DOCSLIB.ORG

Turbonycoil 600 Is Approved for Use on General Electric GE90 Engine Family

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Turbonycoil 600 Is Approved for Use on General Electric GE90 Engine Family PRESS RELEASE For immediate release Turbonycoil 600 is approved for use on General Electric GE90 engine family Paris, June 19th, 2019: NYCO announces that General Electric recently approved Turbonycoil® 600, a synthetic standard turbine oil, for use in General Electric GE90 engine which was specifically designed for the Boeing 777 aircraft. Its 115 000 lbs thrust version is the world’s most powerful turbofan engine. This qualification enables NYCO to increase its support for mixed fleet airlines. Boeing 777 © Air France “This qualification confirms NYCO’s growing position in the civil aviation market by allowing it to reach the majority of mixed fleet airlines worldwide”, said Guillaume Forestier, NYCO Director - Aeronautics & Defence Division. “We strive to provide our customers the most advanced technologies and the most exhaustive range of products for all fleets.” A service evaluation on a few GE90 engines following the manufacturer’s procedures was led in collaboration with Air France. Air France’s fleet includes 70 Boeing 777 and already uses Turbonycoil 600 on all its Airbus A320 & A340 aircraft. “The success of the turbine oil evaluation on some of our Boeing 777 engines shows that the product meets all the GE9O’s operation requirements. This allows us to contemplate a smooth transition on the Boeing fleet comparable to the one experienced on the Airbus fleet. The relationship established between our companies, since the beginning of the project, leads us to believe in a long-term collaboration with NYCO.” Said Didier Verté, Engine Fleets and Engineering Vice President at Air France Industries. Approved against demanding specifications, including SAE AS5780 SPC Class and MIL-PRF-23699 F STD Class, Turbonycoil® 600 is approved by all major engine manufacturers (General Electric, Pratt & Whitney, Pratt & Whitney Canada, Rolls-Royce, Snecma, Turbomeca, CFMI, Klimov, Motor Sich, Aviadvigatel). It has logged more than 30 years of experience in jet engines of military and commercial aircraft. NYCO, 66 avenue des Champs-Élysées, BP 414 75366 Paris Cedex 08 - France Tel : +33 1 45 61 50 00 – [email protected] - www.nyco-group.com PRESS RELEASE About NYCO NYCO is a French company, expert in the development and manufacture of high performance lubricants and synthetic ester bases for Aeronautics, Defence and Industry. A key partner for Armed Forces, Airlines, OEMs, MROs and Aero derivative Gas Turbines users around the world, NYCO offers a comprehensive products range approved to the most demanding civil and military specifications. Our international network of subsidiaries, distributors and agents has enabled us to expand our presence in more than 100 countries around the world with more than 80% of our export sales. For more information: www.nyco-group.com Contact Anna PATIN [email protected] +33 6 43 74 33 14 NYCO, 66 avenue des Champs-Élysées, BP 414 75366 Paris Cedex 08 - France Tel : +33 1 45 61 50 00 – [email protected] - www.nyco-group.com .
Load more

Recommended publications
  • Large Composite Fan Blade Development for Modern Aeroengines
    Volume I: Composites Applications and Design LARGE COMPOSITE FAN BLADE DEVELOPMENT FOR MODERN AEROENGINES Keith T. Kedward University of California at Santa Barbara Department of Mechanical & Environmental Engineering Santa Barbara, California 93106-5070, USA SUMMARY: The state of maturity of contemporary PMC’s after almost 30 years of scientific and technology development has resulted in a capability that far exceeds that available in the late 1960’s, and which, in 1989, prompted General Electric to engage in the notably successful development and flight certification of large PMC fan blades for their GE90 engine. In this paper an accounting of the specific enhancements in (i) constituent (fiber and matrix) property characteristics, (ii) fabrication and processing options, and (iii) design analysis methods combined with computational capabilities will be discussed. However, an equally important aspect is the variation in the design options that has resulted from evolving high by-pass ratio engine technology, which will also be addressed. The GE90 fan blade represents one of these options, being a relatively large blade designed to operate at lower tip speeds, thereby reducing the severity of the impact threat represented by the ingestion of large birds. A comparison between various modern turbofan engine fan blades and other rotor blades serves to indicate the important parameters and the difficulty of establishing a composite threshold range for rotor blades in general. KEYWORDS: polymer matrix composite, composite fan blade, constituent properties, impact performance, textile reinforcement architectures, engine certification INTRODUCTION Since the ill-fated attempt by Rolls-Royce to develop large polymer matrix composite (PMC) fan blades for a large commercial turbofan engine in 1968, i.e., the RB211, this potential application had eluded the engine designer until the emergence of General Electric’s GE90 engine development.
    [Show full text]
  • An Investigation in Gold-Plating Scaled Turbofan Engine Simulators
    An Investigation in Gold-Plating Scaled Turbofan Engine Simulators through Means of Aerodynamic and Load Cell Thrust Measurements with Comparisons to Full-Scale Engine Results A Thesis Presented in Partial Fulfillment of the Requirements for the Degree of Master of Science in the Graduate School of The Ohio State University By Jacob T. Allenstein, B. Sci. Graduate Program in Aeronautical and Astronautical Engineering The Ohio State University 2013 Thesis Committee: Dr. Richard J. Freuler, Advisor Dr. Clifford A. Whitfield, Co-Advisor Copyright by Jacob T. Allenstein © 2013 ABSTRACT Model testing offers investigators a useful tool that can provide good insight into the aerodynamics behind full-scale engines and test facilities. Understanding the aerodynamics of a full-scale engine can help investigators update old test facilities and help design new facilities and engines. Gold-plating an engine is a process that the industry uses to compare the performance of an engine from the same family or class of engines in various facilities. The gold-plated engine can be used to determine a correlation factor of a testing facility or to determine the similarities in performance between a new or old engine to the gold-plated engine. The use of a correlation or correction factor can be used to correct a deviation in a measurement made in a test facility to bring the engine’s performance back to readings performed in a “free-air” environment. Model testing consists of the use of a simulator or scaled version of an engine that generates performance close to full-scale operation conditions. The simulator used in this study was constructed to not have any moving parts but rather be driven by a high pressure air system, providing a safe alternative to testing the full-scale engine.
    [Show full text]
  • ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics
    National Research University Higher School of Economics Institute for Statistical Studies and Economics of Knowledge Big Data Augmented Horizon Scanning: Combination of Quantitative and Qualitative Methods for Strategic and Marketing Analytics [email protected] [email protected] XIX April International Academic Conference on Economic and Social Development Moscow, 11 April 2018 Outline - Role of artificial intelligence and big data in modern analytics - System of Intelligent Foresight Analytics iFORA - Combined quantitative and qualitative analysis methodology and software solutions - Use cases - Conclusion and discussion 2 Growing interest in Artificial Intelligence, Big Data and Machine Learning International analytical reports & news feed 12000 10000 8000 Artificial Intelligence 6000 Big Data Machine Learning 4000 2000 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 Russian analytical reports & news feed 800 700 600 500 Artificial Intelligence 400 Big Data 300 Machine Learning 200 100 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 3 Source: System of Intelligent Foresight Analytics iFORA™ (ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics AI-related tasks Tracking latest and challenges trends, technologies, drivers, barriers Market forecasting Trend analysis Understanding S&T modern skills and Instruments for Customers Market Intelligence competences analysis feedback knowledge discovery HR policy Vacancy Feedback mining
    [Show full text]
  • Rolls-Royce Trent
    Rolls-Royce Trent Rolls-Royce Trent 900 on A380 prototype Rolls Royce Trent is a family of high-bypass turbofan engines manufactured by Rolls-Royce. All are developments of the famous RB211 with thrust ratings spanning between 53,000 to 95,000 lbf (236 to 423 kN). The name has also been used for a number of previous designs. Earlier designations The first Trent - a Rolls-Royce RB.50 Trent on a test rig at Hucknall, in March 1945 "Trent" was the name originally given by Rolls-Royce to the world's first turboprop engine (right). It was based on a concept provided by Sir Frank Whittle and derived by mating a five-bladed propeller driven through a reduction gearbox onto the company's Derwent II turbojet. It first flew on an experimental Gloster Meteor aircraft in the middle 1940s. The designation was reused again in the 1960s for the RB203 bypass turbofan which was designed to replace the Spey. It was the first three-spool engine, forerunner of the RB211 series. It was rated at 9980 lbf (44.4 kN). Present designation The current Trent is the development of the three-shaft RB211 family of engines. By 1987, a variant of the RB211, the RB211-524L, had been developed to such an extent that it bore little resemblance to the original RB211, other than the three-shaft layout. Rolls-Royce decided that the 524L would be the basis of a new engine family, and so the newest Trent was born. Rolls-Royce had started naming their engines after British rivers in 1942—a practice which was revived for the Trent after a 30-year gap.
    [Show full text]
  • The Market for Aviation Turbofan Engines
    The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7
    [Show full text]
  • Aviation Magazine – Index Général Simplifié @ Dominique Mahieu (2010)
    Aviation Magazine – Index Général Simplifié @ Dominique Mahieu (2010) / www.aero-index.com Numéro 101 du 01/07/1954 Mémoires d’Adolf Galland Les leçons de Dien Bien Phu Les erreurs de pilotage (J. Lecarme) Le GC 1/1 Corse Meetings de l’entre deux guerre La kermesse de Toussus-le-Noble Le SE Aquilon Air-Tourist Numéro 102 du 15/07/1954 Mémoires d’Adolf Galland J’ai piloté le Caproni F.5 De France en Angleterre le Hurel Dubois 31 50 ans d’aviation à Coventry Paris-Biarritz : première course vélivole par étapes Le Piel CP-30 Emeraude Vickers Viscount d’Air France Championnats du monde de vol à voile à Camp Hill Numéro 103 du 01/08/1954 Mémoires d’Adolf Galland J’ai piloté le Miles Aries Ecole complète du vol à voile : Saint-Auban L’Aéronautique navale au Tonkin Le Marcel Brochet MB-100 L’Aéro-club Paul-Tissandier Numéro 104 du 15/08/1954 Mémoires d’Adolf Galland Le meeting de Nice en 1922 L’invitation polonaise (festival international de vol à voile) Championnat du monde de vol à voile (Gérard Pierre champion du monde 1954) Les avions d’entraînement de l’OTAN à Villacoublay Le De Havilland Canada DHC-3 Otter Numéro 105 du 01/09/1954 Mémoires d’Adolf Galland Les meetings de Vincennes Classiques ou laminaires Saint-Yan : victoire éclatante des soviétiques (championnats du monde de parachutisme) Le Breguet 901 L’Aéro-club Jean Réginensi Numéro 106 du 15/09/1954 Mémoires d’Adolf Galland Le turbopropulseur Napier Eland Le Tour de France aérien 1954 L’Avro Canada CF-100 L’Aéro-club Jean Maridor Numéro 107 du 01/10/1954 Mémoires d’Adolf Galland Farnborough 1954 Numéro 108 du 15/10/1954 Mémoires d’Adolf Galland Farnborough 1954 Le colonel Cressaty Opération Shooting Star (exercice aérien) Le porte-avions « Ville de Paris » Le Pasotti Airone F.6 Numéro 109 du 01/11/1954 Mémoires d’Adolf Galland J’ai essayé le Pasotti F.6 Airone Les décrochages (J.
    [Show full text]
  • Pdf, Accessed June 1, 2009
    THE “APOLLO” OF AERONAUTICS Copyright © 2010 by the National Aeronautics and Space Administration The opinions expressed in this volume are those of the authors and do not necessarily reflect the official position of the United States Government or of the National Aeronautics and Space Administration. THE “APOLLO” OF AERONAUTICS NASA’s Aircraft Energy Efficiency Program 1973–1987 MARK D. BOWLES National Aeronautics and Space Administration Headquarters 300 E St SW Washington, DC 20546 2010 SP-2009-574 www.nasa.gov About the Cover: Front cover: NASA Langley Research Center’s Boeing 737 test aircraft on the ramp at Orlando International Airport after a day of flight tests. (NASA Langley Research Center [NASA LaRC].) Cover design by Janine Wise. Library of Congress Cataloging-in-Publication Data Bowles, Mark D. The “Apollo” of aeronautics : NASA’s Aircraft Energy Efficiency Program, 1973-1987 / Mark D. Bowles. p. cm. Includes bibliographical references and index. 1. Aircraft Energy Efficiency Program (U.S.)--History. 2. Airplanes--Fuel consumption- -Research--United States--History--20th century. 3. Aerodynamics--Research--United States--History--20th century. 4. Jet engines--Research--United States--History--20th century. I. Title. TL704.7.B634 2009 629.134’35--dc22 2009046465 For Nancy, Isabelle, Emma, and Sarah Table of Contents Introduction ..............................................................................ix Chapter 1: Oil as a Weapon ........................................................................1 Chapter 2: Threads
    [Show full text]
  • National Air & Space Museum Technical Reference Files: Propulsion
    National Air & Space Museum Technical Reference Files: Propulsion NASM Staff 2017 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Scope and Contents........................................................................................................ 1 Accessories...................................................................................................................... 1 Engines............................................................................................................................ 1 Propellers ........................................................................................................................ 2 Space Propulsion ............................................................................................................ 2 Container Listing ............................................................................................................. 3 Series B3: Propulsion: Accessories, by Manufacturer............................................. 3 Series B4: Propulsion: Accessories, General........................................................ 47 Series B: Propulsion: Engines, by Manufacturer.................................................... 71 Series B2: Propulsion: Engines, General............................................................
    [Show full text]
  • High Capacity Short Range Transport Aircraft Final Design Report
    High Capacity Short Range Transport Aircraft Final Design Report By: Connor Flanagan, Luke DiStasio, Omar Abed, Mitchell Foster, Eitan Ghelman, Jeffrey Hernandez, Hamid Nazemi, Eric Richter, Abdulrahman Shuraym May 14, 2020 Condor Aviation Design Team Omar Abed Luke DiStasio Connor Flanagan CAD Aerodynamics, Materials, Subsystems AIAA 937419 Structures AIAA 1097608 AIAA 1098428 Mitchell Foster Eitan Ghelman Jeffrey Hernandez Cost, Business Case Business Case Propulsion, Performance AIAA 1097599 AIAA 1098432 AIAA 1097601 Hamid Nazemi Eric Richter Abdulrahman Shuraym CAD, Configuration Sizing, Performance, Performance, Stability Selection CG/Stability AIAA 933856 AIAA 1098044 AIAA 1097607 ii Condor Aviation Advisors Neil Weston Carl Johnson Faculty Advisor Faculty Advisor iii Contents List of Figures .............................................................................................................................................. vi List of Tables ................................................................................................................................................ x List of Abbreviations ................................................................................................................................... xi Introduction ................................................................................................................................................... 1 Design Process .............................................................................................................................................
    [Show full text]
  • Dynamic Modeling and Simulation on GE90 Engine
    The International Journal Of Engineering And Science (IJES) || Volume || 5 || Issue || 12 || Pages || PP 111-119 || 2016 || ISSN (e): 2319 – 1813 ISSN (p): 2319 – 1805 Dynamic Modeling and Simulation on GE90 Engine Shray Benawra & Jiqiang Wang Jiangsu Province Key Laboratory of Aerospace Power System Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China --------------------------------------------------------ABSTRACT----------------------------------------------------------- The paper talks about a better numerical method for predicting on-design performance on a High-Bypass Turbofan engine GE90. A dynamic optimization turbofan engine for GE90 has been designed using MATLAB/Simulink software. Individual components including Ambient, Fan, Low Pressure Compressor (LPC), High Pressure Compressor (HPC), Combustion Chamber, High Pressure Turbine (HPT), Low Pressure Turbine (LPT), Exit Nozzle and Plenum volumes, Makes a combination to identify the performance characteristics of a turbofan engine throughout the flight condition. The specific engine characteristics are matched and adopted through the use of variables from developed a model. The results will validate through simulation with the software to look through for problems and understand the air flow from the intake to the nozzle. Good designs can intensify a better performance to the engine, which performance analysis can be applied and tested to each component of the GE90 engine during design point condition. Keywords: Dynamic Turbofan; GE90; Design Point; Modeling
    [Show full text]
  • =British Airways Plc (BA) Is the Flag Carrier Airline of the United
    =British Airways plc (BA) is the flag carrier airline of the United Kingdom which is based and headquartered in Waterside, near its main hub at London Heathrow Airport. British Airways operates a second hub at Gatwick Airport and a third hub, served through its fully owned subsidiary, BA CityFlyer, at London City Airport. British Airways is the largest airline in the UK based on fleet size, international flights and international destinations. BA's UK passengers originating at non-London airports must connect via London after British Airways discontinued all direct overseas flights from UK airports outside London following the sale of BA Connect to British regional carrier Flybe in 2007. The British Airways Board was established in 1971 to control the two nationalised airline corporations, BOAC and BEA, and two much smaller regional airlines, Cambrian Airways from Cardiff and Northeast Airlines from Newcastle upon Tyne. On 31 March 1974 all four companies were dissolved to form British Airways (BA). After almost 13 years as a nationalised company, British Airways was privatised in February 1987 as part of the privatisation plan by the Conservative Government of the time. The carrier soon expanded with the acquisition of British Caledonian (BCAL) in 1987 and Gatwick-based carrier Dan-Air in 1992. Despite being a longtime Boeing customer, British Airways placed a major order for Airbus aircraft in August 1998 with the purchase of 59 Airbus A320 family aircraft. In 2007, the carrier placed its next major order, marking the start of its long-haul fleet replacement, ordering 12 Airbus A380s and 24 Boeing 787s.
    [Show full text]
  • Delta Virtual Airlines Boeing 777-200Er Aircraft Operating Manual
    DELTA VIRTUAL AIRLINES BOEING 777-200ER AIRCRAFT OPERATING MANUAL THIRD EDITION NOVEMBER 2005 TABLE OF CONTENTS Table of Contents ......................................................................................................2 Aircraft History and Background .................................................................................1 Engine Types.............................................................................................................3 Rolls-Royce Trent 800 ............................................................................................3 General Electric GE90.............................................................................................3 Pratt & Whitney PW4090 ........................................................................................4 Flight Deck................................................................................................................5 Aircraft Specifications.................................................................................................7 Aircraft Dimensions ................................................................................................7 Design Weights......................................................................................................7 Capacity ................................................................................................................7 Power Plants..........................................................................................................7 Field Lengths .........................................................................................................8
    [Show full text]