Methane Hydrates: More Than a Viable Aviation Fuel Feedstock Option
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Sustainable Jet Fuel for Aviation
Sustainable jet fuel for aviation Nordic perpectives on the use of advanced sustainable jet fuel for aviation Sustainable jet fuel for aviation Nordic perpectives on the use of advanced sustainable jet fuel for aviation Erik C. Wormslev, Jakob Louis Pedersen, Christian Eriksen, Rasmus Bugge, Nicolaj Skou, Camilla Tang, Toke Liengaard, Ras- mus Schnoor Hansen, Johannes Momme Eberhardt, Marie Katrine Rasch, Jonas Höglund, Ronja Beijer Englund, Judit Sandquist, Berta Matas Güell, Jens Jacob Kielland Haug, Päivi Luoma, Tiina Pursula and Marika Bröckl TemaNord 2016:538 Sustainable jet fuel for aviation Nordic perpectives on the use of advanced sustainable jet fuel for aviation Erik C. Wormslev, Jakob Louis Pedersen, Christian Eriksen, Rasmus Bugge, Nicolaj Skou, Camilla Tang, Toke Liengaard, Rasmus Schnoor Hansen, Johannes Momme Eberhardt, Marie Katrine Rasch, Jonas Höglund, Ronja Beijer Englund, Judit Sandquist, Berta Matas Güell, Jens Jacob Kielland Haug, Päivi Luoma, Tiina Pursula and Marika Bröckl ISBN 978-92-893-4661-0 (PRINT) ISBN 978-92-893-4662-7 (PDF) ISBN 978-92-893-4663-4 (EPUB) http://dx.doi.org/10.6027/TN2016-538 TemaNord 2016:538 ISSN 0908-6692 © Nordic Council of Ministers 2016 Layout: Hanne Lebech Cover photo: Scanpix Print: Rosendahls-Schultz Grafisk Copies: 100 Printed in Denmark This publication has been published with financial support by the Nordic Council of Ministers. However, the contents of this publication do not necessarily reflect the views, policies or recom- mendations of the Nordic Council of Ministers. www.norden.org/nordpub Nordic co-operation Nordic co-operation is one of the world’s most extensive forms of regional collaboration, involv- ing Denmark, Finland, Iceland, Norway, Sweden, and the Faroe Islands, Greenland, and Åland. -
The Deep Hot Biosphere: the Myth of Fossil Fuels Free
FREE THE DEEP HOT BIOSPHERE: THE MYTH OF FOSSIL FUELS PDF Thomas Gold,Freeman J. Dyson | 243 pages | 01 Jun 2001 | Springer-Verlag New York Inc. | 9780387952536 | English | New York, NY, United States The Deep Hot Biosphere: The Myth of Fossil Fuels - Thomas Gold - Google книги Post a comment. Total Pageviews. The Deep Hot Biosphere. It concerns of a microbial biosphere that exists at depth, profuse both within the Earth and probably other planets, feed by primordial and abiotic hydrocarbonsmainly methane and chemical energy. Deep levels in the Earth would be an environment that could form catalytic and autocatalytic molecules that contribute for the emergence of life. After, this deep primeval life developed a sophisticated apparatus to conquest the surface of planet - by photosynthesis - using energy from sunlight to dissociated water and carbon dioxide to produce carbohydrates, permitting autotrophy. The main reason consists in understanding the origin of hydrocarbons whose base is in Deep-Earth Gas Theory. Thomas Gold postulated that hydrocarbons such as oil, natural gas and black coal are primary compounds, i. He stated that hydrocarbons are surelly abiotic compounds and very common on Earth and the universe. In summary his ideas can thus be defined as its own quote:. The deep, hot biosphere. Gold, T. Sci, USA. Vol 89, pp. There are strong indications that microbial life is widespread at depth in the crust of the Earth, just as such life has been identified in numerous ocean vents. This life is not dependent on The Deep Hot Biosphere: The Myth of Fossil Fuels energy and photosynthesis for its primary energy supply, and it is essentially independent of the surface circumstances. -
Chemical Composition and Low-Temperature Fluidity Properties of Jet Fuels
processes Article Chemical Composition and Low-Temperature Fluidity Properties of Jet Fuels Alirio Benavides 1, Pedro Benjumea 1,* , Farid B. Cortés 2,* and Marco A. Ruiz 1 1 Grupo de Yacimientos de Hidrocarburos, Departamento de Procesos y Energía, Facultad de Minas, Universidad Nacional de Colombia, Sede Medellín, Medellín 050034, Colombia; [email protected] (A.B.); [email protected] (M.A.R.) 2 Grupo de Investigación en Fenómenos de Superficie—Michael Polanyi, Departamento de Procesos y Energía, Facultad de Minas, Universidad Nacional de Colombia, Sede Medellín, Medellín 050034, Colombia * Correspondence: [email protected] (P.B.); [email protected] (F.B.C.) Abstract: The physicochemical properties of petroleum-derived jet fuels mainly depend on their chemical composition, which can vary from sample to sample as a result of the diversity of the crude diet processed by the refinery. Jet fuels are exposed to very low temperatures both at altitude and on the ground in places subject to extreme climates and must be able to maintain their fluidity at these low temperatures otherwise the flow of fuel to turbine engines will be reduced or even stopped. In this work, an experimental evaluation of the effect of chemical composition on low-temperature fluidity properties of jet fuels (freezing point, crystallization onset temperature and viscosity at −20 ◦C) was carried out. Initially, a methodology based on gas chromatography coupled to mass spectrometry (GC–MS) was adapted to determine the composition of 70 samples of Jet A1 and Jet A fuels. This methodology allowed quantifying the content, in weight percentage, of five main families of hydrocarbons: paraffinic, naphthenic, aromatic, naphthalene derivatives, and tetralin- and indane-derived compounds. -
Sustainable Aviation Fuels Road-Map
SUSTAINABLE AVIATION FUELS ROAD-MAP Fueling the future of UK aviation sustainableaviation.co.uk Sustainable Aviation wishes to thank the following organisations for leading the work in producing this Road-Map: Sustainable Aviation (SA) believes the data forecasts and analysis of this report to be correct as at the date of publication. The opinions contained in this report, except where specifically attributed to, are those of SA, and based upon the information that was available to us at the time of publication. We are always pleased to receive updated information and opinions about any of the contents. All statements in this report (other than statements of historical facts) that address future market developments, government actions and events, may be deemed ‘forward-looking statements’. Although SA believes that the outcomes expressed in such forward-looking statements are based on reasonable assumptions, such statements are not guarantees of future performance: actual results or developments may differ materially, e.g. due to the emergence of new technologies and applications, changes to regulations, and unforeseen general economic, market or business conditions. CONTENTS EXECUTIVE SUMMARY INTRODUCTION 1.1 Addressing the sustainability challenge in aviation 1.2 The role of sustainable aviation fuels 1.3 The Sustainable Aviation Fuels Road-Map SUSTAINABLE AVIATION FUELS 2.1 Sustainability of sustainable aviation fuels 2.2 Sustainable aviation fuels types 2.3 Production and usage of sustainable aviation fuels to date THE FUTURE FOR SUSTAINABLE -
FACT SHEET 7: Liquid Hydrogen As a Potential Low- Carbon Fuel for Aviation
FACT SHEET 7: Liquid hydrogen as a potential low- carbon fuel for aviation This fact sheet aims to explain how current aviation fuels operate before providing descriptions of how alternative fuel options, like sustainable aviation fuels (SAF) and liquid hydrogen, could help meet the rigorous climate targets set by the aviation industry. Secondly, this document explores the limitations and opportunities of liquid hydrogen when it comes to the manufacturing, safety, current uses and outlooks. This document concludes with a discussion on policy, mandates and incentives on the topic of hydrogen as a potential fuel for aviation. Introduction – Why hydrogen? Aircraft fly thanks to a combination of air and a combustion process that occurs in the aircraft engines. The primary source of energy is the fuel. Each kilogram of fuel, which would occupy less than 1 litre of volume, contains a significant amount of energy, 42.8 MJ [1]. If we could convert the energy of a 1L bottle of fuel into electric energy to power a cell phone, the battery would last for over 2 months. This energy is extracted in the combustion chamber of the engine in the form of heat; Compressed air enters the combustion chamber and gets heated up to temperatures nearing 1,500°C. This hot high- pressure air is what ultimately moves the aircraft forward. Kerosene is composed of carbon and hydrogen (hence it’s a hydrocarbon fuel). When the fuel is completely burned, these carbon and hydrogen molecules recombine with oxygen to create water vapor (H2O) and carbon dioxide (CO2) (Fig.1). August 2019 Emissions: From Combustion: H2O + CO2 Other: NOx, nvPM SOx, soot Fuel in (C + H) Figure 1 Schematic of a turbofan engine adapted from: [2] Carbon dioxide will always be created as a by-product of burning a carbon-based fuel. -
Fire Test Evaluation Using the Kerosene and Aviation Fuel
Fire Test Evaluation using the Kerosene and Aviation Fuel K. S. Bang, J.C. Lee, C. S. Seo, K. S. Seo, H. J. Kim* Korea Atomic Energy Research Institute, 150 Dukjin-Dong, Yuseung-gu, Daejeon, Korea 305-353 *Korea Radioactive Waste Management Corporation, 150 Dukjin-Dong, Yuseung-gu, Daejeon, Korea 305-353 [email protected] Abstract The fire test was performed by using kerosene and Jet-A-1 as the fire source under a compartment condition in order to evaluate the flame temperature in the fire due to the release of the kerosene involving the impact of a vehicle, and the fire due to the release of Jet fuel involving the collision of an airplane. The combustion time of the Jet-A-1 was shorter than the kerosene. And the flame temperature in the Jet-A-1 was measured higher than the kerosene. The opening became bigger; the fuel consumption rate became bigger. Therefore, the flame temperature was higher when the size of the opening was big. In the compartment fire, the flame temperature gradually increased. Keywords: Fire Test, Compartment, Opening, Combustion, Flame Temperature 1. Introduction Regulatory requirements for a Type B package are specified in the Korea MEST Act 2009-37, IAEA Safety Standard Series No. TS-R-1, and the US 10 CFR Part [1~3]. These regulations are adequate to ensure the shipping package containment effectiveness for the transport conditions including most credible accident conditions; a 9 m drop onto an unyielding surface, a 1 m puncture onto a puncture bar, 30 minutes under 800 °C thermal, and an one hour immersion under a head of water of 200 m . -
SAFO 18015: Jet Fuel Contaminated with Diesel Exhaust Fluid (DEF)
SAFO Safety Alert for Operators SAFO 18015 U.S. Department DATE: 11/13/18 of Transportation Federal Aviation Flight Standards Service Administration Washington, DC http://www.faa.gov/other_visit/aviation_industry/airline_operators/airline_safety/safo A SAFO contains important safety information and may include recommended action. SAFO content should be especially valuable to air carriers in meeting their statutory duty to provide service with the highest possible degree of safety in the public interest. Besides the specific action recommended in a SAFO, an alternative action may be as effective in addressing the safety issue named in the SAFO. Subject: Jet Fuel Contaminated with Diesel Exhaust Fluid (DEF). Purpose: This SAFO alerts and advises aircraft operators, Fixed Base Operators (FBO), Federal Aviation Administration (FAA)-certificated repair stations, Flight Standard District Offices (FSDO), and foreign civil aviation authorities that certain aircraft refueled with jet fuel contaminated with DEF or used in refueling equipment that was exposed to DEF. Background: Between August 12 and August 16, 2018, five aircraft were identified as being serviced with jet fuel containing DEF at Miami-Opa Locka Executive Airport (OPF) located in Opa-locka, Florida. Also during the same time period, nine other aircraft were identified as being serviced using refueling equipment that had been exposed to DEF. An investigation revealed that Diesel exhaust fluid was inadvertently used instead of fuel system icing inhibitor (FSII) on a refueling truck at OPF and injected into the fuel with the truck’s FSII injection system. This affected both the aircraft receiving the contaminated fuel and the aircraft that were serviced with the refueling equipment that had been exposed to DEF. -
Investigation of the Effects of Civil Aviation Fuel Jet A1 Blends on Diesel Engine Performance and Emission Characteristics
Indian Journal of Engineering & Materials Science Vol. 21, April 2014, pp. 200-206 Investigation of the effects of civil aviation fuel Jet A1 blends on diesel engine performance and emission characteristics Hamit Solmaza*, Hasan Yamıkb, Yakup İçingüra & Alper Calamc aAutomotive Engineering Department, Faculty of Technology, Gazi University, 06500, Teknikokullar, Ankara, Turkey bEngineering Faculty, Bilecik University, 06570, Bilecik, Turkey, cAutomotive Technology Program, Atatürk Vocational High School, Gazi University, Ankara, Turkey Received 14 November 2012; accepted 10 January 2014 Study on use of aviation fuels in the internal combustion engines in road vehicles has been conducted for a long time. After the JP-8 is accepted as a single fuel on land and in the air (single fuel concept) by the North Atlantic Treaty Organization (NATO), the majority of these studies have focused on JP-8. For this reason, there is hardly any study on using the Jet A1, which is structurally very similar to the JP-8, in the internal combustion engine. However, in obligatory cases such as in periods of war, using the Jet A1 in the same way as the JP-8 in internal combustion engines may be required. In cold climates especially, the Jet A1 may gain strategic importance due to its very low freezing point. In this study, both the effects of the diesel and Jet A1 blends on engine performance and exhaust emissions in both the single cylinder, and the direct injection diesel engine have been examined. As a result, it has been determined that use of Jet A1 reduces engine torque to 5.85% and increases the specific fuel consumption to 8.77%. -
Sustainable Aviation Fuel from Ethanol Laurel Harmon VP Government Relations, Lanzatech
Sustainable Aviation Fuel from Ethanol Laurel Harmon VP Government Relations, LanzaTech LanzaTech Sustainable Aviation Fuel: ATJ-SPK from Ethanol Jet & Dehydration Oligomerization Hydrogenation Fractionation Diesel Ethanol Development and Scale Up Timeline 2016-2018: ASTM 2010-2012: Initial 2011+: 2014-2017: Scale up •LanzaTech Research 2018+: Flight Demos Research and Proof of Collaboration with and Fuel Production Report on Ethanol Based and Demonstration Concept Industry Leaders •Freedom Pines pilot ATJ-SPK Submitted Scale Fuel Production September 2016 •2010: PNNL facility •First Commercial flight on •Virgin Atlantic •ASTM SAF Standard •2011: DARPA •4,000 gallons of jet October 2, 2018 •HSBC produced including Ethanol as •2011: FAA Feedstock for Jet •DOE Demonstration Plant •Boeing •DOE demo funding •2012: DOE Published April 2018 •RSB •Based on LanzaTech data LanzaJet: Taking Off 4,000 gallons Jet 600 gallons Diesel Waste Gas Ethanol from RSB Certified Facility Grain Ethanol Jet A LanzaTech 50/50% v October 3rd 2018 First Commercial Flight Fuel Property Spec ATJ-SPK with Jet A Freeze Point, °C -40 max -61 -54 Energy Density, 42.8 min 44.4 43.8 MJ/kg Thermal Stability Baseline Excellent Excellent 4 Flights on 92% LanzaJet SPK Viscosity @ -40 °C 12 max 7.0 9.3 mm2/sec >80-90% Lower Contrails and Soot Particles Hydrogen % 13.4 min 15.1 14.5 April 1, 2018 8 min, Aromatics % Nil 8.8 D7566 ATJ SPK Annex A5 25 max Ethanol feedstock Sulfur, total mass % 0.30 max <0.001 0.02 Final blend ratio to max 50 % Path to Economic Volumes 2015 Lab -
Assessing the Sustainability Implications of Alternative Aviation Fuels
WORKING PAPER 2021-11 © 2021 INTERNATIONAL COUNCIL ON CLEAN TRANSPORTATION MARCH 2021 Fueling flight: Assessing the sustainability implications of alternative aviation fuels Authors: Nikita Pavlenko, Stephanie Searle Keywords: Aviation, biofuels, low-carbon fuels Aviation faces large technical barriers to making a transition to hydrogen or electricity- powered airframes, so the industry will probably have to rely on liquid fuels through 2050. That is particularly true for the medium- and long-haul flights that generate two- thirds of aviation emissions. If the industry is to meet its long-term climate goal of cutting greenhouse gas (GHG) emissions 50% by 2050 without curbing traffic growth or using out-of-sector carbon offsets, sustainable aviation fuels (SAFs) will need to play a key role. SAFs can be used to generate in-sector GHG reductions when they supplant conventional petroleum jet fuel. In 2018, less than 0.01% of aviation fuel came from alternative sources (Hupe, 2019; Graver, Zhang, & Rutherford, 2019). While reducing petroleum consumption in aviation is an important objective for decarbonization, the specific types of alternative fuels used to displace petroleum will determine the net climate impact of any alternative fuels policy. A fuel’s feedstock and its conversion process—together called the fuel pathway—determine the fuel’s life-cycle GHG emissions. The European Union’s recently announced Green New Deal framework calls for a clear regulatory roadmap for the decarbonization of aviation, to be achieved using a combination of new technology, SAFs, modal shift, and improved efficiency (European Parliament, 2020). As part of this effort, the European Commission announced the ReFuelEU initiative to deploy SAFs to decarbonize EU aviation (European Commission, n.d.). -
Alexander II and Gorbachev: the Doomed Reformers of Russia
University of Vermont UVM ScholarWorks UVM Honors College Senior Theses Undergraduate Theses 2017 Alexander II and Gorbachev: The Doomed Reformers of Russia Kate V. Lipman The University of Vermont Follow this and additional works at: https://scholarworks.uvm.edu/hcoltheses Recommended Citation Lipman, Kate V., "Alexander II and Gorbachev: The Doomed Reformers of Russia" (2017). UVM Honors College Senior Theses. 158. https://scholarworks.uvm.edu/hcoltheses/158 This Honors College Thesis is brought to you for free and open access by the Undergraduate Theses at UVM ScholarWorks. It has been accepted for inclusion in UVM Honors College Senior Theses by an authorized administrator of UVM ScholarWorks. For more information, please contact [email protected]. 1 Alexander II and Gorbachev: The Doomed Reformers of Russia Kate V. Lipman Thesis Submitted for College Honors in History Advisor: Denise J. Youngblood The University of Vermont May 2017 2 Note on Sources: There is, surprisingly, little available in English on the reign of Alexander II, therefore I rely primarily on the works of W.E. Mosse, N.G.O Pereira, and the collection of works on Russia’s reform period edited by Ben Eklof. W.E. Mosse’s book Alexander II and the Modernization of Russia, a secondary source, provides in-depth descriptions of the problems facing Alexander II when he came into power, the process of his reforms, descriptions of the reforms, and some of the consequences of those reforms including his assassination in 1881. Similarly, N.G.O Pereira’s Tsar-Liberator: Alexander II of Russia 1818-1881 is a secondary source, describing some of his reforms, but focuses most specifically on the process of the emancipation of the serfs, the emancipation itself and the impact it had on the population. -
S Alzburg S Eminar
S ALZBURG S EMINAR UNIVERSITIES PROJECT THE FIRST FOUR YEARS 1997–2000 MESSAGE his report is an overview of the first four years of the Salzburg TSeminar’s Universities Project, which was created to help promote FROM THE higher education reform in Central and East Europe and in the Russian Federation. It is also an acknowledgement and expression of gratitude to PRESIDENT those who made this Project possible by their generosity and their spirit of volunteerism. First and foremost, we owe this initiative to the AND THE visionary and sustained commitment of the William and Flora Hewlett Foundation and the W.K. Kellogg Foundation, which are funding the DIRECTOR Universities Project and its adjunct Visiting Advisors Program, respectively. Without the generous and steady support of these two OF THE foundations, none of the activities described herein would have happened. We are also grateful for the Project’s growing number of UNIVERSITIES partners and friends who have donated their time and expertise to give intellectual and practical guidance to the Universities Project. The ROJECT P continuing counsel of the Project’s Advisory Committee has been absolutely crucial to the success of our work, as has been the support of many other individuals who have become active participants of the Project. We believe it is fair to say that, over time, the Project has become one of the most active and effective interfaces between North American and European university leaders, not only as a neutral interface, but as an active advocate of transatlantic mutual learning and understanding. The Salzburg Seminar will continue to provide a meeting place where leaders in higher education can meet, exchange views, and share experiences.