE 4 PAGE 11 LightVERY JETS DELENG/2008/24199 RNI NUMBER: TRENDS PAGE 8 451964-2009 SP GUIDE PUBLICATIONS WIDENING NEW HORIZONS... • Indiaʼs Homeland Security IN THIS & Ministry EDITION of Home Affairs Elements • IDS Headquartersʼ role in Procurement Process elaborated Ministry of Home Affairs Elements • IDS Headquartersʼ role in Procurement Process elaborated • Eventsʼ Reference - Special Insert • Indiaʼs IN Homeland THIS EDITION Security & - • Eventsʼ Reference - Special Insert � ������������ � ������ � ����� 8 � ������� 200 � ����������� ������������������� 9 Get your copies ������������������� www.spsmilitaryyearbook.com 2009 200 2008 via - ��������������� 4/9/09 3:12:44 PM � ������ ��������������� [email protected] ������������������������������������������������������������������� ����������������������������������������� ������������������������ �� ������������������ ��������������������� ����������������������������� SP's MYB 0809 CVR01.indd 1 � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � � www.spguidepublications.com Table of Contents Regular Departments SP’s AN SP GUIDE PUBLICATION 8 2 A Word from Editor News Flies. We Gather Intelligence. Every Month. From India. AviationISSUE 3 • 2009 -
Development of a Forecast Model for Global Air Traffic Emissions
Forschungsbericht 2012-08 Development of a Forecast Model for Global Air Traffic Emissions Martin Schaefer Deutsches Zentrum für Luft- und Raumfahrt Institut für Antriebstechnik Köln 235 Seiten 137 Bilder 70 Tabellen 133 Literaturstellen Development of a Forecast Model for Global Air Traffic Emissions Dissertation zur Erlangung des Grades Doktor-Ingenieur der Fakultät für Maschinenbau der Ruhr-Universität Bochum von Martin Schaefer aus Nürnberg Bochum 2012 Dissertation eingereicht am: 07. März 2012 Tag der mündlichen Prüfung: 29. Juni 2012 Erster Referent: Prof. Dr.-Ing. Reinhard Mönig (Ruhr-Universität Bochum) Zweiter Referent: Prof. Dr. rer. nat. Johannes Reichmuth (RWTH Aachen) PAGE I CONTENTS LIST OF FIGURES............................................................................. V LIST OF TABLES ............................................................................. XI LIST OF ABBREVIATIONS...............................................................XIV PREFACE.....................................................................................XIX 1 EXECUTIVE SUMMARY ......................................................................1 1.1 Objectives of this Study ..............................................................................................1 1.2 Abstract of Methodology .............................................................................................1 1.3 Summary of Results ...................................................................................................4 1.3.1 Overview -
SP's Aviation August 2010
SP’s AN SP GUIDE PUBLICATION A-BASED BUYER ONLY) BUYER A-BASED I News Flies. We Gather Intelligence. Every Month. From India. RS. 75.00 (IND RS. Aviationwww.spsaviation.net AUGUST • 2010 IAF to get more AWACS Military Aero Engines Interviews with Lockheed Martin’s Ralph Heath & Boeing’s Chris Chadwick FARNBOROUGH AIRSHOW 2010 Iconic RNI NUMBER: DELENG/2008/24199 PAGE 24 SHOW Answering the call with confidence. It’s in our power.™ Pratt & Whitney builds and supports the most advanced military engines in the world, including the F117 engine for the C-17 Globemaster III airlifter. In fact, 27 armed services across the globe employ 11,000 of our engines to deliver when it really counts. Learn more at www.pw.utc.com. Military Engines SP’s AN SP GUIDE PUBLICATION TABLE of CONTENTS News Flies. We Gather Intelligence. Every Month. From India. AviationIssue 8 • 2010 CEOSPEAK 28 Ralph Heath ‘We are the only provider of the fifth generation aircraft to the world’ OEM 30 Interview ‘We focus on the market through the eyes of our customers’ INTERVIEW 32 OEM ‘Reliability and maintainability: A400M, manufactured by Airbus Military, during an impressive two outstanding benefits’ flying display at the Farnborough Airshow 2010. T he aircraft 24 was rechristened – Grizzly HALL OF famE 34 Lawrence Hargrave FIRST Lead Story REGULAR DEpaRTMENTS 8 Transformer 5 A Word from Editor ICONIC SHOW TECH WATCH Farnborough, the biggest air 6 NewsWithViews show of the year, witnessed 9 – Phantom Eye several new aircraft, new - Laser System to track – At an Advantage players and new orders.