Annual Report 2017/18
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Effectiveness of the Compound Helicopter Configuration in Rotorcraft Performance Increase
transactions on aerospace research 4(261) 2020, pp.81-106 DOI: 10.2478/tar-2020-0023 eISSN 2545-2835 effectiveness of the compound helicopter configuration in rotorcraft performance increase Jarosław stanisławski Retired doctor of technical sciences [email protected] • ORCID: 0000-0003-1629-4632 abstract The article presents the results of calculations applied to compare flight envelopes of varying helicopter configurations. Performance of conventional helicopter with the main and tail rotors, in the case of compound helicopter, can be improved by applying wings and pusher propellers which generate an additional lift and horizontal thrust. The simplified model of a helicopter structure, consisting of a stiff fuselage and the main rotor treated as a stiff disk, is applied for evaluation of the rotorcraft performance and the required range of control system deflections. The more detailed model of deformable main rotor blades, applying the Galerkin method, is used to calculate rotor loads and blade deformations in defined flight states. The calculations of simulated flight states are performed considering data of a hypothetical medium class helicopter with the take-off mass of 6,000kg. In the case of both of the helicopter configurations, the articulated main rotor hub is taken under consideration. According to the Galerkin method, the elastic blade model allows to compute blade deformations as a combination of the blade bending and torsional eigen modes. Introduction of additional wing and pusher propellers allows to increase the range of operational speed over 300 km/h. Results of the simulation are presented as time- runs of rotor loads and blade deformations and in a form of disk distribution plots of rotor parameters. -
Aircraft Requirements for Sustainable Regional Aviation
aerospace Article Aircraft Requirements for Sustainable Regional Aviation Dominik Eisenhut 1,*,† , Nicolas Moebs 1,† , Evert Windels 2, Dominique Bergmann 1, Ingmar Geiß 1, Ricardo Reis 3 and Andreas Strohmayer 1 1 Institute of Aircraft Design, University of Stuttgart, 70569 Stuttgart, Germany; [email protected] (N.M.); [email protected] (D.B.); [email protected] (I.G.); [email protected] (A.S.) 2 Aircraft Development and Systems Engineering (ADSE) BV, 2132 LR Hoofddorp, The Netherlands; [email protected] 3 Embraer Research and Technology Europe—Airholding S.A., 2615–315 Alverca do Ribatejo, Portugal; [email protected] * Correspondence: [email protected] † These authors contributed equally to this work. Abstract: Recently, the new Green Deal policy initiative was presented by the European Union. The EU aims to achieve a sustainable future and be the first climate-neutral continent by 2050. It targets all of the continent’s industries, meaning aviation must contribute to these changes as well. By employing a systems engineering approach, this high-level task can be split into different levels to get from the vision to the relevant system or product itself. Part of this iterative process involves the aircraft requirements, which make the goals more achievable on the system level and allow validation of whether the designed systems fulfill these requirements. Within this work, the top-level aircraft requirements (TLARs) for a hybrid-electric regional aircraft for up to 50 passengers are presented. Apart from performance requirements, other requirements, like environmental ones, Citation: Eisenhut, D.; Moebs, N.; are also included. -
2018 Undergraduate Team Aircraft Design Competition Hybrid-Electric
2017 – 2018 Undergraduate Team Aircraft Design Competition Hybrid-Electric General Aviation Aircraft (HEGAA) Presented by Federal University of Uberlândia Department of Aerospace Engineering Minas Gerais, Brazil 2017 – 2018 Undergraduate Team Aircraft Design Competition Hybrid-Electric General Aviation Aircraft (HEGAA) Presented by Federal University of Uberlândia Department of Aerospace Engineering Minas Gerais, Brazil Team Members AIAA Numbers Signatures Alexandre Acerra Gil 922668 Eduardo Pavoni Gamba 922678 Gabriel Araújo Hernández 922675 Guilherme Miquelim Caires 922581 Higor Luis Silva 922459 João Paulo Vieira 922563 Kimberlly Costa Carvalho 922564 Luiz Gustavo Santiago 922576 Pedro Brito 922566 Roberto Martins de Castro Neto 922571 Advisor: Dr. Thiago A. M. Guimarães - 498079 Table of Contents 1. Introduction .......................................................................................................................................................... 6 2. Design Requirements and Proposals .................................................................................................................... 7 3. Market Research ................................................................................................................................................... 9 4. Conceptual Design .............................................................................................................................................. 10 4.1. Initial Design Estimate ................................................................................................................................. -
Siemens Eaircraft Overview
eAircraft: Hybrid-elektrische Antriebe für Luftfahrzeuge Dr. Frank Anton, Siemens AG, Corporate Technology 14. Tag der Deutschen Luft- und Raumfahrtregionen, Potsdam, 10. September 2019 © Siemens AG 2019 siemens.com We develop hybrid electric propulsion systems for aircraft Hybrid-electric propulsion is a scalable technology eVTOL potentially large number economy of scale Enabler to reduce total cost of ownership and envinronmental impact: Hybrid electric propulsion Useful range Decreased fuel flow & emission Separation of power generation and thrust generation Silent propulsion Distributed propulsion Increased aerodynamic efficiency Vectorized thrust eSTOL, eVTOL Page 2 Dr. Frank Anton, Siemens AG eAircraft September 10th, 2019 Unrestricted © Siemens AG 2019. All rights reserved The eAircraft portfolio has been designed to meet aerospace requirements and is now on the way to industrialization & certification The eAircraft portfolio has been shaped by close collaboration with partners such as Airbus. In the lower power classes, the systems have already been tested in flight and are being installed in first commercial applications. In the high power classes, a 2 MW lab demonstrator is currently awaiting test results and a design of a 10 MW generator based on superconducting technology exists as digital twin. Page 3 Dr. Frank Anton, Siemens AG eAircraft September 10th, 2019 Unrestricted © Siemens AG 2019. All rights reserved Our core portfolio – electric propulsion units (EPU) for applications with high power/weight requirements Condition-based Services System Integration Controller Fuel Battery Cell DC/DC Inverter Power Signal AC/DC DC/AC Generator Distri- Distri- Motor G Inverter Inverter bution bution Turbine/ICE Siemens Trading item Page 4 Dr. Frank Anton, Siemens AG eAircraft September 10th, 2019 Unrestricted © Siemens AG 2019. -
Hybrid-Electric Aircraft: Conceptual Design, Structural and Aeroelastic Analyses
ALEXANDRE ACERRA GIL HIGOR LUIS SILVA HYBRID-ELECTRIC AIRCRAFT: CONCEPTUAL DESIGN, STRUCTURAL AND AEROELASTIC ANALYSES UNIVERSIDADE FEDERAL DE UBERLÂNDIA FACULDADE DE ENGENHARIA MECÂNICA 2017 ALEXANDRE ACERRA GIL HIGOR LUIS SILVA HYBRID-ELECTRIC AIRCRAFT: CONCEPTUAL DESIGN, STRUCTURAL AND AEROELASTIC ANALYSES Projeto de Conclusão de Curso apresentado ao Curso de Graduação em Engenharia Aeronáutica da Universidade Federal de Uberlândia, como parte dos requisitos para a obtenção do título de BACHAREL em ENGENHARIA AERONÁUTICA. Área de concentração: Projeto Aeronáutico, Mecânica dos Sólidos e Vibrações. Orientador: Prof. Dr. Thiago Augusto Machado Guimarães UBERLANDIA - MG 2017 HYBRID-ELECTRIC AIRCRAFT: CONCEPTUAL DESIGN, STRUCTURAL AND AEROELASTIC ANALYSES Projeto de conclusão de curso APROVADO pelo Colegiado do Curso de Graduação em Engenharia Aeronáutica da Faculdade de Engenharia Mecânica da Universidade Federal de Uberlândia. BANCA EXAMINADORA ________________________________________ Prof. Dr. Thiago Augusto Machado Guimarães Universidade Federal de Uberlândia ________________________________________ Prof. Dr. Leonardo Sanches Universidade Federal de Uberlândia ________________________________________ Prof. Dr. Tobias Souza Morais Universidade Federal de Uberlândia UBERLANDIA - MG 2017 To our moms and dads. ACKNOWLEDGEMENTS I would like to thank all my family and especially my mom and dad, Alessandra and Sergio, for all the unconditional support they gave me during my journey in Uberlândia, helping me through difficult moments and encouraging me to always move on. I would also like to thank my colleagues and professors from the Aeronautical Engineering Teaching Laboratory who participated actively in the development of this work, especially my friends Guilherme Miquelim, Gabriel Hernández, João Paulo Vieira, Kimberlly Costa, Luiz Santiago, Pedro Brito and Eduardo Gamba; professors Dr. Leonardo Sanches, MSc. Giuliano Venson and Dr. -
Preliminary Feasibility Analysis on the Use of Hydrogen Fuel Cells for a Hybrid-Electric Aircraft Testbed
Preliminary Feasibility Analysis on the use of Hydrogen Fuel Cells for a Hybrid-Electric Aircraft Testbed Evan Gibney Co-op Student National Research Council Canada 1200 Montreal Rd, Ottawa, ON K1A 0R6 [email protected] Overview A lithium-ion battery based powertrain was developed for a Cessna 337G Skymaster under the Hybrid Electric Aircraft Testbed (HEAT II) project at the National Research Council Canada (NRC). As the project approaches its conclusion, a future area of exploration for the HEAT project may be in the integration of hydrogen fuel cells onto the Cessna aircraft. Due to their low carbon emissions and high specific energy density relative to batteries, fuel cells are becoming an increasingly important area of research for the future of low emissions aviation. Fuel cells are expected to play a large role in helping the aviation industry meet the ambitious 2050 target for 50% reduction in carbon emissions relative to 2005 levels. This is evidenced by the significant growth of hydrogen based aviation developments in recent years. Companies such as H2FLY have begun to demonstrate test flights using hydrogen propulsion systems. Additionally, the government of Canada has made clear the importance of hydrogen in the future of Canada’s energy landscape. In December of 2020, a report, titled, “Hydrogen Strategy for Canada, Seizing the Opportunities for Hydrogen, A Call to Action”, was released by Natural Resources Canada (NRCan) outlining the path towards a Canadian hydrogen economy by 2050. The report outlines the need to support further R&D, and encourage “Canadian demonstrations in emerging applications” such as aviation. -
Battery Centric Serial Hybrid Aircraft Performance and Design Space
Dissertations and Theses 5-2017 Battery Centric Serial Hybrid Aircraft Performance and Design Space Lenny Gartenberg Follow this and additional works at: https://commons.erau.edu/edt Part of the Aerospace Engineering Commons Scholarly Commons Citation Gartenberg, Lenny, "Battery Centric Serial Hybrid Aircraft Performance and Design Space" (2017). Dissertations and Theses. 327. https://commons.erau.edu/edt/327 This Thesis - Open Access is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Dissertations and Theses by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. BATTERY CENTRIC SERIAL HYBRID AIRCRAFT PERFORMANCE AND DESIGN SPACE A Thesis Submitted to the Faculty of Embry-Riddle Aeronautical University by Lenny Gartenberg In Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering May 2017 Embry-Riddle Aeronautical University Daytona Beach, Florida iii TABLE OF CONTENTS LIST OF TABLES .............................................................................................................. v LIST OF FIGURES ........................................................................................................... vi SYMBOLS ....................................................................................................................... viii ABBREVIATIONS ............................................................................................................ x ABSTRACT ...................................................................................................................... -
Aircraft Technology Roadmap to 2050 | IATA
Aircraft Technology Roadmap to 2050 NOTICE DISCLAIMER. The information contained in this publication is subject to constant review in the light of changing government requirements and regulations. No subscriber or other reader should act on the basis of any such information without referring to applicable laws and regulations and/or without taking appropriate professional advice. Although every effort has been made to ensure accuracy, the International Air Transport Association shall not be held responsible for any loss or damage caused by errors, omissions, misprints or misinterpretation of the contents hereof. Furthermore, the International Air Transport Association expressly disclaims any and all liability to any person or entity, whether a purchaser of this publication or not, in respect of anything done or omitted, and the consequences of anything done or omitted, by any such person or entity in reliance on the contents of this publication. © International Air Transport Association. All Rights Reserved. No part of this publication may be reproduced, recast, reformatted or transmitted in any form by any means, electronic or mechanical, including photocopying, recording or any information storage and retrieval system, without the prior written permission from: Senior Vice President Member & External Relations International Air Transport Association 33, Route de l’Aéroport 1215 Geneva 15 Airport Switzerland Table of Contents Table of Contents .............................................................................................................................................................................................................. -
Russian Helicopters to Make Aircraft for Regional
www.aeromag.in n March - April 2018 | Vol 12 | Issue 2 HAL Invites Private Players to Manufacture ALH Dhruv in association with Society of Indian Aerospace Technologies & Industries Advertising is all about visibility We provide you the Maximum Advertise with AEROMAG Official Show Dailies For details Contact : Preethi M | Email: [email protected] | [email protected] Mob: +91 9448447509 1 AEROSPACE th 5 DEFENCE Edition DIRECTORY A Compendium of Aerospace & Defence Industries in association with SOCIETY OF DEFENCE TECHNOLOGISTS 2018 -19 4A Unique Platform Connecting Aerospace & Defence Industries Globally 4More than 1200 Company Profiles 4Contact Address, Product Details 4Details of R & D Facilites 4List of Indian and Overseas Partners 4Certification Details 4Joint Venture Partner Details Pre - Publication Offer 4DPSU, DRDO, Private Industry Listing Cost : Rs. 2000 + 12% GST 4Product, Category Wise Indexing For Copies of the Directory Please Contact: Email : [email protected] Mob : +91 9448447509 / 9449061925 / 9480551925, Tel : +91 - 80-25284145 AEROMAG ASIA Aeronautical Society of India Building, Suranjandas Rd, Off Old Madras Rd, Bangalore - 560 075, Karnataka, India EOS GmbH India Branch Office( Electro Optical Systems)No.36, Sivananda Nagar, Kolathur| T : +91 80 25604055 / 9449061925. Email :[email protected] | www.aeromag.in 2 Chennai-600 099, IndiaPhone +91 443 964 8000 | 3 Fax +9144 3964 8099 | Mobile:+91984 003 3223 formnext_AufstellerA5_Linde.Liebherr.Ariane.Nextgeneration.Tireapplication.indd 3 09.11.2017 11:24:25 EDITORIAL The tenth edition Def expo India , the biennial Land, Naval and Internal Homeland Security Systems Exhibition, to be held at Chennai, Tamil Nadu, Content Editorial Advisory Board from 11th to 14th April 2018 offers an excellent 6 Countdown Begins for Defexpo 2018 Dr. -
Electrified Aircraft Propulsion John S
Summer 2020 AERONAUTICS The BRIDGE LINKING ENGINEERING AND SOCIETY Aeropropulsion: Advances, Opportunities, and Challenges Alan H. Epstein Hybrid Electric Aircraft to Improve Environmental Impacts of General Aviation Jean J. Botti Electrified Aircraft Propulsion John S. Langford and David K. Hall Supersonic Flight and Sustainability: A New Horizon Raymond Russell, Lourdes Maurice, and Rachel E. Devine Embracing the Risk Sciences to Enhance Air Travel Safety B. John Garrick and Ali Mosleh Some Steps toward Autonomy in Aeronautics John-Paul B. Clarke and Claire J. Tomlin Flying at the Edge of Space and Beyond: The Opportunities and Challenges of Hypersonic Flight Kevin G. Bowcutt Aerospace Prizes Inspire the Five I’s of Success: Imagination, Invention, Innovation, Investment, and Impact Darryll J. Pines EES Perspective: Ethical Decision Making and the Aviation Industry Elizabeth A. Hoppe Putting Out Fire … with Gasoline? A Pragmatic Path toward Clean Fuels Nicholas C. Margiewicz The mission of the National Academy of Engineering is to advance the well-being of the nation by promoting a vibrant engineering profession and by marshalling the expertise and insights of eminent engineers to provide independent advice to the federal government on matters involving engineering and technology. The BRIDGE NATIONAL ACADEMY OF ENGINEERING Gordon R. England, Chair John L. Anderson, President Corale L. Brierley, Vice President Julia M. Phillips, Home Secretary James M. Tien, Foreign Secretary Martin B. Sherwin, Treasurer Editor in Chief: Ronald M. Latanision Managing Editor: Cameron H. Fletcher Production Associate: Penelope Gibbs The Bridge (ISSN 0737-6278) is published quarterly by the National Acad emy of Engineering, 2101 Constitution Avenue NW, Washington, DC 20418. -
Conceptual Design of Operation Strategies for Hybrid Electric Aircraft
energies Article Conceptual Design of Operation Strategies for Hybrid Electric Aircraft Julian Hoelzen 1, Yaolong Liu 2,* ID , Boris Bensmann 1,*, Christopher Winnefeld 1, Ali Elham 3, Jens Friedrichs 4 and Richard Hanke-Rauschenbach 1 1 Institute of Electric Power Systems, Leibniz Universität Hannover, Appelstr. 9a, 30167 Hanover, Germany; [email protected] (J.H.); [email protected] (C.W.); [email protected] (R.H.-R.) 2 Aeronautics Research Centre Niedersachsen (NFL), Technische Universität Braunschweig, Hermann-Blenk-Straße 42, 38108 Braunschweig, Germany 3 Institute of Aircraft Design and Lightweight Structures, Technische Universität Braunschweig, Hermann-Blenk-Straße 35, 38108 Braunschweig, Germany; [email protected] 4 Institute of Jet Propulsion and Turbomachinery, TU Braunschweig, Hermann-Blenk-Straße 37, 38108 Brunswick, Germany; [email protected] * Correspondence: [email protected] (Y.L.); [email protected] (B.B.); Tel.: +49-531-391-66662 (Y.L.); +49-511-762-14404 (B.B.) Received: 15 December 2017; Accepted: 12 January 2018; Published: 16 January 2018 Abstract: Ambitious targets to reduce emissions caused by aviation in the light of an expected ongoing rise of the air transport demand in the future drive the research of propulsion systems with lower CO2 emissions. Regional hybrid electric aircraft (HEA) powered by conventional gas turbines and battery powered electric motors are investigated to test hybrid propulsion operation strategies. Especially the role of the battery within environmentally friendly concepts with significantly reduced carbon footprint is analyzed. Thus, a new simulation approach for HEA is introduced. The main findings underline the importance of choosing the right power-to-energy-ratio of a battery according to the flight mission. -
Daily News the European Rotorcraft Technology Launchpad
DAILY NEWS THE EUROPEAN ROTORCRAFT TECHNOLOGY LAUNCHPAD Airbus dominates DAY THREE 18 OCT 2018 show orders count HIGHLIGHTS Safe and sound Page 14 Ensuring the safety of helicopter crews can be achieved through a variety of measures that industry is continuously developing. Photo: Tony Skinner Having announced an impressive haul of 19 position, with 70% share – which is, of orders during Helitech International, largely course, great for the company,’ he said. buoyed by light single and light twin returns, ‘At the same time, when it comes to oil and Airbus continues to consolidate its strong gas, things are still challenging but showing Heavy metal global civil helicopter market position. signs of recovery. From my perspective, it will Page 20 Breaking the contracts down, the company take time. There is still over-capacity in the is set to deliver up to six H135s to air rescue market and real demand will take time.’ Are we likely to see heavy operator Royal Dutch Touring Club ANWB, as Stressing the need to address the entire models fade away as focus part of a framework agreement signed this helicopter market across light, medium and shifts towards the next week, while a split of three light single and heavy types, Even explained that Airbus will generation of fl ight? three light twin aircraft have been agreed not simply prioritise one segment over another. with French Alps civil operator SAF Group. ‘The core of our strategy is to be in a position to A further four H125s have been ordered address – with our large portfolio of products – by Norwegian operator Helitrans and will be all the needs of the market.