Aviation Gasolines and Future Alternatives
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UAT-ARC Final Report
Unleaded AVGAS Transition Aviation Rulemaking Committee FAA UAT ARC Final Report Part I Body Unleaded AVGAS Findings & Recommendations 17 February 2012 UAT ARC Final Report – Part I Body February 17, 2012 Table of Contents List of Figures …………………………………………………………………………… 6 Executive Summary……………………………………………………………………… 8 1. Background …………………..……………………………………………………. 11 1.1. Value of General Aviation………………………………………………… 11 1.2. History of Leaded Aviation Gasoline…………………………………….. 13 1.3. Drivers for Development of Unleaded Aviation Gasoline……………… 14 2. UAT ARC Committee ……………………………………………………………… 16 2.1. FAA Charter……………………………………………………………….. 16 2.2. Membership ………………..…………………………………………….. 17 2.3. Meetings, Telecons, & Deliberations…………….……………………… 17 3. UAT ARC Assessment of Key Issues…………………………………………… 18 3.1. Summary of Key Issues Affecting Development & Transition to an Unleaded AVGAS…………………………………………………………….. 18 3.1.1. General Issues……………………………………………………… 18 3.1.2. Market & Economic Issues………………………………………… 18 3.1.3. Certification & Qualification Issues……………………………….. 18 3.1.4. Aircraft & Engine Technical Issues………………………………. 19 3.1.5. Production & Distribution Issues………………………………….. 19 3.1.6. Environment & Toxicology Issues………………………………… 19 3.2. General Issues – Will Not Be A Drop-In…………………………….……. 20 3.2.1. Drop-In vs. Transparent……………..……………………………. 20 3.2.2. Historic Efforts Focused on Drop-In…………………………….. 21 3.2.3. No Program to Support Development of AVGAS………………. 21 3.3. Market & Economic Issues…………………….. …………………………. 22 3.3.1. Market Forces……………………………………………………… 22 3.3.2. Aircraft Owner Market Perspective……………………………….. 23 3.3.3. Fleet Utilization …………..…………………………………………. 24 3.3.4. Design Approval Holder (DAH) Perspective ……………………. 25 3.4. Certification & Qualification Issues…………………………………………. 26 3.4.1. FAA Regulatory Structure…….……………………………………. 26 3.4.2. ASTM and FAA Data Requirements………………..……………. 27 3.4.3. FAA Certification Offices…………………………………………… 28 3.4.4. -
General Aviation Aircraft Propulsion: Power and Energy Requirements
UNCLASSIFIED General Aviation Aircraft Propulsion: Power and Energy Requirements • Tim Watkins • BEng MRAeS MSFTE • Instructor and Flight Test Engineer • QinetiQ – Empire Test Pilots’ School • Boscombe Down QINETIQ/EMEA/EO/CP191341 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Contents • Benefits of electrifying GA aircraft propulsion • A review of the underlying physics • GA Aircraft power requirements • A brief look at electrifying different GA aircraft types • Relationship between battery specific energy and range • Conclusions 2 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Benefits of electrifying GA aircraft propulsion • Environmental: – Greatly reduced aircraft emissions at the point of use – Reduced use of fossil fuels – Reduced noise • Cost: – Electric aircraft are forecast to be much cheaper to operate – Even with increased acquisition cost (due to batteries), whole-life cost will be reduced dramatically – Large reduction in light aircraft operating costs (e.g. for pilot training) – Potential to re-invigorate the GA sector • Opportunities: – Makes highly distributed propulsion possible – Makes hybrid propulsion possible – Key to new designs for emerging urban air mobility and eVTOL sectors 3 RAeS Light Aircraft Design Conference | 18 Nov 2019 | © QinetiQ UNCLASSIFIED UNCLASSIFIED Energy conversion efficiency Brushless electric motor and controller: • Conversion efficiency ~ 95% for motor, ~ 90% for controller • Variable pitch propeller efficiency -
Motor Gasolines Technical Review Motor Gasolines Technical Review Chevron Products Company
fold Motor Gasolines Technical Review Motor Gasolines Technical Review Technical Gasolines Motor Chevron Products Company Products Chevron Chevron Products Company 6001 Bollinger Canyon Road San Ramon, CA 94583 www.chevron.com/products/ourfuels/prodserv/fuels/ technical_safety_bulletins/ Chevron Products Company is a division of a wholly owned subsidiary of Chevron Corporation. © 2009 Chevron Corporation. All rights reserved. Chevron is a trademark of Chevron Corporation. Recycled/RecyclableRecycled/recyclable paper paper 10M IDC 69083 06/09 MS-9889 (06-09) center The products and processes referred to in this document are trademarks, registered trademarks, or service marks of their respective companies or markholders. Motor Gasolines Technical Review Written, edited, and designed by employees and contractors of Chevron Corporation: Lew Gibbs, Bob Anderson, Kevin Barnes, Greg Engeler, John Freel, Jerry Horn, Mike Ingham, David Kohler, David Lesnini, Rory MacArthur, Mieke Mortier, Dick Peyla, Brian Taniguchi, Andrea Tiedemann, Steve Welstand, David Bernhardt, Karilyn Collini, Andrea Farr, Jacqueline Jones, John Lind, and Claire Tom. Chapter 5 prepared by Jack Benson of AFE Consulting Services. Motor Gasolines Technical Review (FTR-1) © 2009 Chevron Corporation. All rights reserved. center The products and processes referred to in this document are trademarks, registered trademarks, or service marks of their respective companies or markholders. Motor Gasolines Technical Review Written, edited, and designed by employees and contractors of Chevron Corporation: Lew Gibbs, Bob Anderson, Kevin Barnes, Greg Engeler, John Freel, Jerry Horn, Mike Ingham, David Kohler, David Lesnini, Rory MacArthur, Mieke Mortier, Dick Peyla, Brian Taniguchi, Andrea Tiedemann, Steve Welstand, David Bernhardt, Karilyn Collini, Andrea Farr, Jacqueline Jones, John Lind, and Claire Tom. -
(12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz Et Al
USOO88695 04B1 (12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz et al. (45) Date of Patent: Oct. 28, 2014 (54) GEAREDTURBOFAN ENGINE GEARBOX 5.431,539 A 7/1995 Carvalho ARRANGEMENT 5,443,365 A * 8/1995 Ingling et al. ............. 416, 193A 5,778,659 A 7/1998 Duesler et al. 6,464,401 B1 10/2002 Allard (71) Applicant: United Technologies Corporation, 7,144.221 B2 * 12/2006 Giffin ............................ 416,189 Hartford, CT (US) 8,137,070 B2 * 3/2012 Van Houten ... 416,189 2006.0024162 A1* 2, 2006 Giffin .......... ... 415,208.3 (72) Inventors: Frederick M. Schwarz, Glastonbury, 2007/015.1258 A1* 7/2007 Gaines et al. ................... 60,792 CT (US); William G. Sheridan, 2008/00987.17 A1* 5, 2008 Orlando et al. .... ... 60,226.1 Southington, CT (US) 2010/0218478 A1* 9/2010 Merry et al. .................... 60,205 glon, 2011/0056208 A1 3/2011 Norris et al. .................... 6Of772 2011/O123326 A1 5/2011 DiBenedetto et al. (73) Assignee: United Technologies Corporation, 2012/0110979 A1* 5, 2012 Rosenkrans et al. ......... 60,226.1 Hartford, CT (US) 2012fO251306 A1* 10/2012 Reinhardt et al. ......... 415, 1821 2012fO263579 A1* 10, 2012 Otto et al. .......... ... 415,124.2 (*) Notice: Subject to any disclaimer, the term of this 2012/0291449 A1* 11/2012 Adams et al. ................... 60,793 2012/03 15130 A1 12/2012 Hasel et al. patent is extended or adjusted under 35 2013, OO25257 A1 1/2013 Suciu et all U.S.C. 154(b) by 0 days. 2013/0025258 A1* 1/2013 Merry et al. -
9914 the Manufacturability of the Rotapower® Engine
9914 The Manufacturability of the Rotapower® Engine Paul S. Moller, Ph.D. Freedom Motors Freedom Motors 1855 N 1st St., Suite B Dixon, CA 95620 www.freedom-motors.com All rights reserved. © 2018. No part of this publication may be reproduc ed, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, and recording or otherwise without the prior written permission of the authors. 9914 The Manufacturability of the Rotapower® Engine Paul S. Moller, Ph.D. Freedom Motors ABSTRACT introduced their rotary powered Evinrude RC-35-Q and Johnson Phantom snowmobiles. There are many elements of the charge cooled Wankel type rotary engine that make it inexpensive OMC also investigated liquid cooled housing marine to produce. OMC was able to show that they could models. OMC’s four rotor outboards raced six produce this type of engine at a cost competitive times in the summer and fall of 1973, winning every with their carbureted two-stroke engines. race in U class (unlimited). At the Galveston Speed Classic, they placed 1 st, 2nd and 3rd, lapping the THE PRODUCTION CHARGE COOLED WANKEL entire field three times (a fourth OMC boat rolled). WAS FIRST INTRODUCED AS A POTENTIALLY It was rumored that they once made a straightaway CLEAN, LOW COST, POWERFUL REPLACEMENT pass at 165 mph. FOR TW O-STROKES. THE CHARGE-COOLED ROTOR WANKEL TYPE In the late 60’s Outboard Marine Corporation ENGINE HAS A LOW PART COUNT (OMC) recognized the market value of an advanced, more powerful engine. This interest was When choosing an engine for a particular intensified by a growing concern that emission application or comparing the part count between issues would necessitate a clean burning, engines, the required power and torque environmentally friendly powerplant. -
Numerical Analysis on Combustion Characteristic of Leaf Spring Rotary Engine
Energies 2015, 8, 8086-8109; doi:10.3390/en8088086 OPEN ACCESS energies ISSN 1996-1073 www.mdpi.com/journal/energies Article Numerical Analysis on Combustion Characteristic of Leaf Spring Rotary Engine Yan Zhang, Zhengxing Zuo and Jinxiang Liu * School of Mechanical Engineering, Beijing Institute of Technology, Beijing 100081, China; E-Mails: [email protected] (Y.Z.); [email protected] (Z.Z.) * Author to whom correspondence should be addressed; E-Mail: [email protected]; Tel./Fax: +86-10-6891-1392. Academic Editors: Paul Stewart and Chris Bingham Received: 19 March 2015 / Accepted: 17 July 2015 / Published: 4 August 2015 Abstract: The purpose of this paper is to investigate combustion characteristics for rotary engine via numerical studies. A 3D numerical model was developed to study the influence of several operative parameters on combustion characteristics. A novel rotary engine called, “Leaf Spring Rotary Engine”, was used to illustrate the structure and principle of the engine. The aims are to (1) improve the understanding of combustion process, and (2) quantify the influence of rotational speed, excess air ratio, initial pressure and temperature on combustion characteristics. The chamber space changed with crankshaft rotation. Due to the complexity of chamber volume, an equivalent modeling method was presented to simulate the chamber space variation. The numerical simulations were performed by solving the incompressible, multiphase Unsteady Reynolds-Averaged Navier–Stokes Equations via the commercial code FLUENT using a transport equation-based combustion model; a realizable turbulence model and finite-rate/eddy-dissipation model were used to account for the effect of local factors on the combustion characteristics. -
550 Series Avgas Engine
The 550 series includes 550 in3 models in either naturally aspirated or turbocharged configurations. With the right combination of thrust and efficiency, our 550-series engines are powering some of the most successful and high performing aircraft in general aviation history like the Cirrus® SR22T and Beechcraft® Baron/Bonanza, and Mooney®. With a powerful range of 280 to 350 HP at 2500 to 2700 RPM, you’ll be glad you fly a 550. THE 550 SERIES IS A FAMILY CERTIFIED FUELS: STROKE: TYPICAL WEIGHT: 100/100LL & 94UL 107.95 mm 207 to 317 kg OF AIR COOLED, NATURALLY AvGas (TSIO-550-K only) 4.25 in 456 to 699 lbs ASPIRATED, HORIZONTALLY DISPLACEMENT: COMPRESSION TIME BETWEEN OPPOSED, 6-CYLINDER, 9046 cm³ (COMP.) RATIO: OVERHAUL (TBO): 552 in3 7.5:1 1800 – 2200 hours GASOLINE, FUEL INJECTED, SPARK 8.5:1 IGNITION, FOUR-STROKE, DIRECT POWER: TURBO MODEL 209 to 261 kW HEIGHT: AVAILABILITY: DRIVE, RIGHT (CW) ROTATING, 280 to 350 HP 501.7 to 933.2 mm Yes AIRCRAFT ENGINE WITH MANUAL 19.75 to 36.74 in MAXIMUM ENGINE CONTROLS FOR FIXED RATED RPM: WIDTH: 2500 to 2700 r/min 852.4 to 1076.7 mm WING AIRCRAFT. THE TURBO 2500 to 2700 rpm 33.56 to 42.39 in SERIES IS TURBOCHARGED FOR BORE: LENGTH: FIXED WING AIRCRAFT. 133.35 mm 933.2 to 1215.6 mm 5.25 in 36.74 to 47.86 in WWW.CONTINENTAL.AERO # RATED DRY CERTIFIED COMP. TIME BETWEEN FAA MODEL 1 BORE × STROKE DISPLACEMENT 2 FUEL OVERHAUL CYL POWER WEIGHT GRADE RATIO (TBO) TCDS 224 kW @ 2700 133.35 x 107.95 mm 9046 cm³ 206.8 kg IO-550-A 6 100/ 100LL 8.5:1 1900 hours E3SO 300 HP @ 2700 5.25 x 4.25 in 552 in³ 455.9 -
Comments of the General Aviation Avgas Coalition
COMMENTS OF THE GENERAL AVIATION AVGAS COALITION ON THE ADVANCE NOTICE OF PROPOSED RULEMAKING ON LEAD EMISSIONS FROM PISTON-ENGINE AIRCRAFT USING LEADED AVIATION GASOLINE EPA DOCKET NO. EPA–HQ–OAR–2007–0294 - 1 - I. INTRODUCTION On April 28, 2010, the Environmental Protection Agency (“EPA”) published in the Federal Register an “Advance Notice of Proposed Rulemaking on Lead Emissions from Piston- Engine Aircraft Using Leaded Aviation Gasoline” (the “ANPR”). 75 Fed. Reg. 22440. The General Aviation AvGas Coalition (the “Coalition”) respectfully submits the following comments on the ANPR. The Coalition is comprised of associations that represent industries, businesses, and individuals that would be directly impacted by any finding made by the EPA in regard to lead emissions from piston-engine aircraft, corresponding aircraft emissions standards, and related changes to the formulation of aviation gasoline. Coalition membership includes the Aircraft Owners and Pilots Association (“AOPA”), the Experimental Aircraft Association (“EAA”), the General Aviation Manufacturers Association (“GAMA”), the National Air Transportation Association (“NATA”), the National Business Aviation Association (“NBAA”), the American Petroleum Institute (“API”) and the National Petrochemical and Refiners Association (“NPRA”). Together, these organizations represent general aviation aircraft owners, operators, and manufacturers, and the producers, refiners, and distributors of aviation gasoline. 1 Since the establishment of the first National Ambient Air Quality Standard (“NAAQS”) for lead in 1978, the general aviation and petroleum industries have been committed to safely reducing lead emissions from piston powered aircraft. Today, 100 octane low lead (“100LL”) aviation gasoline (or “avgas”) contains 50 percent less lead than it did when the lead NAAQS were first introduced, dramatically reducing lead emissions from general aviation. -
Anteproyecto De Una Aeronave
CENTRO UNIVERSITARIO DE LA DEFENSA ACADEMIA GENERAL DEL AIRE ANTEPROYECTO DE UNA AERONAVE AERONAVE DE ENTRENAMIENTO AVANZADO Trabajo Fin de Grado Autor: A. A. D. Rafael Ángel Reyes Rodríguez (LXVI – CGEA-EOF) Director: José Serna Serrano Co-director: Francisco Javier Sánchez Velasco Grado en Ingeniería en Organización industrial Curso: 2014/2015 – convocatoria: junio Tribunal nombrado por la dirección del Centro Universitario de la Defensa de San Javier, el día ____ de ____________ de 20____. Presidente: Dr. D. Manuel Caravaca Garratón Secretario: Dr. D. Alejandro López Belchí Vocal: Col. Dr. Andrés Dolón Payán Realizado el acto de defensa del Trabajo Fin de Grado, el día____ de _________ de 20____, en el Centro Universitario de la Defensa de San Javier. Calificación: __________________________. EL PRESIDENTE EL SECRETARIO EL VOCAL ANTEPROYECTO DE UNA AERONAVE AERONAVE DE ENTRENAMIENTO AVANZADO RESUMEN: Este trabajo trata de plasmar en su desarrollo el anteproyecto de una hipotética aeronave de entrenamiento avanzado. En él se busca encontrar una solución de compromiso al estado del arte actual, a partir del cálculo de los parámetros definitorios básicos de dicha aeronave, incluida la polar del avión. Para ello se acude a las referencias señaladas en busca de las herramientas necesarias para el establecimiento de los valores aerodinámicos y motrices deseados. Como producto final se obtiene un compendio de constantes que nos permite evaluar las características diferenciadoras de la aeronave con las ya existentes. ABSTRACT: This work tries to develop a conceptual advanced jet trainer design for a hypothetical aircraft. It seeks to find a compromise solution to the current state of the art, from the calculation of the basic parameters defining the aircraft, including polar aircraft. -
Replacing Gasoline: Alternative Fuels for Light-Duty Vehicles
Executive Summary OVERVIEW als requirements, feedstock requirements, and so forth. The variety of effects, coupled with the Recent interest in alternative fuels for light-duty existence of the three separate “policy drivers” for highway vehicles (automobiles and light trucks) is introducing alternative fuels, create a complex set of based on their potential to address three important trade-offs for policymakers to weigh. Further, there societal problems: unhealthy levels of ozone in are temporal trade-offs: decisions made now about major urban areas; growing U.S. dependence on promoting short-term fuel options will affect the imported petroleum; and rising emissions of carbon range of options open to future policymakers, e.g., dioxide and other greenhouse gases. This assess- by emplacing new infrastructure that is more or less ment examines the following alternative fuels: adaptable to future fuel options, or by easing methanol, ethanol, natural gas (in either compressed pressure on oil markets and reducing pressure for (CNG) or liquid (LNG) form), electricity (to drive development of nonfossil alternative fuels. Table 1 electric vehicles (EVs)), hydrogen, and reformulated presents some of the trade-offs among the alternative gasoline. fuels relative to gasoline. Substituting another fuel for gasoline affects the Much is known about these fuels from their use in entire fuel cycle, with impacts not only on vehicular commerce and some vehicular experience. Much performance but on fuel handling and safety, materi- remains to be learned, however, especially about Photo credtt General Motors Corp. GM’s Impact electric vehicle, though a prototype requiring much additional testing and development, represents a promising direction for alternative fuel vehicles: a “ground up,” innovative design focused on the unique requirements of the fuel sources, in this case electricity. -
An Experimental Study of a Hydrogen-Enriched Ethanol Fueled Wankel Rotary Engine at Ultra Lean and Full Load Conditions ⇑ F
Energy Conversion and Management 123 (2016) 174–184 Contents lists available at ScienceDirect Energy Conversion and Management journal homepage: www.elsevier.com/locate/enconman An experimental study of a hydrogen-enriched ethanol fueled Wankel rotary engine at ultra lean and full load conditions ⇑ F. Amrouche a, , P.A. Erickson b, S. Varnhagen b, J.W. Park b a Centre de Développement des Énergies Renouvelables, CDER, 16340 Algiers, Algeria b Mechanical and Aerospace Engineering Department, UC Davis, CA 95616, USA article info abstract Article history: In this paper, the effect of hydrogen addition to ethanol in a monorotor Wankel engine at wide open Received 29 March 2016 throttle position and in an ultra-lean operating regime was experimentally investigated. For this aim, Received in revised form 20 May 2016 variation of hydrogen enrichment levels on the ethanol engine performance and emissions were consid- Accepted 12 June 2016 ered. Experiments were carried out under a constant engine speed of 3000 rpm and fixed spark timing of Available online 18 June 2016 15 °BTDC. The test results showed that hydrogen enrichment improved the combustion process through shortening of the flame development and flame propagation periods and reducing the cyclic variation. Keywords: Furthermore, the reduction of burn duration with the increase of hydrogen fraction enhances the thermal Wankel rotary engine efficiency, reducing the brake-specific energy consumption, as well as reducing the unburned hydrocar- Hydrogen enriched ethanol Ultra-lean burn bons emissions of the Wankel engine. Engine economy Ó 2016 Elsevier Ltd. All rights reserved. Unburned hydrocarbons emissions 1. Introduction new generation of rotary engines. -
Biogas Technology
FOOD AND AGRICULTURE ORGANIZATION OF THE UNITED NATIONS SUPPORT FOR DEVELOPMENT OF NATIONAL BIOGAS PROGRAMME (FAO/TCP/NEP/4451-T) BIOGAS TECHNOLOGY: A TRAINING MANUAL FOR EXTENSION NEPAL September 1996 Consolidated Management Services Nepal (P) Ltd. CMS House, Lazimpat, GPO Box # 10872, Kathmandu, Nepal Tel # (977-1 ) 410 498/421 654, Fax # (977-1) 415 886 E-mail : [email protected] FOOD AND AGRICULTURE ORGANIZATION OF THE UNITED NATIONS SUPPORT FOR DEVELOPMENT OF NATIONAL BIOGAS PROGRAMME (FAO/TCP/NEP/4451-T) BIOGAS TECHNOLOGY: A TRAINING MANUAL FOR EXTENSION NEPAL September 1996 Consolidated Management Services Nepal (P) Ltd. CMS House, Lazimpat, GPO Box # 10872, Kathmandu, Nepal Tel # (977-1 ) 410 498/421 654, Fax # (977-1) 415 886 E-mail : [email protected] FAO/TCP/NEP/4415-T Consolidated Management Services Nepal PREFACE Biogas has proved to be a viable technology in the physical and socio-economic conditions of Nepal. The hydropower generating potential of Nepal is calculated as one of the highest in the world but only about 12 percent of the population is connected to the national electricity grid. The percapita energy consumption is one of the lowest in the world and more than 90 percent of the energy use is in the domestic sector, mainly for cooking. Nepal's agrarian economy is fully dependent on imports for all of its chemical fertilizer, petroleum and coal requirements. The growing population and small scale industries are pushing the use of traditional sources of energy (forest and agricultural waste) beyond the sustainable generation capacity of the existing forest and farm lands.