Avgas Vs. Mogas in Light-Sport Aircraft
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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. -
FLASHBLACK Instruction Manual
Instruction manual Variable pitch propellers in flight FLASHBLACK FLASHBLACK Tractor Pusher BLACK Tractor Aérodrome de Villefranche Tarare (LFHV) 289 Avenue Odette & Edouard DURAND 69620 FRONTENAS - FRANCE Phone: + 33 (0)4 74 72 12 69 - Fax: +33 (0)4 74 72 10 01 ISO 9001:2015 Certified Company E-mail: [email protected] - www.DUC-helices.com for its Quality System Management DH_FSH-PV_BE_02_F Made in France 04/12/2018 Revision update Date Index Object of modification 23/07/2014 A Creation 20/07/2017 F Add SWIRLBLACK-3 & TBO update 11/12/2017 F Minor correction 10/04/2018 F English language correction 04/12/2018 F Minor change in page 42 This instruction manual is to be maintained throughout the life of the propeller. He may have to evolve. The owner must check with the DUC Hélices Company the latest version being valid applicable to the propeller. Identification Date Delivery note n° Engine/Gearbox Owner ratio Aircraft Pitch range Min: Max: Notes: .............................................................................................................................................................................. .......................................................................................................................................................................................... .......................................................................................................................................................................................... ......................................................................................................................................................................................... -
Looking After Your Rotax 912 Series Engine
LOOKING AFTER YOUR ROTAX 912 SERIES ENGINE Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale Copyright ConAir Sports Ltd. All rights reserved. Page 1 of 20 Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale This article has been written by Conrad Beale of ConAir Sports Ltd. It is intended to help you look after your 912 series engine. It is in no way endorsed by Rotax. All information contained here in may be subject to change without notice. It does not substitute, override or in any way replace the information given in the Installation / Maintenance or Operators Manuals or any subsequent documentation issued by Rotax. The intention of this article is to assist the many Rotax 4 stroke engine owners, operators and engineers to carry out the work necessary to prolong the life of their Rotax 912/914 series aircraft engines. This article will touch on a number of subjects and will hopefully clear up some of the common questions we get asked. Some areas will be covered in detail, others less so. I hope it covers everything sufficiently. I have been involved with Rotax engines for 25+ years, 18 of which have been working commercially on Rotax aircraft engines. 8 years ago I set up ConAir Sports Ltd with my wife Louise and we are the only UK Skydrive appointed Service Centre for Rotax Aircraft Engines. -
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. -
ENGINE TYPE 914 | 115 Hp (UL/F) AIRCRAFT ENGINES
ENGINE TYPE 914 | 115 hp (UL/F) AIRCRAFT ENGINES DESCRIPTION • 4-cylinder • 4-stroke liquid/air-cooled engine with opposed cylinders • with turbo charger • with automatic waste gate control • dry sump forced lubrication with separate oil tank • automatic adjustment by hydraulic valve tappet • 2 carburetors • dual electronic ignition • electric starter • propeller speed reduction unit • engine mount assembly • air intake system • exhaust system FACTS The turbo charged Rotax 914 series offers more performance at high altitudes while keeping weight at a low level. This series offers a time between overhauls of 2.000 hrs and is available as certified (Rotax 914 F) according to FAR 33 and JAR-E and non-certified version (Rotax 914 UL). ENGINE DATA WEIGHT kg lb engine with propeller speed reduction unit i = 2,43 64.0 140.8 exhaust system 4.0 8.8 engine suspension frame 2.0 3.7 overload clutch 1.7 3.7 external alternator 3.0 6.6 air guide hood 0.8 1.8 VERSION PERFORMANCE TORQUE MAX RPM kW ft. lb. 1/min Nm ft. lb. 1/min 1/min 914 UL1)/F2) 84.5 115 5800 144 106 4900 5800 Limited for max. 5 min. BORE STROKE DISPLACEMENT FUEL min. MON 85 RON 95* 79.5 mm 3.13 in 61 mm 2.4 in 1211.2 cm3 73.91 cu. in. min. AKI 91* * leaded or unleaded or AVGAS 100LL 1) UL = non certified 2) F = certified acc. to ARF 33 and JAR-E Picture: 914 UL - DCDI with options WWW.FLYROTAX.COM ® and TM are trademarks of BRP-Rotax GmbH & Co. -
Rotax Service Interval Guide Not New News, but a Very Informative Summary
Rotax Service Interval Guide Not new news, but a very informative summary With growing numbers of 912 & 914 series engines in service these days Rotax have gathered a great deal of field experience and have been continually updating the maintenance procedures. Operators of 912 & 914 series engines can obtain current maintenance manuals free of charge, (yep I did say FREE) from the Rotax aircraft engines web site www.rotax-aircraft-engines.com – just click on the documentation tab & fill in the relevant search boxes to obtain the documents you require. You will find parts lists, line & heavy maintenance manuals, service bulletins, operator’s manuals, installation manuals, and a whole host of information you may not have known about. The system is not perfect, for example parts lists for early engines are not available, but it is pretty good & full of useful documentation. We do find that some Rotax owners find the documentation difficult to interpret and occasionally miss things - agreed it can be difficult to see the wood through the trees, especially after translation. As the maintenance & overhaul information has changed over the last couple of years it’s probably a good time to have a recap on how things are now. So before the flying season gets too busy why not take the opportunity to make sure your engine is ready for the new flying season – I’m assured its going to be a good one this year! Figure 1: Documentation page of the Rotax Aircraft Engines website (www.rotax-aircraft-engines.com) MAINTENANCE SCHEDULES The alterations to the maintenance schedules over the years have mainly been to reduce the work required and the parts replaced, so should you want to save a few pennies in these difficult times you better read on. -
Carburetor Synchronization
Carburetor Synchronization With the proliferation of the Rotax 912 80 hp and the Rotax 912S 100 hp engines, the topic of carburetor synchronization has come to the forefront. Until about the 1980s, the popularity of Continental and Lycoming engines dominated the general aviation market, these engines used a single carburetor providing for a single source of air and fuel to the cylinders. The use of dual carburetors was primarily relegated to the area of the two-stroke ultralight market. And, even with these engines, the process of carburetor synchronization was quite simple and reliable. How- ever, with the popularity of the Rotax 9 series engines, it has become import- ant to under- stand a little bit more about how the induc- tion system works on this amazing little powerhouse. This understand- ing is important not only from a maintenance standpoint, but from a pilot’s per- spective as well. The Rotax 912 is essentially two engines connected to a single crankshaft and gearbox with both Figure: 1 The Rotax 912 is two separate engines connected to a common crankshaft the left and right sides of the engine having their own independent carburetor, ignition, and exhaust sys- tem Figure: 1. As you might well imagine, having two engines trying to run a single propeller requires a bit of choreography between the right and left side of the en- gine in order to make things run smoothly. Most of us, who have spent a consider- able amount of time in the air, can remember a time when one of the cylinders on a four-cylinder engine just quit firing, maybe from fouled spark plugs, or a plugged fuel Figure: 2 Clamping off the crossover (Balance) hose injector. -
The Drive to Outperform
2018 ANNUAL REVIEW FOR THE YEAR ENDED JANUARY 31, 2018 THE DRIVE TO OUTPERFORM FINANCIAL HIGHLIGHTS FISCAL YEAR 2018 REVENUE BASE REVENUE BASE BY CATEGORY BY REGION AT 31/01/18 AT 31/01/18 40.8% 34.8% 15.7% 8.7% 50.5% 32.2% 17.3% YEAR-ROUND SEASONAL PARTS, ACCESSORIES PROPULSION UNITED STATES INTERNATIONAL CANADA PRODUCTS PRODUCTS AND CLOTHING SYSTEMS SHARE PRICE MONTHLY CLOSING PRICE IN CA$ $50.86 JANUARY 2018 $26.03 FEBRUARY 2017 MARCH APRIL MAY JUNE JULY AUGUST SEPTEMBER OCTOBER NOVEMBER DECEMBER TOTAL NORMALIZED NORMALIZED RESEARCH AND REVENUES EBITDA1 EARNINGS PER DEVELOPMENT CA$ MILLIONS, CA$ MILLIONS, SHARE – DILUTED1 SPENDING AT 31/01/18 AT 31/01/18 CA$, AT 31/01/18 IN CA$ MILLIONS + AS A % OF REVENUES CAGR* 9% CAGR* 10% CAGR* 12% 3,194 3,525 3,829 4,172 4,487 380.2 421.3 460.0 502.7 558.6 1.49 1.65 1.71 1.96 2.38 145 + 4% 158 + 4% 164 + 4% 184 + 4% 199 + 4% 14 15 16 17 18 14 15 16 17 18 14 15 16 17 18 14 15 16 17 18 1 See Non-IFRS measures section on p.15. * Compound Annual Growth Rate since 31 January 2014 LETTER TO SHAREHOLDERS FOR FISCAL YEAR 2018 – JOSÉ BOISJOLI THE DRIVE TO OUTPERFORM I am very pleased with the strong financial results we delivered once again, featuring another year of record revenues, continuing our steady positive performance since we became a public company five years ago. We are now three years into our ambitious 2020 plan and remain focused on our strategic priorities of Growth, Agility and Lean enterprise to reach our target: the $6 billion mark and $3.50 diluted earnings per share by fiscal year 2021. -
Flying Efficiently
MIKE BUSCH COMMENTARY / SAVVY AVIATOR A GPS-coupled fuel totalizer (like this Shadin Digifl o that I have in my airplane) is a great help in achieving Flying maximum effi ciency. Efficiently It’s more important than ever to get the best bang for the buck HOW CAN WE GET THE BEST FUEL economy from our airplanes? Given much energy as possible from each combus- the painful cost of avgas these days, this question is on lots of airplane tion event before the exhaust valve opens and owners’ minds. That goes at least double for unfortunate folks like me discards what’s left. and Mac McClellan who fl y twins. It’s a subject I’ve thought about— Operating at WOT and low rpm will make and researched—quite a bit. some pilots uncomfortable, because they had a It turns out that there are lots of pieces to this puzzle. There are all fl ight instructor who taught them never to sorts of things we can do to optimize effi ciency. Some are simple; some operate the engine oversquare—that is, with are a bit more complex. It takes considerable attention to detail to fl y manifold pressure (in inches) greater than the as effi ciently as possible. rpm (divided by 100). This is exactly what I was taught by my primary instructor in 1965, THROTTLE and it took me more than a decade to fi gure Let’s start with something simple: throttle position. out that my CFI didn’t know what the heck he Our piston aircraft engines are always most effi cient at wide-open was talking about.