Master IA Refresher Course Data Base Current As of January 16, 2018
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Fiber Optic (Flight Quality) Sensors for Advanced Aircraft Propulsion
/ .. < / • _7 _ NASA Contractor Report 191195 ? R94AEB175 Fiber Optic (Flight Quality) Sensors For Advanced Aircraft Propulsion Final Report Gary L. Poppel GE Aircraft Engines Cincinnati, Ohio 45215 July 1994 Prepared for: Robert J. Baumbick, Project Manager National Aeronautics and Space Administration 2 I000 Brookpark Road Cleveland, Ohio 44135 Contract NAS3-25805 N94-37401 (NASA-CR-I9II95) FISER OPTIC (FLIGHT QUALITY) SENSORS FOR NationalAeronauticsand ADVANCED AIRCRAFT PROPULSION Fina] Uncl as Space Administration Report, Jan. 1990 - Jun. 1994 (GE) 90 p G3/06 0016023 TABLE OF CONTENTS Section Page 1.0 SUMMARY 2.0 INTRODUCTION 3.0 SENSOR SET DESCRIPTION 3.1 Identification and Requirements 3.2 Engine/System Schematics 3.3 F404 Implementation 3.4 Optical/Electrical Signal Comparison 9 4.0 SENSOR DESIGN, FUNCTIONALITY, & TESTING 9 4.1 TI Temperature Sensor 4.2 T2.5 Temperature Sensor I0 11 4.3 T5 Temperature Sensor 4.4 FVG Position Sensor 12 14 4.5 CVG Position Sensor 4.6 VEN Position Sensor 15 16 4.7 NL Speed Sensor 17 4.8 Nil Speed Sensor 4.9 AB Flame Detector 18 20 5.0 ELECTRO-OPTIC CIRCUITRY 5.1 Litton EOA Circuitry 20 23 5.2 GE Circuitry 24 5.3 Conax T5 Signal Processor 5.4 Ametek AB Flame Detector Assembly 25 26 6.0 ELECTRO-OPTICS UNIT DESIGN, ASSEMBLY, & TESTING 26 6.1 Chassis Design 26 6.2 Assembly Process 6.3 Internal Features 26 27 6.4 Input/Output Interfaces 6.5 Thermal Studies 27 27 6.6 Testing 7.0 CABLE DESIGN & FABRICATION 33 7.1 Identification of Cable Set 33 33 7.2 Optical Sensor Loop Configurations 7.3 GE-Designed Fiber -
MANUAL Kohler 1000 DIESEL Kohler 750 EFI Intimidator 800
2017 OWNER’S MANUAL Kohler 1000 DIESEL Kohler 750 EFI Intimidator 800 UTVRevised 10/18/2017 Owner Memo Name: ____________________________________ Purchasing Date: ____________________________ Type: _____________________________________ Pin Number: _______________________________ Special Notice: _____________________________ Key Number: _______________________________ PAGE 2 OWNER’S MANUAL Table of Contents: Title ........................... Page Number Introduction ......................................................Page 4 Definitions ........................................................Page 4 Safety Labels ...............................................Pages 4-8 ROPS Inspection Guide .............................Pages 9-10 General Safety ..........................................Pages 11-14 Safe Riding Gear .............................................Page 15 Features, Controls and Operation ............Pages 16-33 New Vehicle Break-in ......................................Page 33 Service and Maintenance .........................Pages 34-71 Storing and Maintaining Appearance .......Pages 72-73 Transporting your Intimidator .........................Page 74 Accessories ....................................................Page 74 Specifications ......................................... Pages 75-83 Troubleshooting ...................................... Pages 84-89 Warranties .............................................. Pages 90-99 Service Record .................................... Pages 100-101 Training Certificate ........................................Page -
Sae 2019-01-0249
Downloaded from SAE International by John Kargul, Friday, May 29, 2020 2019-01-0249 Published 02 Apr 2019 Benchmarking a 2018 Toyota Camry 2.5-Liter INTERNATIONAL. Atkinson Cycle Engine with Cooled-EGR John Kargul, Mark Stuhldreher, Daniel Barba, Charles Schenk, Stanislav Bohac, Joseph McDonald, and Paul Dekraker US Environmental Protection Agency Josh Alden Southwest Research Institute Citation: Kargul, J., Stuhldreher, M., Barba, D., Schenk, C. et al., “Benchmarking a 2018 Toyota Camry 2.5-Liter Atkinson Cycle Engine with Cooled-EGR,” SAE Int. J. Advances & Curr. Prac. in Mobility 1(2):601-638, 2019, doi:10.4271/2019-01-0249. This article was presented at WCXTM19, Detroit, MI, April 9-11, 2019. Abstract idle, low, medium, and high load engine operation. Motoring s part of the U.S. Environmental Protection Agency’s torque, wide open throttle (WOT) torque and fuel consumption (EPA’s) continuing assessment of advanced light-duty are measured during transient operation using both EPA Tier Aautomotive technologies in support of regulatory and 2 and Tier 3 test fuels. Te design and performance of this 2018 compliance programs, a 2018 Toyota Camry A25A-FKS 2.5-liter engine is described and compared to Toyota’s published 4-cylinder, 2.5-liter, naturally aspirated, Atkinson Cycle engine data and to EPA’s previous projections of the efciency of an with cooled exhaust gas recirculation (cEGR) was bench- Atkinson Cycle engine with cEGR. The Brake Thermal marked. Te engine was tested on an engine dynamometer Efciency (BTE) map for the Toyota A25A-FKS engine shows with and without its 8-speed automatic transmission, and with a peak efciency near 40 percent, which is the highest value of the engine wiring harness tethered to a complete vehicle parked any publicly available map for a non-hybrid production gasoline outside of the test cell. -
Save a Turbine Engine: Serve It Water
Clare Leavens Award Joe Chase Award Aviall High Achievement Award Transport Canada Approved for R/T Save a turbine engine: serve it water Minimum equipment lists and dispatch deviation guides PAMA and AME news February -March 2015 Volume 13/Issue 5 Publication Mail Agreement No. 0041039024 and Return Undeliverable Canadian Addresses to Alpha Publishing Group (2004) Inc. Unit 7, 11771 Horseshoe Way, Richmond, BC, V7A 4V4 email: [email protected] $7.95 AMU-OFC-IFC.indd 1 1/29/15 7:28 PM AMU-OFC-IFC.indd 2 1/29/15 7:28 PM In perspective: Departments the P&WC PT6 nd here some of you thought Gran- 4 Upcoming Events dad put a lot of miles and years on his good ol’ Harley Flathead 45. Hah! 6 STCs & New Products AThat was nothing. Pratt & Whitney Canada 8 Industry Forum recently tweeted out that its venerable PT6 turbine has now clocked 400 million hours 20 AME Association of flight operation. and PAMA News Four hundred million! What does that 39 Classified even mean? Let’s calculate (roughly): There are 8,760 hours in any 365-day year. Di- 42 AMU Chronicles vide 400 million by 8,760 and you get By Sam Longo 45,662.100456621. Round that number off — without fac- toring in Leap, Aztec or dog years (this is al- Features ready getting too complicated for my lousy math)—and you’re now standing at 46,000 10 subscribe and download at www.amumagazine.com AMU is viewable online: years of service. Did I just do that right? As- Save a Turbine Engine: Serve it Water 10 suming I did (and that’s a big ask, I know) By Mike Broderick then we can break down that history into bite-sized pieces. -
Technical Addendum to the Guidance for Noise Screening of Air Traffic Actions
MP130001 MITRE PRODUCT Technical Addendum to the Guidance for Noise Screening of Air Traffic Actions Koffi A. Amefia February 2013 The contents of this material reflect the views of the author and/or the Director of the Center for Advanced Aviation System Development (CAASD), and do not necessarily reflect the views of the Federal Aviation Administration (FAA) or the Department of Transportation (DOT). Neither the FAA nor the DOT makes any warranty or guarantee, or promise, expressed or implied, concerning the content or accuracy of the views expressed herein. This is the copyright work of The MITRE Corporation and was produced for the U.S. Government under Contract Number DTFAWA-10-C-00080 and is subject to Federal Aviation Administration Acquisition Management System Clause 3.5-13, Rights in Data-General, Alt. III and Alt. IV (Oct. 1996). No other use other than that granted to the U.S. Government, or to those acting on behalf of the U.S. Government, under that Clause is authorized without the express written permission of The MITRE Corporation. For further information, please contact The MITRE Corporation, Contract Office, 7515 Colshire Drive, McLean, VA 22102 (703) 983-6000. 2013 The MITRE Corporation. The Government retains a nonexclusive, royalty-free right to publish or reproduce this document, or to allow others to do so, for “Government Purposes Only.” MP130001 MITRE PRODUCT Technical Addendum to the Guidance for Noise Screening of Air Traffic Actions Sponsor: The Federal Aviation Administration Koffi A. Amefia Dept. No.: F072 Project No.: 0213BB03-2B Outcome No.: 3 PBWP Reference: 3-2.1-2 February 2013 “Wind Farm and Environmental Assessment Processes” For Release to all FAA This document was prepared for authorized distribution only. -
Los Motores Aeroespaciales, A-Z
Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales. -
2017 SUN Baseline Noise Modeling Memo
To: CHRIS POMEROY, FRIEDMAN MEMORIAL AIRPORT From: Chris Sandfoss Cc: Rob Adams Date: 3/1/2017 Re: SUN Noise Modeling Methodology and Preliminary Results This memo summarizes the basic input data for, and the preliminary results of, the noise modeling of existing (2017) baseline conditions at Friedman Memorial Airport (SUN). Noise contours have been be prepared using the AEDT at levels of DNL 65, 70, and 75. The following sections describe the input data and results of the noise contour modeling. NOISE MODELING METHODOLOGY Number of Operations and Fleet Mix: The number of annual operations that were modeled for the existing (2017) conditions at SUN is based on a variety of sources, including ATCT operations counts, Airport landing fee reports, and FAA Aviation System Performance Metrics (ASPM) databases. There were 25,316 total operations at SUN from January 2016 through December 2016, which corresponds to 69.4 average-annual day operations. Table 1 provides a summary of the average daily operations and fleet mix at SUN, organized by aircraft type, operation type, and time of day. Several aircraft types use the same FAA-approved substitute in the noise database of the AEDT as indicated by the noise model ID in Table 1. Daytime/Nighttime Operations: Data on the ratio of daytime to nighttime operations is based on data from the Draft Environmental Impact Statement (DEIS) and data from FMAA staff. Approximately 98 percent of all operations occur during the daytime (7:00 am to 9:59 pm) and 2 percent of all operations occur during the nighttime (10:00 pm to 6:59 am). -
Service Specifications Service Data
EG1–77 ENGINE – ENGINE MECHANICAL SERVICE SPECIFICATIONS SERVICE DATA Compression STD pressure Limit Difference between each cylinder Cylinder head Head surface warpage Limit Manifold surface warpage Limit Valve seat Refacing angle Intake Exhaust Contacting angle Contacting width Valve guide Inner diameter Intake bushing Exhaust Outer diameter STD O/S 0.05 Replacing temperature (cylinder head side) Valve Valve overall length STD Intake Exhaust Valve face angle Stem diameter STD Intake Exhaust Stem end refacing Limit Stem oil clearance STD STD Intake Exhaust Limit Intake Exhaust Valve head edge thickness STD Limit Valve spring Free length Installed load at 40.5 mm (1.594 in.) STD Limit Squareness Limit Rocker arm Rocker arm inside diameter and shaft Rocker shaft diameter Shaft to arm oil clearance STD Limit Intake, exhaust Manifold surface warpage manifolds and Limit Intake air intake chamber Exhaust Air intake chamber Chain and Crankshaft sprocket wear Limit sprocket Camshaft sprocket wear Limit EG1–78 ENGINE – ENGINE MECHANICAL Tension and Tensioner head thickness Limit damper No. 1 damper wear Limit No. 2 damper wear Limit Camshaft Thrust clearance STD Limit Journal oil clearance STD Limit Journal diameter STD Circle runout Limit Cam height STD Intake Exhaust Limit Intake Exhaust Cylinder block Cylinder head surface warpage Cylinder bore STD Cylinder bore wear Limit Cylinder block main journal bore STD Piston and Piston diameter STD piston ring Piston to cylinder clearance Ring to ring groove clearance STD Limit Piston ring end gap -
Operator's Manual
OPERATOR'S MANUAL L 3 2 4 0 á L 3 TRACTOR 5 4 0 MODELS L3240áL3540áL3940 á L L4240áL4740áL5040 3 9 L5240áL5740 4 0 á L 4 2 4 0 á L 4 7 4 0 á L 5 0 4 0 á L 5 2 4 0 á L 5 English (Australia) 7 Code No. TD170-1974-2 4 0 PRINTED IN JAPAN ABBREVIATION LIST Abbreviations Definitions 2WD Two Wheel Drive 4WD Four Wheel Drive API American Petroleum Institute ASAE American Society of Agricultural Engineers, USA ASTM American Society for Testing and Materials, USA DIN Deutsches Institut für Normung, GERMANY DT Dual Traction z4WDx fpm Feet Per Minute GST Glide Shift Transmission Hi-Lo High Speed-Low Speed HST Hydrostatic Transmission m/s Meters Per Second PTO Power Take Off RH/LH Right-hand and left-hand sides are determined by facing in the direction of forward travel ROPS Roll-Over Protective Structures rpm Revolutions Per Minute r/s Revolutions Per Second SAE Society of Automotive Engineers, USA SMV Slow Moving Vehicle ABBREVIATION LIST Abbreviations Definitions 2WD Two Wheel Drive 4WD Four Wheel Drive API American Petroleum Institute ASAE American Society of Agricultural Engineers, USA ASTM American Society for Testing and Materials, USA DIN Deutsches Institut für Normung, GERMANY DT Dual Traction z4WDx fpm Feet Per Minute GST Glide Shift Transmission Hi-Lo High Speed-Low Speed HST Hydrostatic Transmission m/s Meters Per Second PTO Power Take Off RH/LH Right-hand and left-hand sides are determined by facing in the direction of forward travel ROPS Roll-Over Protective Structures rpm Revolutions Per Minute r/s Revolutions Per Second SAE Society of Automotive Engineers, USA SMV Slow Moving Vehicle UNIVERSAL SYMBOLS As a guide to the operation of your tractor, various universal symbols have been utilized on the instruments and controls. -
Sw24/Sw28 St35/St45
Operator's Manual Compact loaders SW24/SW28 ST35/ST45 Machine type S04-01/S04-02/S04-03/S04-04 Edition 1.7 Order no 5200022252 Language us 5200022252 Dokumentationen Documentations Language Order no. Documentations Language Order no. Operator's Manual [us] 5200022252 SW24 [de en fr] 1000323666 ST35 [de en fr] 1000323692 SW24 [it es en] 1000323669 ST35 [it es en] 1000323693 Spare parts list Spare parts list SW28 [de en fr] 1000323670 ST45 [de en fr] 1000323865 SW28 [it es en] 1000323691 ST45 [it es en] 1000323870 Legend Original Operator‘s Manual x Translation of original Operator‘s – Manual Edition 1.7 Date 05/2016 Document 5200022252_1_7 Copyright © 2015 Wacker Neuson Baumaschinen GmbH, Hörsching Printed in Austria. All rights reserved, in particular the globally applicable copyright, right of reproduction and right of distribution. No part of this publication may be reproduced, translated or used in any form or by any means – graphic, electronic or mechanical including photocopying, recording, taping or information storage or retrieval systems – without prior permission in writing from the manufacturer. No reproduction or translation of this publication, in whole or part, without the written consent of Wacker Neuson Linz GmbH. Violations of legal regulations, in particular of the copyright protection, will be subject to civil and criminal prosecution. Wacker Neuson Linz GmbH keep abreast of the latest technical developments and constantly improve their products. For this reason, we may from time to time need to make changes to diagrams and descriptions in this documentation which do not reflect products which have already been delivered and which will not be implemented on these machines. -
Textron: Action & Results
130124 5/14/03 2:16 PM Page FC1 Textron: Action & Results 2002 Fact Book 130124 5/14/03 2:16 PM Page IFC2 Textron is an $11 billion multi-industry company with approximately 49,000 employees in 40 countries. We leverage our global network of businesses to provide customers with innovative solutions and services in industries such as aircraft, fastening systems, industrial products and components, and finance. Textron is known around the world for its powerful brands, such as Bell Helicopter, Cessna Aircraft, Kautex, Lycoming, E-Z-GO and Greenlee, among others. Stock and Contact Information Stock Exchange Listings General Information Ticker Symbol – TXT This Fact Book is one of several sources of information available to Textron Inc. shareholders and the investment community. To receive Annual Common Stock Reports, 10-K, 10-Q reports and/or press releases, please call (888) TXT- New York, Chicago and Pacific Stock Exchanges LINE or visit our website at www.textron.com Preferred Stock ($2.08 and $1.40) New York Stock Exchange Contacts Investors Mandatorily Redeemable Preferred Securities of Subsidiary Trust (7.92%) Douglas R. Wilburne New York Stock Exchange Vice President, Communications & Investor Relations [email protected] Capital Stock (401) 457-2353 (as of December 28, 2002) (401) 457-3598 (fax) Common stock: par value $0.125; 500,000,000 shares authorized; Marc Kaplan 136,499,608 shares outstanding. Director, Investor Relations $2.08 Cumulative Convertible Preferred stock, Series A: [email protected] 120,515 shares outstanding. (401) 457-2502 (401) 457-3598 (fax) $1.40 Convertible Preferred Dividend stock, Series B: 56,394 shares outstanding. -
Woodside Aircraft Noise Monitoring
Woodside Aircraft Noise Monitoring Prepared by San Francisco International Airport Aircraft Noise Abatement Office Technical Report #042017-969 1st Quarter 2017 April 2017 San Francisco International Airport Woodside Aircraft Noise Monitoring Report Page | 2 Table of Contents Executive Summary ................................................................................................................................ 3 Community and SFO Operations............................................................................................................ 3 Equipment ............................................................................................................................................... 3 Aircraft Noise Analysis........................................................................................................................... 4 Aircraft Operations ................................................................................................................................. 6 SFO Aircraft Noise Event Flights by Altitude ........................................................................................ 8 Conclusion .............................................................................................................................................. 9 Figure 1 – Woodside Portable Noise Monitoring Comparison Table .................................................. 11 Figure 2 – Microphone mounted on tripod and Monitor at the Woodside VOR and Monitoring Location #969 at Woodside (blue zone) ..............................................................................................