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VTOL Hybrids: Tiltrotors Are Gaining Acceptance Nihad E Daidzic,, Ph.D., Sc.D
Minnesota State University, Mankato From the SelectedWorks of Nihad E. Daidzic, Dr.-Ing., D.Sc., ATP, CFII, MEI February, 2017 VTOL hybrids: Tiltrotors are gaining acceptance Nihad E Daidzic,, Ph.D., Sc.D. This work is licensed under a Creative Commons CC_BY-NC-ND International License. Available at: https://works.bepress.com/nihad-daidzic/30/ VTOL HYBRIDS Tiltrotors are gaining acceptance Led by Bell’s XV3 and XV15 and military service-proven Bell-Boeing V22, Leonardo will market the AW609 with other wing & rotor hybrids forthcoming. ry-wing VTOL aircraft that can hov- er, ly vertically up and down, and ly forward, sideways and backward – simply amazing machines. Heli- copters produce thrust as a vector component of the total lift force by effectively tilting the main rotor disc. Gyroplanes, on the other hand, 1st lown in 1923, are hybrids between helicopters and airplanes in which case the lift-producing rotary-wing is in the constant state of autorota- tion (windmilling), while horizontal thrust is normally produced by an internal combustion engine driving conventional propellers. So why do Photo courtesy Leonardo we need yet another airplane-heli- Leonardo AW609, jointly developed by Bell Helicopter and AgustaWestland, holds promise to be copter crossbreed? We need it be- the 1st tiltrotor aircraft certified for civilian operations. Configuration options include corporate, cause helicopters and gyroplanes SAR and EMS. Projected max range is 1100 nm with aux fuel tank, cruise speed of up to 275 kts. are limited by low cruising airspeeds and ranges, while airplanes are not By Nihad Daidzic, PhD, ScD cipal innovations in the published VTOL-capable. -
PROGRAM #Aiaascitech
9–13 JANUARY 2017 GRAPEVINE, TX Addressing Full Spectrum Disruptions Across the Global Aerospace Community PROGRAM www.aiaa-SciTech.org #aiaaSciTech 17-4000 WHAT’S IMPOSSIBLE TODAY WON’T BE TOMORROW. AT LOCKHEED MARTIN, WE’RE ENGINEERING A BETTER TOMORROW. We are partnering with our customers to accelerate manufacturing innovation from the laboratory to production. We push the limits in additive manufacturing, advanced materials, digital manufacturing and next generation electronics. Whether it is solving a global crisis like the need for clean drinking water or travelling even deeper into space, advanced manufacturing is opening the doors to the next great human revolution. Learn more at lockheedmartin.com © 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech Forum Welcome Welcome to the 2017 AIAA Science and Technology Forum and Exposition (AIAA SciTech Forum) – the world’s largest event for aerospace research, development, and technology! Only here will you find the diversity of topics, caliber of speakers, and level of discourse about issues that directly impact your work, your career, and your industry – we are confident you will leave Grapevine prepared to shape the future of aerospace in new and exciting ways. Chuck Gustafson Jill Marlowe By bringing together 11 aerospace science and technology conferences, and by attracting attendees The Aerospace NASA Langley from across academia, industry, and government, AIAA SciTech will give you an unparalleled Corporation Research Center opportunity to hear from industry thought leaders, interact with your peers, and begin the inspired exchange of ideas that so often leads to breakthroughs in our community. Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine some of the most critical issues facing aerospace today, especially the role that disruption plays in our community for better or worse. -
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. -
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner Andrew S. Hahn 1 NASA Langley Research Center, Hampton, VA, 23681 Most jet airliner conceptual designs adhere to conventional takeoff and landing performance. Given this predominance, takeoff and landing performance has not been critical, since it has not been an active constraint in the design. Given that the demand for air travel is projected to increase dramatically, there is interest in operational concepts, such as Metroplex operations that seek to unload the major hub airports by using underutilized surrounding regional airports, as well as using underutilized runways at the major hub airports. Both of these operations require shorter takeoff and landing performance than is currently available for airliners of approximately 100-passenger capacity. This study examines the issues of modeling performance in this now critical flight regime as well as the impact of progressively reducing takeoff and landing field length requirements on the aircraft’s characteristics. Nomenclature CTOL = conventional takeoff and landing FAA = Federal Aviation Administration FAR = Federal Aviation Regulation RJ = regional jet STOL = short takeoff and landing UCD = three-dimensional Weissinger lifting line aerodynamics program I. Introduction EMAND for air travel over the next fifty to D seventy-five years has been projected to be as high as three times that of today. Given that the major airport hubs are already congested, and that the ability to increase capacity at these airports by building more full- size runways is limited, unconventional solutions are being considered to accommodate the projected increased demand. Two possible solutions being considered are: Metroplex operations, and using existing underutilized runways at the major hub airports. -
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. -
Ramp Fee Schedule
RAMP FEE SCHEDULE Ramp Fees (charged by aircraft category and waived with purchase of minimum fuel load): Transport Aircraft Min. Gallons Ramp Fee B-717/DC-9 200 $550.00 B-727-200 200 $550.00 B-737-200/300/400/700/800/BBJ1/BBJ2 200 $550.00 BAe-146/ Avro RJ85 200 $550.00 BAC 111 200 $550.00 Embraer ERJ 170 200 $550.00 C130 200 $550.00 Super Heavy Jets Min. Gallons Ramp Fee Global Express 150 $200.00 Gulfstream G-V, G-550, 650 150 $200.00 Heavy Jet Aircraft Min. Gallons Ramp Fee Citation X / 10 / Cit 750 100 $150.00 Citation Sovereign / Cit 680 100 $150.00 Challenger CL-300/600/601/604/605 100 $150.00 C-Regional Jet / CRJ 200/700/900 150 $150.00 Embraer 145 Legacy 150 $150.00 Falcon-50/900/2000 100 $150.00 Gulfstream G-II,G-III & GIV & G-450 100 $150.00 G200 / Galaxy 100 $150.00 Jetstar I & II 100 $150.00 Medium Jet Aircraft Min. Gallons Ramp Fee Astra / Astra SPX / G-100 75 $125.00 Citation Excel / Cit 560XL 75 $125.00 Citation III/VI/VII / Cit 650 75 $125.00 Falcon-20/200 75 $125.00 Hawker HS-125-700/800/1000 75 $125.00 Learjet LR-40/45/55/60 75 $125.00 Sabreliner NA-40/60/65/80 75 $125.00 Westwind WW-1123/24/24 II 75 $125.00 BOE-234LR/UT (Chinook) (Helicopter) 75 $125.00 Sikorsky S-92 (Helicopter) 75 $125.00 Super Puma AS332 (Helicopter) 75 $125.00 Westland EH-101 (Helicopter) 75 $125.00 Light Jet Aircraft Min. -
Global Fleet & Mro Market Forecast Summary
GLOBAL FLEET & MRO MARKET FORECAST SUMMARY 2017-2027 AUTHORS Tom Cooper, Vice President John Smiley, Senior Manager Chad Porter, Technical Specialist Chris Precourt, Technical Analyst For over a decade, Oliver Wyman has surveyed aviation and aerospace senior executives and industry influencers about key trends and challenges across the Maintenance, Repair, and Overhaul market. If you are responsible for maintenance and engineering activities at a carrier, aftermarket activities at an OEM, business operations at an MRO, or a lessor, you may want to participate in our survey. For more information, please contact our survey team at: [email protected]. To read last year’s survey, please see: http://www.oliverwyman.com/our-expertise/insights/2016/apr/mro-survey-2016.html . CONTENTS 1. EXECUTIVE SUMMARY 1 2. STATE OF THE INDUSTRY 5 Global Economic Outlook 7 Economic Drivers 11 3. FLEET FORECAST 17 In-Service Fleet Forecast 18 4. MRO MARKET FORECAST 31 Copyright © Oliver Wyman 1 EXECUTIVE SUMMARY EXECUTIVE SUMMARY Oliver Wyman’s 2017 assessment and 10-year outlook for the commercial airline transport fleet and the associated maintenance, repair, and overhaul (MRO) market marks the 17th year of supporting the industry with informed, validated industry data. This has become the most credible go-to forecast for many executives in the airline and MRO industry as well as for those with financial interests in the sector, such as private equity firms, investment banks and investment analysts. The global airline industry has made radical changes in the last few years and is producing strong financial results. While the degree of success varies among the world regions, favorable fuel prices and widespread capacity discipline are regarded as key elements in the 2016 record high in global profitability ($35.6 billion). -
Future of Vertical Flight
www.vtol.org Kenneth Swartz, Regional Director – Americas The Vertical Flight Society www.vtol.org | [email protected] Kitty Hawk Cora © Vertical Flight Society: CC-BY-SA 4.0 © Vertical Flight Society: CC-BY-SA 4.0 Released March 2018 1 www.vtol.org . Founded as “The American Helicopter Society, Inc.” 75 years ago in Connecticut on Feb. 25, 1943 – “For the purpose of collecting, compiling and disseminating information concerning the helicopter” – Sikorsky Aircraft received its order for the first American helicopters on January 5, 1943 (28 XR-4 helicopters) . The first and longest-serving helicopter non-profit Sikorsky XR-4 helicopter – Founding members Igor Sikorsky, Arthur Young, Frank Piasecki, Courtesy of Sikorsky Aircraft Corp. Stanley Hiller, Reggie Brie, A.A. Griffiths, etc. – Included engineers, pilots, operators and presidents from industry, academia and government in Allied countries . Now 6,000 individual and 95 corporate members . Advancing vertical flight worldwide First Annual AHS Awards Banquet Born with the American Helicopter Industry Oct. 7, 1944 © Vertical Flight Society: CC-BY-SA 4.0 2 www.vtol.org © Vertical Flight Society: CC-BY-SA 4.0 3 www.vtol.org . The international professional society for those working to advance vertical flight – Founded in 1943 as the American Helicopter Society – Everything from VTOL MAVs/UAS to helicopters and eVTOL to STOVL (everything vertical except rockets) CFD of Joby S4, Aug 2015 . Expands knowledge about vertical flight technology and promotes its application around the world . Advances safety and acceptability . Advocates for vertical flight R&D funding . Helps educate and support today’s and tomorrow’s vertical flight engineers and leaders VFF Scholarship Winners at AHS Forum 71, May 2015 © Vertical Flight Society: CC-BY-SA 4.0 4 www.vtol.org . -
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. -
Chapter Iv Regionals/Commuters
CHAPTER IV REGIONALS/COMMUTERS For purposes of the Federal Aviation REVIEW OF 20032 Administration (FAA) forecasts, air carriers that are included as part of the regional/commuter airline industry meet three criteria. First, a The results for the regional/commuter industry for regional/commuter carrier flies a majority of their 2003 reflect the continuation of a trend that started available seat miles (ASMs) using aircraft having with the events of September 11th and have been 70 seats or less. Secondly, the service provided by drawn out by the Iraq War and Severe Acute these carriers is primarily regularly scheduled Respiratory Syndrome (SARS). These “shocks” to passenger service. Thirdly, the primary mission of the system have led to the large air carriers posting the carrier is to provide connecting service for its losses in passengers for 3 years running. The code-share partners. losses often reflect diversions in traffic to the regional/commuter carriers. These carriers During 2003, 75 reporting regional/commuter recorded double-digit growth in both capacity and airlines met this definition. Monthly traffic data for traffic for the second time in as many years. History 10 of these carriers was compiled from the has demonstrated that the regional/commuter Department of Transportation’s (DOT) Form 41 industry endures periods of uncertainty better than and T-100 filings. Traffic for the remaining the larger air carriers. During the oil embargo of 65 carriers was compiled solely from T-100 filings. 1 1973, the recession in 1990, and the Gulf War in Prior to fiscal year 2003, 10 regionals/commuters 1991, the regional/commuter industry consistently reported on DOT Form 41 while 65 smaller outperformed the larger air carriers. -
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.