Factory New Certified & Experimental Aircraft Engines
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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. -
IN the UNITED STATES DISTRICT COURT for the EASTERN DISTRICT of PENNSYLVANIA CHARLES POWERS, on His Own : CIVIL ACTION Behalf An
Case 2:06-cv-02993-TJS Document 152 Filed 02/09/11 Page 1 of 31 IN THE UNITED STATES DISTRICT COURT FOR THE EASTERN DISTRICT OF PENNSYLVANIA CHARLES POWERS, on his own : CIVIL ACTION behalf and on behalf of the : class defined herein : NO. 06-2993 : v. : : LYCOMING ENGINES, a Division of : AVCO CORPORATION; AVCO : CORPORATION; and TEXTRON, INC. : PLANE TIME, LLC, on its own behalf and : CIVIL ACTION on behalf of others similarly situated : : NO. 06-4228 v. : : LYCOMING ENGINES, a Division of : AVCO CORPORATION; AVCO : CORPORATION; and TEXTRON, INC. : MEMORANDUM OPINION Savage, J. February 9, 2011 In these two consolidated putative nationwide class actions, we conduct a choice-of- law analysis and then re-evaluation of whether the plaintiffs have satisfied Rule 23's requirements for class certification. Moving for class certification under Fed. R. Civ. P. 23(b)(3), the plaintiffs seek to represent a class of owners or previous owners of aircraft equipped with engines designed and built by Lycoming Engines.1 They claim that the engines were manufactured with defective crankshafts that can cause a total loss of engine power and in-flight engine 1 The plaintiffs named three defendants, Lycoming Engines, Avco Corporation (“Avco”) and Textron, Inc. Since the motion for certification was filed, Textron has been dismissed. The two remaining defendants are referred to collectively as “Lycoming.” Case 2:06-cv-02993-TJS Document 152 Filed 02/09/11 Page 2 of 31 failures, and that Lycoming knew of and concealed the defect that prevents the crankshafts from functioning as intended. They seek damages for the cost to replace the defective crankshafts, which includes parts, labor, transportation, storage, insurance, the loss of the use of the aircraft while the crankshafts are being replaced and the diminished value of the aircraft. -
ATP® Libraries Catalog
2 ATP® Libraries Catalog Revision Date May 24 2016 ATP 101 South Hill Drive Brisbane, CA 94005 (+1) 415-330-9500 www.atp.com ATP® Policies and Legal www.atp.com/policy © Copyright 2016, ATP. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form by any means, electronic, mechanical, photocopying, recording or otherwise, without prior written permission of ATP. The information in this catalog is subject to change without notice.ATP, ATP Knowledge, ATP Aviation Hub, HubConnect, NavigatorV, and their respective logos, are among the registered trademarks or trademarks of ATP. All third-party trademarks used herein are the property of their respective owners and ATP asserts no ownership rights to these items. iPad and iPhone are trademarks of Apple Inc., registered in the U.S. and other countries. App Store is a service mark of Apple Inc. All original authorship of ATP is protected under U.S. and foreign copyrights and is subject to written license agreements between ATP and its subscribers. Visit www.atp.com/policy for more information ATP Customer Support Please visit www.atp.com/support for customer support information ATP® Libraries Catalog – Revision Date: May 24 2016 3 CONTENTS CONTENTS ...................................................................................................................................................................... 3 REGULATORY LIBRARIES ............................................................................................................................................. -
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. -
Lycoming Engine Development, June 1963
VOLUME 1, NU BER 3 JUNE, 1963 B. H. WARREN NOW VICE PRESIDENT, GENERAL MANAGER--------------------------- The appointment of Beverly H. Warren as vice president and general manager of Lycoming Division has been announced by James R. Kerr, president and cbief operating officer of AVCO Corporation. General Warren has been vice president of AVCO's Defense and Industrial Products Group since April, 1961, and director of its Operational Missiles Subdivision since September, 1960. He is a veteran of more than 25 years service with the U.S. Air Force, and retired in 1960 with the rank of Major General. In other organizational changes, General Warren announced the appointment of Dr. Anselm Franz as vice president and general manager, gas turbines, and of Paul A. Deegan as director of administration. Dr. Franz in turn announced that Dr. Heinrich Adenstedt bas been named to the position of vice president, gas turbines operations. LYCOMING SALES DEPARTMENT ACTIVE------------------------------------------- Sales promotion efforts during the Summer will be centered on demonstrations of the Bell 2u4B, commercial version of the Army's Iroquois helicopter, and sales proposals for Lycoming's T55 turboprop and turbofan engines to potential users in Europe, Canada, and the United States. The Bell 204B helicopter is owered by the 1100 shaft horsepower Lycoming T5309 gas turbine engine which differs from the T53-L-9 military engine only in the use of fireproof fuel and oil lines. Two aircraft will make three month demonstration tours, one heading West, the other East. Customers will be invited to demonstrations by the Bell Helicopter egional sales manager in their area, who will be assisted by Bob McCalpin of Lycoming's sales staff. -
2014 FACT BOOK Textron Inc
2014 FACT BOOK Textron Inc. is a $13.9 billion multi-industry company with approximately 34,000 employees. The company leverages its global network of aircraft, defense and intelligence, industrial and finance businesses to provide customers with innovative solutions and services. Textron is known around the world for its powerful brands such as Beechcraft, Bell Helicopter, Cessna, E-Z-GO, Greenlee, Hawker, Jacobsen, Kautex, Lycoming, Textron Systems, Textron Financial Corporation and TRU Simulation + Training. KEY EXECUTIVES SCOTT C. DONNELLY FRANK T. CONNOR Scott C. Donnelly was named chief Frank T. Connor joined Textron as executive executive officer in December 2009 and vice president and chief financial officer in chairman of the board in September 2010. August 2009. Connor came to Textron after Donnelly joined Textron as executive vice a 22-year career at Goldman, Sachs & Co. president and chief operating officer in where he was most recently managing June 2008 and was promoted to president director and head of Telecom Investment in January 2009. Prior to joining Textron, Banking. Prior to that, he served as Donnelly was president and CEO for Goldman, Sachs & Co.’s chief operating General Electric (GE) Aviation. officer of Telecom, Technology and Media Scott C. Donnelly Frank T. Connor Investment Banking. Chairman, President and Executive Vice President Chief Executive Officer and Chief Financial Officer Scott A. Ernest John L. Garrison Jr. Ellen M. Lord J. Scott Hall R. Danny Maldonado Textron Aviation Bell Helicopter Textron Systems Segment Industrial Segment Finance Segment President and CEO President and CEO President and CEO President and CEO President and CEO Revenue by Segment Revenue by Customer Type Revenue by Geography Textron Aviation 33% Commercial 65% U.S. -
Rules and Regulations Federal Register Vol
31111 Rules and Regulations Federal Register Vol. 67, No. 90 Thursday, May 9, 2002 This section of the FEDERAL REGISTER Attn: Data Distribution, M/S 64–3/2101– above, the FAA has determined that air contains regulatory documents having general 201, P.O. Box 29003, Phoenix, AZ safety and the public interest require the applicability and legal effect, most of which 85038–9003; telephone: (602) 365–2493; adoption of the rule as proposed. are keyed to and codified in the Code of fax: (602) 365–5577. This information Economic Analysis Federal Regulations, which is published under may be examined, by appointment, at 50 titles pursuant to 44 U.S.C. 1510. the Federal Aviation Administration The FAA estimates that there are The Code of Federal Regulations is sold by (FAA), New England Region, Office of approximately 300 Lycoming former the Superintendent of Documents. Prices of the Regional Counsel, 12 New England military T53 series turboshaft engines new books are listed in the first FEDERAL Executive Park, Burlington, MA; or at installed on helicopters of U.S. registry, REGISTER issue of each week. the Office of the Federal Register, 800 that would be affected by this AD. The North Capitol Street, NW, suite 700, FAA also estimates that it would take Washington, DC. approximately 8 work hours per engine DEPARTMENT OF TRANSPORTATION FOR FURTHER INFORMATION CONTACT: to accomplish an initial or repetitive inspection of the centrifugal compressor Federal Aviation Administration Robert Baitoo, Aerospace Engineer, Los Angeles Aircraft Certification Office, impeller, and that the average labor rate is $60 per work hour.