Tribology for Aerospace Systems (La Tribologie Pour Les Systemes Aerospatiaux)

Total Page:16

File Type:pdf, Size:1020Kb

Tribology for Aerospace Systems (La Tribologie Pour Les Systemes Aerospatiaux) AGARD-CP-589 0) 00 10 CL Ü i Q AC < ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT S 7 RUE ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE AGARD CONFERENCE PROCEEDINGS 589 Tribology for Aerospace Systems (la Tribologie pour les systemes aerospatiaux) Papers presented at the 82nd Meeting of the AGARD Structures and Materials Panel, held in Sesimbra, Portugal, 6-7 May 1996. Mm m ® NORTH ATLANTIC TREATY ORGANIZATION Published October 1996 Distribution and Availability on Back Cover THIS DOCUMENT IS BEST QUALITY AVAILABLE. THE COPY FURNISHED TO DTIC CONTAINED A SIGNIFICANT NUMBER OF PAGES WHICH DO NOT REPRODUCE LEGIBLY. AGARD-CP-589 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE AGARD CONFERENCE PROCEEDINGS 589 Tribology for Aerospace Systems (la Tribologie pour les systemes aerospatiaux) Papers presented at the 82nd Meeting of the AGARD Structures and Materials Panel, held in Sesimbra, Portugal, 6-7 May 1996. .BASEMENT K j Approved tor ijäustie rsieaa« ) WTC QUALITY INSPECTED */ North Atlantic Treaty Organization Organisation du Tratte de l'Atlantique Nord The Mission of AGARD According to its Charter, the mission of AGARD is to bring together the leading personalities of the NATO nations in the fields of science and technology relating to aerospace for the following purposes: — Recommending effective ways for the member nations to use their research and development capabilities for the common benefit of the NATO community; — Providing scientific and technical advice and assistance to the Military Committee in the field of aerospace research and development (with particular regard to its military application); — Continuously stimulating advances in the aerospace sciences relevant to strengthening the common defence posture; Improving the co-operation among member nations in aerospace research and development; — Exchange of scientific and technical information; — Providing assistance to member nations for the purpose of increasing their scientific and technical potential; — Rendering scientific and technical assistance, as requested, to other NATO bodies and to member nations in connection with research and development problems in the aerospace field. The highest authority within AGARD is the National Delegates Board consisting of officially appointed senior representatives from each member nation. The mission of AGARD is carried out through the Panels which are composed of experts appointed by the National Delegates, the Consultant and Exchange Programme and the Aerospace Applications Studies Programme. The results of AGARD work are reported to the member nations and the NATO Authorities through the AGARD series of publications of which this is one. Participation in AGARD activities is by invitation only and is normally limited to citizens of the NATO nations. The content of this publication has been reproduced directly from material supplied by AGARD or the authors. Published October 1996 Copyright © AGARD 1996 All Rights Reserved ISBN 92-836-0029-0 Printed by Canada Communication Group 45 Sacre-Cceur Blvd., Hull (Quebec), Canada K1A 0S7 Tribology for Aerospace Systems (AGARD CP-589) Executive Summary Tribology deals with the design, friction, wear, and lubrication of interacting surfaces in relative motion, as bearings or gears. This definition sheds light on problems that tribological phenomena may cause in NATO's armaments, for example, systems failures and downtime repairs, supply and resupply with their costs in the permanent and/or temporary loss of trained personnel, and reoccurring materials and labor costs. In general solutions to these problems include redesign of components, replacement of materials with harder and/or lower friction materials, and improved lubricants. The objective of this AGARD Specialists' Meeting on Tribology for Aerospace Systems was twofold: — discuss the technology problems by having a meeting among specialists of new technologies (such as coatings, lubrication) and people dealing with practical problems in NATO systems (airframe, engines, etc.); — improve the knowledge of Tribology by engineers designing or maintaining NATO systems. The scope of the Meeting was broader than aerospace because papers on reciprocating engines in land based systems were also included. It must be realized that tribological phenomena such as friction and wear are problems that will never be completely overcome by technology but can be put in "remission" through some of the approaches outlined here. Rain and dust erosion were not included in the Terms of Reference and should be the subject of a future AGARD activity. La Tribologie pour les systemes aerospatiaux (AGARD CP-589) Synthese La tribologie concerne la conception, 1'interaction, l'usure par frottement et la lubrification des surfaces en mouvement relatif, tolles que les galets et les engrenages. Cette definition permet d'apprehender plus clairement les problemes qui peuvent etre poses par les phenomenes tribologiques au niveau des systemes d'armes de l'OTAN, comme par exemple, les pannes des systemes, les temps morts demandes pour les reparations, l'approvisionnement et le reapprovisionnement avec les coüts occasionnes par la perte provisoire et/ou permanente du personnel qualifie, ainsi que les coüts recurrents des materiaux et de la main d'ceuvre. En general, les solutions proposees par rapport ä ces problemes comprennent la redefinition des composants, le remplacement des materiaux usuels par des materiaux plus durs et/ou ä coefficient de frottement reduit, et l'emploi de lubrifiants ameliores. L'objectif de cette reunion de specialistes AGARD sur la tribologie pour systemes aerospatiaux etait double, ä savoir: — discuter des problemes technologiques lors d'une reunion rassemblant, d'une part, les - specialistes des nouvelles technologies (tolles que les revetements, la lubrification...), et, d'autre part, ceux qui sont appeles ä traitor les problemes d'ordre pratique poses par les systemes militaires de l'OTAN (cellule, moteur, etc.); — elargir les connaissances en tribologie des Ingenieurs responsables de la conception et de la maintenance des systemes militaires de l'OTAN. Les sujets examines lors de la reunion ont deborde le domaine purement aerospatial puisque des presentations sur les moteurs semblables des systemes terrestres ont ete donnees. Force est de constater que si certains phenomenes tribologiques tels que l'usure par le frottement ne pourront jamais etre totalement resolus technologiquement, ils pourraient neanmoins etre "mis en veilleuse" par 1'adoption de certaines approches decrites ici. L'erosion par la pluie et la poussiere, qui n'a pas ete indue dans les termes de reference de la reunion, meriterait de faire l'objet d'une activite future de l'AGARD. Contents Page Executive Summary iii Synthese iv Preface/Preface vii Structures and Materials Panel viii Technical Evaluation Report T by DJ. Viechnicki Reference SESSION I: NEW TECHNOLOGIES Paper not available 1 Tribological Behaviour of Silicon Nitride-based Ceramics 2 by J.R. Gomes, A.S. Miranda, R.F. Silva and J.M. Vieira Advanced Solid Lubricant Coatings for Aerospace Systems by J.S. Zabinski, S.V. Prasad and N.T. McDevitt Advanced Hard Coatings and Wear Resistant Materials for Aerospace Systems by J.S. Zabinski, A.A. Voevodin and M.A. Capano An Investigation on Surface Treatments for Improving the Fretting Fatigue Resistance of Titanium Alloys by A.K. Koul, L. Xue, W. Wallace, M. Bibby, S. Chakravarty, R.G. Andrews and P.C. Patnaik Thin Film Lubrication of Non-Smooth Surfaces by B. Jacobson Machining and Slip-Rolling of Ceramics by M. Woydt and U. Effner Sputter-Deposited Lubricant Thin Films Operating at Elevated Temperatures in Air by C. Zimmermann and Y. Pauleau SESSION II: APPLICATIONS: GEARS AND BEARINGS Paper 9 Withdrawn Tribological Problems in Spacecrafts 10 by A. Borrien Metallic and Non-Metallic Protection Systems for Reduction of Tribologic Influences in 11 Several Areas on Tornado Aircraft by CD. Hamm and K. Blomeier Improving Solid Lubricated Aerospace Bearings 12 by B. Mortimer and S. Mason Analysis of Fretting and Fretting Corrosion in Airframe Riveted Connections 13 by K. Iyer, M. Xue, P.C. Bastias, C.A. Rubin and G.T. Hahn SESSION HI: APPLICATIONS ENGINES EHD Analysis of a Roller/Inner Ring Contact in a Jet Engine Roller Bearing 14 by J. Seabra and A. Campos Rolling Contact Testing of Vapor Phase Lubricants 15 by N.H. Forster La fiabilite des roulements des petites et moyennes turbines de plus en plus dependante de la 16 tribologie by G. Paty and B. Cheftel Airseals for Advanced Military Jet Engines I7 by TJ. Uihlein High Temperature Tribology for Future Diesel Engines 18 by W. Bryzik and R. Kamo Tribological Assessments and Concepts for an Oilfree Internal Combustion Engine 19 by M. Woydt Preface The fretting and wear of hinges, tracks, bearings, gearboxes in airframes and engines is a constant problem for aircraft or other defense systems, as it causes breakages and jamming, necessitating costly in-service inspections and replacement of parts. As a result, there is ample room for improvement both for in-service systems and new systems being developed. The meeting was divided into three sessions: — one session on new technologies such as coatings, new materials, lubrication; — one session on practical applications for airframes and their mechanical systems; — one session on practical applications for engines. The meeting closed with a round table discussion. D. Chaumette Chairman Sub-Committee on Tribology for
Recommended publications
  • Handbook of MASS MEASUREMENT
    Handbook of MASS MEASUREMENT FRANK E. JONES RANDALL M. SCHOONOVER CRC PRESS Boca Raton London New York Washington, D.C. © 2002 by CRC Press LLC Front cover drawing is used with the consent of the Egyptian National Institute for Standards, Gina, Egypt. Back cover art from II Codice Atlantico di Leonardo da Vinci nella Biblioteca Ambrosiana di Milano, Editore Milano Hoepli 1894–1904. With permission from the Museo Nazionale della Scienza e della Tecnologia Leonardo da Vinci Milano. Library of Congress Cataloging-in-Publication Data Jones, Frank E. Handbook of mass measurement / Frank E. Jones, Randall M. Schoonover p. cm. Includes bibliographical references and index. ISBN 0-8493-2531-5 (alk. paper) 1. Mass (Physics)—Measurement. 2. Mensuration. I. Schoonover, Randall M. II. Title. QC106 .J66 2002 531’.14’0287—dc21 2002017486 CIP This book contains information obtained from authentic and highly regarded sources. Reprinted material is quoted with permission, and sources are indicated. A wide variety of references are listed. Reasonable efforts have been made to publish reliable data and information, but the author and the publisher cannot assume responsibility for the validity of all materials or for the consequences of their use. Neither this book nor any part may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopying, microfilming, and recording, or by any information storage or retrieval system, without prior permission in writing from the publisher. The consent of CRC Press LLC does not extend to copying for general distribution, for promotion, for creating new works, or for resale. Specific permission must be obtained in writing from CRC Press LLC for such copying.
    [Show full text]
  • MASTER En GENIE BIOMEDICAL USING X-RAYS in BIOMATERIALS
    Université Abou BakrBelkaïd de Tlemcen Faculté de Technologie Département de Génie Biomédical MEMOIRE DE PROJET DE FIN D’ETUDES Pourl’obtention du Diplôme de MASTER en GENIE BIOMEDICAL Spécialité :Imagerie Médicale / instrumentation biomédicale Présentépar : DJEBARNI Asma et ZIREK Amina USING X-RAYS IN BIOMATERIALS Soutenu le14/09/ 2017 devant le Jury M. BESSAID Abdelhafid Prof Université de Tlemcen Président M. SOULIMANE Sofiane MCB Université de Tlemcen Examinateur M. DIB Nabil MCB Université de Tlemcen Examinateur Année universitaire 2017-2018 [Texte] ACKNOWLEDGEMENT Thanks to “ALLAH” for the strength that he gives us that helped and supported us.This work has been realized in the frame ofERASMUS + Internationalstudent exchange program session February-July 2017 in LUBLIN UNIVERSITY OF TECHNOLOGY, POLAND. We would like to thank all the stuff from both countries for all the hard work for trying to make everything easier and to create such a memorable experience. Special thanks to: Mr SalimKERAI, head of department of biomedical engineering, University Tlemcen. MrSylwester SAMBORSKI, head of department of mechanical engineering, University Lublin. MrFethiREGUIG BEREKSI and Abdel hafid BESSAID, Professors, Responsibles, University Tlemcen. Mme Monika OSTAPIUK, Supervisor Professor and framer, University Lublin. Mr Omar BEHDADA, Home University Coordinator, University Tlemcen. Mme Anna RADZISZEWSKA, Host University Coordinator, University Lublin. We would first like to thank our thesis advisor Mr SOULIMANESofianeand Mr DIB Nabil for accepting being examiners and juries members. Finally, we must express our very profound gratitude to our parents and family for providing us with unfailing support and continuous encouragement throughout our years of study and through the process of researching and writing this thesis.
    [Show full text]
  • High-Temperature Reactor Components and Systems
    EUROPEAN COMMISSION 5th EURATOM FRAMEWORK PROGRAMME 1998-2002 KEY ACTION : NUCLEAR FISSION HTR-E High-Temperature Reactor Components and Systems CONTRACT N° FIKI-CT-2001-00177 Deliverable D39 for " Tribology in Helium Environment" Isabelle BOBIN VASTRA FRAMATOME -ANP FRANCE Dissemination level : RE Document N°: HTR-E- 03/12 – D – 5- 1 - 3 Status : Preliminary Deliverable D39 Framatome ANP identification N° :NFTW – R/03.898A FRA-ANP TFCW-IBV-R.03.898A HTR-E / WP5 – Tribology in Helium environment – D39 HTR-E Modifications Revision Date Modifications 0 30th January 2004 First issue Page 3 / 87 FRA-ANP TFCW-IBV-R.03.898A HTR-E / WP5 – Tribology in Helium environment – D39 HTR-E Content MODIFICATIONS .........................................................................................................................................................................3 LIST OF TABLES ……………………………………………………………………………………………………………….. 5 LIST OF REFERENCES ...............................................................................................................................................................6 REVIEW OF EXISTING MATERIALS AND COATINGS...........................................................................................................8 INTRODUCTION...........................................................................................................................................................................8 1. POSSIBLE MATERIAL PROBLEMS IN PBMR AND GTMHR (D38 REF [3])..........................................................8
    [Show full text]
  • High Precision Ball Bearings
    General Contents Designations Contents Chapter 5 HIGH PRECISION BALL BEARINGS LA TECHNOLOGIE EN MOUVEMENT TECHNOLOGY IN MOTION General Contents Designations Contents Chapter 5 Contents 1 Directions . .p 2 Chapter 1 • Foreword . .p 3 Chapter 2 • Design . .p 15 A • ADR bearing designations . .p 16 B • Technical Definition of Products . .p 18 Position 1 • Materials for rings and balls . .p 18 Position 2 • Outer shape . .p 22 Position 3 • Dimension reference . .p 24 Position 4 • Inner shape . .p 28 Position 5 • Shields/Seals . .p 30 Position 6 • Cage/Retainer . .p 32 Position 7 • Tolerances . .p 36 Position 8 • Radial internal clearance and contact angle . .p 44 Position 9 • Preload and duplex configurations . .p 48 Position 10 • Vibration level . .p 54 The data in this catalogue is based on our current production. Position 11 • Surface treatment and coating . .p 55 ADR reserves the right to make changes which are necessary by technological development. ADR also reserves the right Position 12 • Torque . .p 56 to change without notice the technical characteristics of illustrated components. Position 13 • Calibration . .p 59 Position 14 • Lubrication . .p 62 ADR S.A.S. copyright. It is prohibited to reproduce or publish by any means or in any form whatsoever all or part of Position 15 • Specification . .p 66 this catalogue without express indication of the sources and written agreement from ADR S.A.S. The technical characteristics and data mentioned apply only to ADR products. Chapter 3 • Bearing characteristics . .p 67 ADR disclaims any responsibility in case technical information is misused or misinterpreted. Chapter 4 • Mounting study . .p 70 Chapter 5 • Bearing tables .
    [Show full text]
  • Npl Report Cmam(Res)
    NPL REPORT CMAM 36(a) A Collaboration Between Ten National Measurement Institutes To Measure The Mass Of Two One Kilogram Mass Standards This Report Supersedes NPL Report CMAM 36 I Severn SEPTEMBER 2000 NPL Report CMAM 36(a) NPL Report CMAM 36(a) A Collaboration Between Ten National Measurement Institutes To Measure The Mass of Two One Kilogram Mass Standards I Severn Centre for Mechanical and Acoustical Metrology National Physical Laboratory Queens Road, Teddington, TW11 0LW United Kingdom September 2000 ABSTRACT A comparison has been carried out in which ten Western European national metrology institutes have determined the mass difference between a pair of 1 kg mass standards and assigned mass values to each of the weights. The results obtained illustrate that the measurements of the participants agree to within their quoted uncertainties (for a coverage factor of k=2), so demonstrating the metrological equivalence of mass measurements using stainless steel 1 kg standards in each of these institutes. NPL Report CMAM 36(a) Crown copyright 2000 Reproduced by permission of the controller of HMSO ISSN 1369 - 6785 National Physical Laboratory Teddington, Middlesex, United Kingdom, TW11 0LW No extracts from this report may be reproduced without the prior written consent of Managing Director, National Physical Laboratory; if consent is given the source must be acknowledged and may not be used out of context. Approved on behalf of the Managing Director, NPL, by Dr G R Torr, Head of Centre Centre for Mechanical and Acoustical Metrology. NPL Report CMAM 36(a) CONTENTS 1. INTRODUCTION 1 2. MEASUREMENTS 1 2.1 ARTEFACTS 1 2.2 CIRCULATION SCHEME 2 2.3 TRANSPORTATION 2 3.
    [Show full text]
  • 2019 La Passion De L’Excellence Passion for Excellence Au Service Des Entreprises Et De L’Emploi, Caux Seine Développement Vous Accompagne
    La passion de l'Excellence ANNUAIRE 2019 La passion de l’excellence passion for excellence Au service des entreprises et de l’emploi, Caux Seine développement vous accompagne. Biens immobiliers et fonciers Aides financières Aide au recrutement Ingénierie de projets Réseaux d’acteurs ©Studio Huon - Caudebec-en-Caux Vous avez un projet ? cauxseinedeveloppement.com +33 (0)2 32 84 40 32 You have a project ? [email protected] Caux Seine agglo : la se [ré]invente ici ! NORMANDIE AEROESPACE LA PASSION DE L’EXCELLENCE CHIFFRES CLÉS Une filière 155 MEMBRES d’excellence 155 MEMBERS en Normandie 3 MDS € DE CA La passion de l'Excellence 3 BILLION € TURNOVER UNE CROISSANCE CONTINUE CONTINUED GROWTH www.nae.fr 21 000 SALARIÉS 21 000 EMPLOYEES 4 AXES RECHERCHE, TECHNOLOGIE & INNOVATION Faire de la recherche, technologie et innovation un levier majeur de compétitivité RESEARCH, TECHNOLOGY & INNOVATION To make research, technology and innovation a major level for competitiveness BUSINESS & PERFORMANCE Soutenir le développement des entreprises BUSINESS & PERFORMANCE To support the business development and a high-level of suppliers and competencies EMPLOI & FORMATION Répondre aux besoins en compétences et préparer les métiers de demain EMPLOYMENT & TRAINING To meet the companies need for skills and prepare tomorrow’s jobs COMMUNICATION Valoriser l’excellence de la filière normande. COMMUNICATION To increase the popularity and attractiveness of aerospace in Normandy Création graphique : LE BUREAU ET L’ÉQUIPE NAE — PRÉSIDENCE Philippe EUDELINE Gérard LISSOT
    [Show full text]
  • Thermal Desorption Mass Spectrometry (Tds) Application on Mass Metrology
    XIX IMEKO World Congress Fundamental and Applied Metrology September 6 11, 2009, Lisbon, Portugal THERMAL DESORPTION MASS SPECTROMETRY (TDS) APPLICATION ON MASS METROLOGY Zaccaria Silvestri1 and Patrick Pinot2 1Laboratoire commun de métrologie LNE-Cnam, La Plaine Saint-Denis, France, [email protected] 2Laboratoire commun de métrologie LNE-Cnam, La Plaine Saint-Denis, France, [email protected] Abstract A new device has been developed for the There are different elements that affect long term stability of study of physisorbed elements on polished and large surface a mass standard of high accuracy level such as: used in mass metrology. - physical and chemical characteristics of the This technique, based on the analysis by mass materials: spectrometry of desorbed molecules caused by heating o good hardness (>180 Hv) to facilitate under vacuum from the analyzed surface, is presented. machining, polishing and to reduce wear The first application of this device is the study of the when manipulating the artefact; current and future mass standards to understand the o high density in order to limit surface effect reactivity of their surface depending of the storage in air and so to have a more stable mass; conditions, of the cleaning process and polishing method. o good homogeneity without porosity, So, an example of surface contamination analysis by thermal cavity and occluded gases in order to desorption mass spectrometry (about cleaning effect on a guarantee long-term stability; super alloy based on cobalt) is given. o sufficient electrical conductivity to avoid accumulating electrostatic charges and Keywords: Mass spectrometry, thermal desorption, good thermal conductivity to minimize cleaning effect, contamination.
    [Show full text]
  • (12) United States Patent (10) Patent No.: US 8,852.264 B2 Pacetti Et Al
    USOO8852264B2 (12) United States Patent (10) Patent No.: US 8,852.264 B2 Pacetti et al. (45) Date of Patent: *Oct. 7, 2014 (54) RADIOPAQUE INTRALUMINAL STENT (56) References Cited (75) Inventors: Stephen Pacetti, San Jose, CA (US); U.S. PATENT DOCUMENTS Pamela A. Kramer, San Jose, CA (US) 4,685,977 A 8/1987 Chang 5,061.275 A 10, 1991 Wallsten et al. (73) Assignee: Abbott Cardiovascular Systems, Inc., 5.330,826 A 7/1994 Taylor et al. 5,421.955 A 6/1995 Lau et al. Santa Clara, CA (US) 5,514,154 A 5/1996 Lau et al. 5,569,295 A 10, 1996 Lam (*) Notice: Subject to any disclaimer, the term of this 5,603,721 A 2f1997 Lau et al. patent is extended or adjusted under 35 5,618,299 A 4/1997 Khosravi et al. 5,628,787 A 5/1997 Mayer U.S.C. 154(b) by 0 days. 5,630,840 A 5/1997 Mayer This patent is Subject to a terminal dis 5,636,641 A 6, 1997 Fariabi claimer. 5,649,952 A 7, 1997 Lam 5,716,417 A 2f1998 Girard et al. 5,725,572 A 3, 1998 Lam et al. (21) Appl. No.: 13/618,602 5,728, 158 A 3, 1998 Lau et al. 5,735,893 A 4/1998 Lau et al. 5,759,192 A 6/1998 Saunders (22) Filed: Sep. 14, 2012 5,766,238 A 6/1998 Lau et al. (65) Prior Publication Data (Continued) US 2013/OO 13055A1 Jan. 10, 2013 FOREIGN PATENT DOCUMENTS EP O804934 3, 1997 EP 1604691 12/2005 Related U.S.
    [Show full text]