Identifying CO2 Reducing Aircraft Technologies and Estimating Their Impact on Global Emissions
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Approaches to Representing Aircraft Fuel Efficiency Performance for the Purpose of a Commercial Aircraft Certification Standard
APPROACHES TO REPRESENTING AIRCRAFT FUEL EFFICIENCY PERFORMANCE FOR THE PURPOSE OF A COMMERCIAL AIRCRAFT CERTIFICATION STANDARD Brian M. Yutko and R. John Hansman This report is based on the Masters Thesis of Brian M. Yutko submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science at the Massachusetts Institute of Technology. Report No. ICAT-2011-05 May 2011 MIT International Center for Air Transportation (ICAT) Department of Aeronautics & Astronautics Massachusetts Institute of Technology Cambridge, MA 02139 USA [Page Intentionally Left Blank] -2- Approaches to Representing Aircraft Fuel Efficiency Performance for the Purpose of a Commercial Aircraft Certification Standard by Brian M. Yutko Submitted to the Department of Aeronautics and Astronautics on May 19, 2011 in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aeronautics and Astronautics Abstract Increasing concern over the potential harmful effects of green house gas emissions from various sources has motivated the consideration of an aircraft certification standard as one way to reduce aircraft CO2 emissions and mitigate aviation impacts on the climate. In order to develop a commercial aircraft certification standard, a fuel efficiency performance metric and the condition at which it is evaluated must be determined. The fuel efficiency metric form of interest to this research is fuel/range, where fuel and range can either be evaluated over the course of a reference mission or at a single, instantaneous point. A mission-based metric encompasses all phases of flight and is robust to changes in technology; however, definition of the reference mission requires many assumptions and is cumbersome for both manufacturers and regulators. -
Propulsione Aeronautica 2020/2021 Francesco Barato
PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO MATERIALE DI SUPPORTO FONDAMENTI DI PROPULSIONE AERONAUTICA Thrust 푇 = (푚̇ 푎 + 푚̇ 푓)푉푒 − 푚̇ 푎푉0 + (푝푒 − 푝푎)퐴푒 푇 ≈ 푚̇ 푎(푉푒 − 푉0) + (푝푒 − 푝푎)퐴푒 1 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Ramjet P-270 Moskit (left), BrahMos (right) Turboramjet Pratt & Whitney J-58 turbo(ram)jet 2 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Scramjet 3 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Specific impulse 푇 푉푒 푇 푚̇ 푝 푉푒 − 푉0 퐼푠푝 = = [푠] 푟표푐푘푒푡푠 퐼푠푝 = = [푠] 푎푟 푏푟푒푎푡ℎ푛푔 푚̇ 푝푔0 푔0 푚̇ 푓푔0 푚̇ 푓 푔0 4 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Propulsive efficiency Overall efficiency Overall efficiency with Mach number 5 PROPULSIONE AERONAUTICA 2020/2021 FRANCESCO BARATO Engine bypass ratios Bypass Engine Name Major applications ratio turbojet early jet aircraft, Concorde 0.0 SNECMA M88 Rafale 0.30 GE F404 F/A-18, T-50, F-117 0.34 PW F100 F-16, F-15 0.36 Eurojet EJ200 Typhoon 0.4 Klimov RD-33 MiG-29, Il-102 0.49 Saturn AL-31 Su-27, Su-30, J-10 0.59 Kuznetsov NK-144A Tu-144 0.6 PW JT8D DC-9, MD-80, 727, 737 Original 0.96 Soloviev D-20P Tu-124 1.0 Kuznetsov NK-321 Tu-160 1.4 GE Honda HF120 HondaJet 2.9 RR Tay Gulfstream IV, F70, F100 3.1 GE CF6-50 A300, DC-10-30,Lockheed C-5M Super Galaxy 4.26 PowerJet SaM146 SSJ 100 4.43 RR RB211-22B TriStar 4.8 PW PW4000-94 A300, A310, Boeing 767, Boeing 747-400 4.85 Progress D-436 Yak-42, Be-200, An-148 4.91 GE CF6-80C2 A300-600, Boeing 747-400, MD-11, A310 4.97-5.31 RR Trent 700 A330 5.0 PW JT9D Boeing 747, Boeing 767, A310, DC-10 5.0 6 PROPULSIONE -
System Requirements Review
AAE 451, SENIOR DESIGN SYSTEM REQUIREMENTS REVIEW TEAM 3: GOLDJET DIANE BARNEY DONALD BARRETT MICHAEL COFFEY JON COUGHLIN MARK GLOVER KEVIN LINCOLN ANDREW MIZENER JARED SCHEID ERIC SMITH Team GoldJet 1 System Requirements Review Table of Contents I. Mission Statement 2 II. Outline of NASA Competition 2 III. Key Assumptions 2 IV. Quality Function Deployment 3 V. Market Research 6 VI. Competitors 11 VII. City Pairs and Key Routes 12 VIII. Design Mission 16 IX. Economic Mission 19 X. Aircraft Sizing 20 XI. Summary and Next Steps 24 XII. References 27 Team GoldJet 2 System Requirements Review I. Mission Statement To design a profitable supersonic aircraft capable of Trans-Pacific travel to meet the needs of airlines and their passengers around the world. II. Outline of NASA Competition The NASA Aeronautics Research Mission Directorate’s (ARMD) 2008-2009 University Competition calls for the design of an N+2 generation supersonic aircraft which would have initial operational capability (IOC) in 2020. More specific goals for the aircraft as outlined by the competition guidelines include: Cruise speed of Mach 1.6 to 1.8 Design Range of 4000 nautical miles Payload of 35-70 passengers, mixed class Fuel Efficiency of 3 passenger-miles per pound of fuel Takeoff field length < 10,000 feet for airport compatibility Supersonic cruise efficiency Low sonic boom (<70 PldB) In addition, entries to the competition are to identify the possible market for a small supersonic airliner, develop design and economic missions for the aircraft (including likely routes), identify technologies that might enable the aircraft design, and complete a conceptual sizing. -
Environautics EN-1
Environautics EN -1 Response to the 2009 -2010 AIAA Foundation Undergraduate Team Aircraft Design Competition Presented by Virginia Polytechnic Institute and State University Left to Right: Justin Cox, Julien Fenouil, Jason Henn, Ryan Hofmeister, Michael Caporellie, Justin Camm, August Sarrol, Richie Mohan Environautics Team Roster ii Executive Summary Environautics presents the EN-1 as a solution to the 2009-2010 American Institute of Aeronautics and Astronautics (AIAA) Undergraduate Aircraft Design Competition Request For Proposal (RFP). The design will serve as an environmentally friendly and efficient strut-braced wing commercial transport to replace the Boeing 737 and Airbus 320. The RFP calls for a medium-range, biofuel-capable transport aircraft capable of carrying 175 passengers and cargo over a range of up to 3500 nautical miles and entering service by the year 2020. The main drivers for the proposal include maximizing performance capabilities with respect to the given RFP mission and maintaining a competitive commercial advantage while reducing the aircraft’s overall environmental impact through improved efficiency and usage of biofuels. The requirements of the RFP are discussed in Section 2.1. The proposed design incorporates the strut-braced wing design, a design proven in lightweight general aviation aircraft that enables a reduction of the weight of the main wing spar, allowing for efficiency enhancements through reduced wing thickness and sweep angle. The inclusion of advanced biofuels in the design minimizes performance penalties while reducing the aircraft’s environmental impact, further enhancing the competitive capability of the design compared to existing aircraft in areas such as operating costs. Operating costs are reduced further through use of advanced technologies that permit the aircraft to operate at increased efficiency and fewer delays. -
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 -
J-20 Stealth Fighter: China's First Strike Weapon
Foreign Affairs, Defence and Trade Committee Joint Strike Fighter Inquiry Department of the Senate PO Box 6100 Parliament House Canberra ACT 2600 Dear Chairman and Committee Members The Planned Acquisition of the F-35A Joint Strike Fighter Please find following my submission to this Inquiry. Yours faithfully, David Archibald Submission to the Joint Strike Fighter Inquiry Table of Contents Page 1. Executive Summary 2 2. Australia’s Future Air Defence Needs 3 3. Costs and Benefits of the F-35 Program 6 4. Changes in the Acquisition Timeline 7 5. The Performance of the F-35 in Testing 13 5.1 Introduction to the deficiencies of the F-35 13 5.2 Basing 18 5.3 Fuel Temperature 21 5.4 Engine 23 5.5 Acquisition Cost 24 5.6 Operating Cost 26 5.7 Directed Energy Weapon 28 5.8 DAS-EOTS 28 5.9 Manoeuvrability 29 5.10 Maintenance 31 5.11 Software 33 5.12 Pilot Training 33 5.13 Helmet Failure 34 5.14 Block Buy Contract 35 5.15 Stealth 35 5.16 Autonomic Logistics Information System 36 6. Potential Alternatives to the F-35 38 6.1 The Evolution of Fighter Aircraft 38 6.2 Fighter design considerations 39 6.3 How To Win In Air-To-Air Combat 45 6.4 Graphical Representation of Aircraft Attributes 46 6.5 Discussion of Alternatives to the F-35 56 6.6 F-18 Super Hornet 58 6.7 Gripen E 58 7. Any Other Related Matters 62 7.1 Basing and Logistics 62 7.2 Maintenance 62 7.3 Interim Aircraft 62 7.4 Aging of the F/A-18 A/B Hornet Aircraft 62 7.5 The US – Australia Alliance 64 8. -
Aircraft Fuel Consumption – Estimation and Visualization
1 Project Aircraft Fuel Consumption – Estimation and Visualization Author: Marcus Burzlaff Supervisor: Prof. Dr.-Ing. Dieter Scholz, MSME Delivery Date: 13.12.2017 Faculty of Engineering and Computer Science Department of Automotive and Aeronautical Engineering URN: http://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2017-12-13.019 Associated URLs: http://nbn-resolving.org/html/urn:nbn:de:gbv:18302-aero2017-12-13.019 © This work is protected by copyright The work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License: CC BY-NC-SA http://creativecommons.org/licenses/by-nc-sa/4.0 Any further request may be directed to: Prof. Dr.-Ing. Dieter Scholz, MSME E-Mail see: http://www.ProfScholz.de This work is part of: Digital Library - Projects & Theses - Prof. Dr. Scholz http://library.ProfScholz.de Published by Aircraft Design and Systems Group (AERO) Department of Automotive and Aeronautical Engineering Hamburg University of Applied Science This report is deposited and archived: Deutsche Nationalbiliothek (http://www.dnb.de) Repositorium der Leibniz Universität Hannover (http://www.repo.uni-hannover.de) This report has associated published data in Harvard Dataverse: http://doi.org/10.7910/DVN/2HMEHB Abstract In order to uncover the best kept secret in today’s commercial aviation, this project deals with the calculation of fuel consumption of aircraft. With only the reference of the aircraft manu- facturer’s information, given within the airport planning documents, a method is established that allows computing values for the fuel consumption of every aircraft in question. The air- craft's fuel consumption per passenger and 100 flown kilometers decreases rapidly with range, until a near constant level is reached around the aircraft’s average range. -
Etu – V Tulpar
2017-2018 Undergraduate Team Engine Candidate Engines for a Next Generation Supersonic Transport ETU – V TULPAR TEAM MEMBERS Veli Can ÜSTÜNDAĞ - 921399 Çağdaş Cem ERGİN - 920976 Baran İPER - 921398 Onur TAN - 921395 Faculty Advisor Asst. Prof. Sıtkı USLU SIGNATURES Faculty Advisor Asst. Prof. Sıtkı USLU TOBB University of Economics and Technology Team Leader Cagdas Cem ERGIN TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 920976 Team Member Veli Can USTUNDAG TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921399 Team Member Baran IPER TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921398 Team Member Onur TAN TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921395 ii TABLE OF CONTENT LIST OF TABLES .................................................................................................................................................. v LIST OF FIGURES ............................................................................................................................................... vi NOMENCLATURE ............................................................................................................................................... ix 1. INTRODUCTION .......................................................................................................................................... 1 2. STATE OF THE -
Conceptual Design of a Passenger Aircraft for In-Flight Refueling
Master of Science Thesis Conceptual design of a passenger aircraft for in-flight refueling operations P.P.M. van der Linden B.Sc. 5 July 2013 Faculty of Aerospace Engineering ¤ Delft University of Technology Conceptual design of a passenger aircraft for in-flight refueling operations Master of Science Thesis For obtaining the degree of Master of Science in Aerospace Engineering at Delft University of Technology P.P.M. van der Linden B.Sc. 5 July 2013 Faculty of Aerospace Engineering ¤ Delft University of Technology Delft University of Technology Copyright c P.P.M. van der Linden B.Sc. All rights reserved. Delft University Of Technology Department Of Design, Integration and Operations of Aircraft and Rotorcraft The undersigned hereby certify that they have read and recommend to the Faculty of Aerospace Engineering for acceptance a thesis entitled \Conceptual design of a passenger aircraft for in-flight refueling operations" by P.P.M. van der Linden B.Sc. in partial fulfillment of the requirements for the degree of Master of Science. Dated: 5 July 2013 Head of department: Prof.Dr.-Ing. G. Eitelberg Supervisor: Dr.ir. G. La Rocca Reader: Dipl.-Ing. S. Zajac Reader: Mo Li M.Sc. Summary Nowadays a big challenge in aviation is represented by the scarcity of fossil fuels. Hence, there is a need for a more fuel efficient air transport system. A possible innovation is a change in operating mode. Conceptual design studies showed staged flight operations to be up to 40% more fuel efficient than non-stop operations. Staged flight operation uses extra stops to split up long range missions. -
Safran's Philippe Petitcolin. Safran Is Easily Europe Rsquo
50SKYSHADESImage not found or type unknown- aviation news SAFRAN'S PHILIPPE PETITCOLIN News / Personalities Image not found or type unknown © 2015-2021 50SKYSHADES.COM — Reproduction, copying, or redistribution for commercial purposes is prohibited. 1 Safran is easily Europe’s most diversified aerospace company, with a range of businesses covering airliner, helicopter and space rocket engines to security detection systems, and landing gear to unmanned air vehicles. However a year into the top job, chief executive Philippe Petitcolin is keen to slim down the partially state-owned group’s sprawling portfolio, divesting non-core subsidiaries in security, and using the proceeds – as well as revenues from Safran’s stake in the booming CFM International – to invest in enterprises in aerospace equipment that “fit our DNA”. At the same time – a decade after Safran came into existence with the merger of French household names Snecma and Sagem – he wants to create a group identity by rebranding its many operating companies. This will see some of the biggest names in aerospace, such as Snecma, Turbomeca, Labinal and Messier-Bugatti-Dowty, begin to disappear later this year. “We are 10 years old as a company and it is time to act and think as one Safran,” says Petitcolin, a 28- year veteran of the group, who previously ran engine maker Snecma and wiring specialist Labinal. Relentless demand for commercial aircraft means Safran’s aerospace propulsion business continues to dominate its revenues. Safran and General Electric each own 50% of 40-year-old joint venture CFM International, whose CFM56 has a roughly three-quarter share of the narrowbody market, powering Boeing 737s and its 737 Max successor, and about half of all Airbus A320 and A320neo family jets. -
Day 2 May 20, 2009
Special RAA 2009 RAA Annual Convention, Salt Lake City, Utah Convention News May 20, 2009 Issue 35 WEDNESDAY Available on the RAA website raa.org Recognizing the importance of addressing the media scrutiny following last week’s three-day NTSB hearing, the RAA Board of Directors and Presidents’ Council met nearly non-stop yesterday, in an unprecedented move. Virtually all of the 32 member airlines, plus Delta and US Airways mainline executives, were represented. All of them committed, under the RAA umbrella, to dedicate whatever resources are necessary to learn not only from the recent accident but also from the two-and-a-half years of a perfect safety record. The nation’s news media were welcomed to attend this week’s Annual Convention and view directly the industry’s singular focus on safety. RAA President Roger Cohen notes, “We’re taking this opportunity to showcase what we’ve done every year for nearly 40 years of collaborative work with the FAA, our airlines and industry partners to share the absolute best safety practices.” In the closed-door Presidents’ Council and Board of Directors meetings yesterday, discussion centered on advancing the multi-layered safety programs such as FOQA, ASAP, SMS and LOSA. The presidents also heard from John Nance (see related story below), Assistant DOT Secretary Christa Fornarotto and key staffers from Congress. Airline CEOs had a private Exhibit Hall walk-thru yesterday afternoon prior to the official ribbon-cutting ceremony (see picture below). Praising the regional airline industry for its “mammoth achievement of professionalism and safety levels equal to main- stream airlines…and probably higher,” John Nance, an internationally recognized air safety analyst and advocate, cautioned regional airline executives to withstand the media scrutiny after the Colgan Air accident and “celebrate that you have accomplished a tremendous effort.” Now completing more than 50% of all the nation’s flights, regionals are the backbone of the air transportation system. -
Wh/Kg Batteries
Technical and Environmental Assessment of All-Electric 180-Passenger Commercial Aircraft by Albert Reuben Gnadt B.S. Mechanical Engineering, University of Wisconsin-Madison, 2015 Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY February 2018 @ Massachusetts Institute of Technology 2018. All rights reserved. Signature redacted A u th o r................................................................................................................................. Department of Aeronautics and Astronautics February 1, 2018 Signature redacted C ertified by ................................................................ ... Sleven R. H. Barrett Associate Professor, Aeronautics and Astronautics Thesis Supervisor Signature redacted Accepted by.......................................... .................... Hamsa Balakrishnan MASSACHUSETS INSTITUTE OF TECHNOLOGY Associate Professor, Aeronautics and Astronautics Chair, Graduate Program Committee MAR 12 2019 LIBRARIES ARCHIVES 2 Technical and Environmental Assessment of All-Electric 180-Passenger Commercial Aircraft by Albert Reuben Gnadt Submitted to the Department of Aeronautics and Astronautics on February 1, 2018 in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics Abstract Aviation emissions contribute to climate change, and all-electric aircraft offer an opportunity