DOCSLIB.ORG

DELTA4000/5000/4D/5D Version / Release 2.1 Manuel Opérateur Multilingue Multilingual Operator’S Manual Ref

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
DELTA4000/5000/4D/5D Version / Release 2.1 Manuel Opérateur Multilingue Multilingual Operator’S Manual Ref 6159938010-07 DELTA4000/5000/4D/5D Version / Release 2.1 Manuel opérateur multilingue Multilingual operator’s manual Ref. / N° : 6159938010-07 English ...................................3 Français................................27 Español ................................51 Deutsch ................................75 Italiano................................101 Português...........................127 Nederlands.........................151 Svenska..............................177 Georges Renault S.A.S - 199 route de Clisson - B.P.13627 44236 Saint Sébastien-sur-Loire Cedex France 6159938010-07 6159938010-07 English 3 / 200 DELTA4000/5000/4D/5D Release 2.1 Operator's Manual No. 6159938010-07 © Copyright 2005, GEORGES RENAULT S.A.S, 44230 France All rights reserved. Any unauthorized use or copying of the contents or part thereof is prohibited. This applies in particular to © trademarks, model denominations, part numbers and drawings. Use only authorized parts. Any damage or malfunction caused by the use of unauthorised parts is not covered by Warranty or Product Liability. Georges Renault S.A.S - 199 route de Clisson - B.P.13627 44236 Saint Sébastien-sur-Loire Cedex France 6159938010-07 TABLE OF CONTENTS English 4 / 200 TABLE OF CONTENTS 1 - INTRODUCTION ................................................................................................................................... 5 2 - DESCRIPTION OF THE UNIT .............................................................................................................. 5 2.1 - Front side .................................................................................................................................................5 2.2 - Rear side .................................................................................................................................................6 2.3 - Battery block ............................................................................................................................................6 2.4 - Maintenance instructions .......................................................................................................................6 3 - MEASURING......................................................................................................................................... 7 4 - "PARAMETERS" MENU ...................................................................................................................... 9 4.1 - "Task" menu...........................................................................................................................................10 4.2 - "Printer" Menu .......................................................................................................................................12 4.3 - "Serial link" Menu..................................................................................................................................12 5 - "RESULTS" MENU............................................................................................................................. 12 5.1 - "Measurements" Menu..........................................................................................................................12 5.2 - "Curve" Menu.........................................................................................................................................13 5.3 - " Statistics" Menu..................................................................................................................................14 6 - DOWNLOAD ....................................................................................................................................... 14 7 - SERVICE............................................................................................................................................. 14 7.1 - "Contrast" Menu ....................................................................................................................................14 7.2 - "Date" Menu ...........................................................................................................................................15 7.3 - "Language" Menu..................................................................................................................................15 7.4 - "Access Code" Menu ............................................................................................................................15 7.5 - "Auto stop" Menu ..................................................................................................................................15 7.6 - "Buzzer" Menu .......................................................................................................................................15 8 - TACHOMETER ................................................................................................................................... 15 9 - MAINTENANCE .................................................................................................................................. 15 9.1 - "Input/Output" Menu .............................................................................................................................15 9.2 - "Transducer" Menu ...............................................................................................................................15 Appendix 1 - Diagrams: PC cable, torque transducer connectors and I/O connector .......16 Appendix 2 - Standard printing format for the measurements.............................................18 Appendix 3 - "Curve" format....................................................................................................18 Appendix 4 - Statistical computations ....................................................................................19 Appendix 5 - Transferring measurements and curves to a PC.............................................25 6159938010-07 DELTA4000/5000/4D/5D English 5 / 200 1 - INTRODUCTION DELTA is a measuring unit designed to be used with the analog torque (and angle) transducers** and DRT range, to check the following: - for the DELTA4000/4D ....the torque applied. - for the DELTA5000/5D ....the torque and/or angle applied. DELTA Torque Torque and angle Transducer 4000 XCMD / DRT 4D XDRT 5000 X X CMD / DRT 5D XXDRT Any other use is prohibited. This equipment is for professional use only Easy to use, lightweight and self-contained, it has been specially designed for checking campaigns on tightening stations. ** DELTA4000/5000 only The unit is supplied with: - universal charger (P.N. 6159229480) - support kit including strap, strap holders, printer and PC connectors. - mains cable (P.N. to be specified on order according to country of destination) Europe (except UK).......6159172010 UK ................................. 6159172020 USA...............................6159172030 Weight: 1 200 g Dimensions: Depth: 190 mm Width: 230 mm Height: 100 mm 2 - DESCRIPTION OF THE UNIT 2.1 - Front side Report angle LED (for the Report LEDs DELTA5000/5D): Min. - torque: Min. - Accept - Accept - Max. Max. 78abc def 9 ghi a On / off Esc Alphanumerical keyboard 4 jkl 5 mno 6 pqr Key for browsing with 12stu vwx 3 yz "Decimal point" and Valid through the menus 0 . -+ "Space" keys DELTA Escape, Validate, Print key Description of the keys: To scroll through a menu. ª « To scroll through a data entry screen. to increment digits. To scroll through a lozenge-tagged list. ¨ © To scroll through a data entry field. To scroll through a horizontal menu. Alphanumerical key £ To scroll the digit and the letters, press the key several times successively. To validate a change. { To display the next screen. To go to the next field. 6159938010-07 DELTA4000/5000/4D/5D English 6 / 200 ¡ To exit a screen without saving changes. ¢ To exit a screen and save the changes. ¥ To open the print request screens. ¤ To perform an Automatic Zero Correction ( AZC) on the transducer. 2.2 - Rear side DRT digital transducer PC connection SubD 9 points (torque or torque and angle) Strap holder* Parallel printer Input/output connection SubD 25 points SubD 15 points Analog torque and angle Analog torque transducer connector (for the DELTA4000/ (for the DELTA5000) 5000**) Charge indicator lamp Battery charger socket * To install the strap holder, untighten the two screws and re-secure the holder with the screws. ** DELTA4000/5000 only 2.3 - Battery block The battery block is extractible and consists of 6 x 1.2 V (7.2 V) NimH elements, rechargeable inside or outside the unit. P.N.: 6159350420. Battery life is 14 hours. It allows up to 1000 Discharging/Recharging cycles. Automatic stop when the unit is idle is programmable (see "Service" menu). When the battery indicator blinks on the screen on the front side, it is necessary to recharge the battery block using the charger supplied with the unit. - The battery indicator crossed out means a connection fault with the battery block. - When blinking, the charge indicator lamp located on the left side of the charger socket means that the cable is correctly connected and the charging of the battery block is running smoothly. - When the lamp is on, it means that the charging process has been completed. Battery block opening procedure: 2.4 - Maintenance instructions Any maintenance task shall be performed by CP authorised representatives 6159938010-07 DELTA4000/5000/4D/5D English 7 / 200 3 - MEASURING Check that the cables are connected correctly on the rear side of the unit. When switched on,
Load more

Recommended publications
  • Douglas Missile & Space Systems Division
    ·, THE THOR HISTORY. MAY 1963 DOUGLAS REPORT SM-41860 APPROVED BY: W.H.. HOOPER CHIEF, THOR SYSTEMS ENGINEERING AEROSPACE SYSTEMS ENGINEERING DOUGLAS MISSILE & SPACE SYSTEMS DIVISION ABSTRACT This history is intended as a quick orientation source and as n ready-reference for review of the Thor and its sys­ tems. The report briefly states the development of Thor, sur'lli-:arizes and chronicles Thor missile and booster launch­ inGs, provides illustrations and descriptions of the vehicle systcn1s, relates their genealogy, explains sane of the per­ fon:iance capabilities of the Thor and Thor-based vehicles used, and focuses attention to the exploration of space by Douelas Aircraf't Company, Inc. (DAC). iii PREFACE The purpose of The Thor History is to survey the launch record of the Thor Weapon, Special Weapon, and Space Systems; give a systematic account of the major events; and review Thor's participation in the military and space programs of this nation. The period covered is from December 27, 1955, the date of the first contract award, through May, 1963. V �LE OF CONTENTS Page Contract'Award . • • • • • • • • • • • • • • • • • • • • • • • • • 1 Background • • • • • • • • • • • • • • • • • • • • • • • • • • • • l Basic Or�anization and Objectives • • • • • • • • • • • • • • • • 1 Basic Developmenta� Philosophy . • • • • • • • • • • • • • • • • • 2 Early Research and Development Launches • • • ·• • • • • • • • • • 4 Transition to ICBM with Space Capabilities--Multi-Stage Vehicles . 6 Initial Lunar and Space Probes ••••••• • • • • • • •
    [Show full text]
  • Space) Barriers for 50 Years: the Past, Present, and Future of the Dod Space Test Program
    SSC17-X-02 Breaking (Space) Barriers for 50 Years: The Past, Present, and Future of the DoD Space Test Program Barbara Manganis Braun, Sam Myers Sims, James McLeroy The Aerospace Corporation 2155 Louisiana Blvd NE, Suite 5000, Albuquerque, NM 87110-5425; 505-846-8413 [email protected] Colonel Ben Brining USAF SMC/ADS 3548 Aberdeen Ave SE, Kirtland AFB NM 87117-5776; 505-846-8812 [email protected] ABSTRACT 2017 marks the 50th anniversary of the Department of Defense Space Test Program’s (STP) first launch. STP’s predecessor, the Space Experiments Support Program (SESP), launched its first mission in June of 1967; it used a Thor Burner II to launch an Army and a Navy satellite carrying geodesy and aurora experiments. The SESP was renamed to the Space Test Program in July 1971, and has flown over 568 experiments on over 251 missions to date. Today the STP is managed under the Air Force’s Space and Missile Systems Center (SMC) Advanced Systems and Development Directorate (SMC/AD), and continues to provide access to space for DoD-sponsored research and development missions. It relies heavily on small satellites, small launch vehicles, and innovative approaches to space access to perform its mission. INTRODUCTION Today STP continues to provide access to space for DoD-sponsored research and development missions, Since space first became a viable theater of operations relying heavily on small satellites, small launch for the Department of Defense (DoD), space technologies have developed at a rapid rate. Yet while vehicles, and innovative approaches to space access.
    [Show full text]
  • John F. Kennedy Space Center
    1 . :- /G .. .. '-1 ,.. 1- & 5 .\"T!-! LJ~,.", - -,-,c JOHN F. KENNEDY ', , .,,. ,- r-/ ;7 7,-,- ;\-, - [J'.?:? ,t:!, ;+$, , , , 1-1-,> .irI,,,,r I ! - ? /;i?(. ,7! ; ., -, -?-I ,:-. ... 8 -, , .. '',:I> !r,5, SPACE CENTER , , .>. r-, - -- Tp:c:,r, ,!- ' :u kc - - &te -- - 12rr!2L,D //I, ,Jp - - -- - - _ Lb:, N(, A St~mmaryof MAJOR NASA LAUNCHINGS Eastern Test Range Western Test Range (ETR) (WTR) October 1, 1958 - Septeniber 30, 1968 Historical and Library Services Branch John F. Kennedy Space Center "ational Aeronautics and Space Administration l<ennecly Space Center, Florida October 1968 GP 381 September 30, 1968 (Rev. January 27, 1969) SATCIEN S.I!STC)RY DCCCIivlENT University uf A!;b:,rno Rr=-?rrh Zn~tituta Histcry of Sciecce & Technc;oGy Group ERR4TA SHEET GP 381, "A Strmmary of Major MSA Zaunchings, Eastern Test Range and Western Test Range,'" dated September 30, 1968, was considered to be accurate ag of the date of publication. Hmever, additianal research has brought to light new informetion on the official mission designations for Project Apollo. Therefore, in the interest of accuracy it was believed necessary ta issue revfsed pages, rather than wait until the next complete revision of the publiatlion to correct the errors. Holders of copies of thia brochure ate requested to remove and destroy the existing pages 81, 82, 83, and 84, and insert the attached revised pages 81, 82, 83, 84, 8U, and 84B in theh place. William A. Lackyer, 3r. PROJECT MOLL0 (FLIGHTS AND TESTS) (continued) Launch NASA Name -Date Vehicle -Code Sitelpad Remarks/Results ORBITAL (lnaMANNED) 5 Jul 66 Uprated SA-203 ETR Unmanned flight to test launch vehicle Saturn 1 3 7B second (S-IVB) stage and instrment (IU) , which reflected Saturn V con- figuration.
    [Show full text]
  • DELTA - Guida Dell’Utente
    Numero di Serie 6159925300 Versione 15 Data 09/2018 Pagina 1 / 245 DELTA - Guida dell’utente AVVERTENZA Per ridurre il rischio di lesioni, prima dell’utilizzo o della manutenzione dello strumento leggere e comprendere le seguenti informazioni. Le caratteristiche e le descrizioni dei nostri prodotti sono soggette a modifiche senza preavviso. 1 (245) 09/2018 Numero di Serie 6159925300 Versione 15 Data 09/2018 Pagina 2 / 245 Cronologia revisioni Versione Rif. versione Versione Data Descrizione minima firmware DeltaQC 01 4 gennaio 2012 Prima versione 1.0x 2.0.x Revisione generale del manuale, aggiunta statistica Q54000, aggiunto DRT per i test 13 novembre 02 di qualità, aggiunta programmazione test, 1.1x 2.2.x 2012 aggiunta interfaccia SIMAP-Box, Statistiche e Impostazioni aggiornate. Coppia/angolo residuo automatico aggiunto (par.17.2), Test rapido aggiunto per Delta 6D/7D (par.8.1), Configurazione Pset aggiornata (par. 9), Visualizzatore curve aggiornato (par. 21), Statistiche 03 2 maggio 2013 1.3x 2.4.x aggiornate (par. 19), Calibrazione CVI3 aggiunta (par.8.3.2), Manutenzione aggiornata (par. 22), Risultati tramite Ethernet aggiunti, Revisione manuale generale Picco angolo aggiunto, inserimento codice 04 2 agosto 2013 1.4x 2.5.x a barre manuale aggiunto (par.8.2.3) 23 gennaio Visualizzatore dei risultati aggiornato (par. 05 1.5x 2.6.x 2014 20), Trasduttore ART aggiunto Scanner di codici a barre interno aggiunto (par.3.5 e 8.2.3), Strategie di produzione 20 ottobre aggiunte (par.19), "Serraggio" aggiunto in 06 2.0x 3.0.x 2014 modalità Demo (par.6.1.4), Trasduttore analogico personalizzato aggiunto (par.
    [Show full text]
  • Ex Latere Christi Ex Latere Christi
    EX LATEREWoman: Her Nature & CHRISTIVirtues THE PONTIFICAL NORTH AMERICAN COLLEGE WINTER 2020 - ISSUE 1 1 11 First Feature 32 Second Feature 34 Third Feature 36 Fourth Feature EX LATERE CHRISTI EX LATERE CHRISTI Rector, Publisher (ex-officio) VERY Rev. PETER C. HARMAN, STD Academic Dean, Executive Editor (ex-officio) Rev. JOHN P. CUSH, STD Editor-in-Chief Rev. RANDY DEJESUS SOTO, STD Managing Editor MR. AleXANdeR J. WYVIll, PHL Student Editor MR. AARON J. KellY, PHL Assistant Student Editor MR. THOMAS O’DONNell, BA www.pnac.org TAble OF CONTENTS A WORD OF INTRODUCTION FROM THE EXECUTIVE EDITOR 7 Rev. John P. Cush, STD EX LATERE CHRISTI 10 Msgr. William Millea, STL, JCD SAlve, AEDES MATER! 11 Rev. Randy DeJesus Soto, STD WOMAN: HER NATURE & VIRTUES 13 Sr. Mary Angelica Neenan, O.P., STD AS THE PERSON GOES, SO GOES THE WHOLE WORLD 39 Aaron J. Kelly, PHL BEING IN THE RIGHT 51 Alexander J. Wyvill, PHL HANS URS VON BALTHASAR AND DIALOGICAL PHILOSOPHY 91 Rev. Walter R. Oxley, STD JESUS CHRIST: WORD, PREACHER AND LORD 101 Rev. Randy DeJesus Soto, STD HOMILY FOR THE MASS OF THE PASSION OF ST. JOHN THE BAPTIST 131 Rev. Adam Y. Park, STL LOGOS, CREATION AND SCIENCE 135 Rev. Joseph Laracy, STD HOLINESS 163 Msgr. James McNamara, M.Div., MS, PA CATHERINE PICKSTOCK’S EUCHARISTIC THEOLOGY 167 Rev. John P. Cush, STD CONTRIBUTORS 211 6 Rev. JOHN P. CUSH, STD A WORD OF INTRODUCTION FROM THE EXecUTIve EDITOR As the college’s academic dean, it is a joy to present to you Ex Latere Christi, the first academic journal published by the faculty, alumni, and friends of the Pontifical North American College.
    [Show full text]
  • Table of Contents
    THE CAPE Military Space Operations 1971-1992 by Mark C. Cleary 45th Space Wing History Office Table of Contents Preface Chapter I -USAF Space Organizations and Programs Table of Contents Section 1 - Air Force Systems Command and Subordinate Space Agencies at Cape Canaveral Section 2 - The Creation of Air Force Space Command and Transfer of Air Force Space Resources Section 3 - Defense Department Involvement in the Space Shuttle Section 4 - Air Force Space Launch Vehicles: SCOUT, THOR, ATLAS and TITAN Section 5 - Early Space Shuttle Flights Section 6 - Origins of the TITAN IV Program Section 7 - Development of the ATLAS II and DELTA II Launch Vehicles and the TITAN IV/CENTAUR Upper Stage Section 8 - Space Shuttle Support of Military Payloads Section 9 - U.S. and Soviet Military Space Competition in the 1970s and 1980s Chapter II - TITAN and Shuttle Military Space Operations Section 1 - 6555th Aerospace Test Group Responsibilities Section 2 - Launch Squadron Supervision of Military Space Operations in the 1990s Section 3 - TITAN IV Launch Contractors and Eastern Range Support Contractors Section 4 - Quality Assurance and Payload Processing Agencies Section 5 - TITAN IIIC Military Space Missions after 1970 Section 6 - TITAN 34D Military Space Operations and Facilities at the Cape Section 7 - TITAN IV Program Activation and Completion of the TITAN 34D Program Section 8 - TITAN IV Operations after First Launch Section 9 - Space Shuttle Military Missions Chapter III - Medium and Light Military Space Operations Section 1 - Medium Launch Vehicle and Payload Operations Section 2 - Evolution of the NAVSTAR Global Positioning System and Development of the DELTA II Section 3 - DELTA II Processing and Flight Features Section 4 - NAVSTAR II Global Positioning System Missions Section 5 - Strategic Defense Initiative Missions and the NATO IVA Mission Section 6 - ATLAS/CENTAUR Missions at the Cape Section 7 - Modification of Cape Facilities for ATLAS II/CENTAUR Operations Section 8 - ATLAS II/CENTAUR Missions Section 9 - STARBIRD and RED TIGRESS Operations Section 10 - U.S.
    [Show full text]
  • Access to Space
    databk7_collected.book Page 989 Monday, September 14, 2009 2:53 PM INDEX A (Office of Space Science), 585 Advanced Transportation Technology, 101 Academic programs, 10, 14 Advanced X-ray Astronomical Facility (AXAF) Accelerometer, 959 approval of, 576 "Access to Space" study, 22, 80, 172 AXAF-I, 653 ACE-Able Engineering, Inc, 857 AXAF-S, 653 Active Cavity Radiometer Irradiance Monitor budgets and funding for, 653–54, 779 (ACRIM), 421, 480 Chandra (AXAF), 576, 579, 652, 655–57, Acuña, Mario H., 940, 945, 953, 956 838–41 Adamson, James C. characteristics, instruments, and experiments, STS-28, 360, 380 654–57, 838–41; Advanced Charged Couple STS-43, 363, 409 Imaging Spectrometer (ACIS), 656, 657, Adrastea, 711 839, 840; High Energy Transmission Grating Advanced Carrier Customer Equipment Support (HETG) spectrometer, 657, 839–40, 841; System, 223 High Resolution Camera (HRC), 656, 657, Advanced Charged Couple Imaging Spectrometer 839, 840; High Resolution Mirror Assembly, (ACIS), 656, 657, 839, 840 654, 656–57; Low Energy Transmission Advanced Communications Technology Satellite Grating (LETG) spectrometer, 657, 839–40; (ACTS), 161, 252, 254, 366, 454 Science Instrument Module (SIM), 657 Advanced Composition Explorer (ACE), 140, deployment of, 579 579, 604–5, 606, 607, 772, 781, 806–9 development of, 652, 653 Advanced Concepts and Technology, Office of objective of, 589, 652–53 (Code C) Advisory Committee on the Future of the U.S. budgets and funding for, 13, 33, 35, 89, 91, 94, Space Program, 204–5, 287, 564 100 Aero Corporation, 894, 897
    [Show full text]
  • RWTH Aachen University Institute of Jet Propulsion and Turbomachinery
    RWTH Aachen University Institute of Jet Propulsion and Turbomachinery DLR - German Aerospace Center Institute of Space Propulsion Optimization of a Reusable Launch Vehicle using Genetic Algorithms A thesis submitted for the degree of M.Sc. Aerospace Engineering by Simon Jentzsch June 20, 2020 Advisor: Felix Wrede, M.Sc. External Advisors: Kai Dresia, M.Sc. Dr. Günther Waxenegger-Wilfing Examiner: Prof. Dr. Michael Oschwald Statutory Declaration in Lieu of an Oath I hereby declare in lieu of an oath that I have completed the present Master the- sis entitled ‘Optimization of a Reusable Launch Vehicle using Genetic Algorithms’ independently and without illegitimate assistance from third parties. I have used no other than the specified sources and aids. In case that the thesis is additionally submitted in an electronic format, I declare that the written and electronic versions are fully identical. The thesis has not been submitted to any examination body in this, or similar, form. City, Date, Signature Abstract SpaceX has demonstrated that reusing the first stage of a rocket implies a significant cost reduction potential. In order to maximize cost savings, the identification of optimum rocket configurations is of paramount importance. Yet, the complexity of launch systems, which is further increased by the requirement of a vertical landing reusable first stage, impedes the prediction of launch vehicle characteristics. Therefore, in this thesis, a multidisciplinary system design optimization approach is applied to develop an optimization platform which is able to model a reusable launch vehicle with a large variety of variables and to optimize it according to a predefined launch mission and optimization objective.
    [Show full text]
  • The Future of the European Space Sector How to Leverage Europe’S Technological Leadership and Boost Investments for Space Ventures
    The future of the European space sector How to leverage Europe’s technological leadership and boost investments for space ventures The future of the European space sector How to leverage Europe’s technological leadership and boost investments for space ventures Prepared for: The European Commission By: Innovation Finance Advisory in collaboration with the European Investment Advisory Hub, part of the European Investment Bank’s advisory services Authors: Alessandro de Concini, Jaroslav Toth Supervisor: Shiva Dustdar Contact: [email protected] Consultancy support: SpaceTec Partners © European Investment Bank, 2019. All rights reserved. All questions on rights and licensing should be addressed to [email protected] Disclaimer This Report should not be referred to as representing the views of the European Investment Bank (EIB), of the European Commission (EC) or of other European Union (EU) institutions and bodies. Any views expressed herein, including interpretation(s) of regulations, reflect the current views of the author(s), which do not necessarily correspond to the views of EIB, of the EC or of other EU institutions and bodies. Views expressed herein may differ from views set out in other documents, including similar research papers, published by the EIB, by the EC or by other EU institutions and bodies. Contents of this Report, including views expressed, are current at the date of publication set out above, and may change without notice. No representation or warranty, express or implied, is or will be made and no liability or responsibility is or will be accepted by EIB, by the EC or by other EU institutions and bodies in respect of the accuracy or completeness of the information contained herein and any such liability is expressly disclaimed.
    [Show full text]
  • Open Robertklein-Dissertation FINAL.Pdf
    The Pennsylvania State University The Graduate School DIELECTRIC PROPERTIES OF CONDUCTIVE IONOMERS A Thesis in Materials Science and Engineering by Robert James Klein c 2007 Robert James Klein Submitted in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy May 2007 The thesis of Robert James Klein was reviewed and approved∗ by the following: James Runt Professor of Polymer Science Associate Head for Graduate Studies of the Department of Materials Science and Engineering Thesis Advisor, Chair of Committee Ralph H. Colby Professor of Materials Science and Engineering Ronald Hedden Assistant Professor of Materials Science and Engineering Janna K. Maranas Associate Professor of Chemical Engineering and Materials Science and Engineering Gary L. Messing Distinguished Professor of Ceramic Science and Engineering Head of the Department of Materials Science and Engineering ∗Signatures are on file in the Graduate School. Abstract Ion and polymer dynamics of ion-containing polymers were investigated, with the majority of results obtained from application of a physical model of electrode polarization (EP) to dielectric spectroscopy data. The physical model of MacDon- ald, further developed by Coelho, was extended for application to tan δ (the ratio of dielectric loss to dielectric constant) as a function of frequency. The validity of this approach was confirmed by plotting the characteristic EP time as a function of thickness and comparing the actual and predicted unrelaxed dielectric constant for a poly(ethylene oxide) (PEO) -based ionomer neutralized by lithium, sodium, and cesium. Results were obtained for ion mobility and mobile ion concentration for a neat PEO-based ionomer, two (methoxyethoxy-ethoxy phosphazene) (MEEP) -based ionomers, two MEEP-based salt-doped polymers, sulfonated polystyrene (SPS) neutralized by sodium with a high sulfonation fraction, and SPS neutralized by zinc with a low sulfonation fraction.
    [Show full text]
  • Ieln® August
    IElN® August - ,- , . , .I , f J . '. 1/1 I , ,,' F "­ - , '- .' ~\ ~... ,' . .. ;:-. , " /' \ / " ; - \ ,. ( / _ f ". \ . , 1 ") I -I " . : I f, • , / . ../ -- - -- / I , . : ~ ." ./ , # MEASURING EMPLOYEE POTENTIAL Also: INFO'75, and IBM's 704: a first-generation money-maker ... l' "j "1 .I , . : 1 '1 " 1I J 1 " , Ii 1, I I I 1 l ' J~) r .• I j I r lJ l, ,: _ ,1 .,. ~ j l;' .J'J' lJ ~. lJ ' .J l j " i ,I I ,'I i We Malee The I Best Data ___ ";";""'.~'""';~U·"":~:::"."~'--::':::--_--- i Terminals Better I , I ,i When you distribute data terminals manufactured by the best names in the business - like DEC, Diablo, Lear Siegler, Techtran - how do you make the best termi nals better? Take the DECwriter II, for example. We're a major distributor of DECwriters. A very good terminal - everybody knows that. We make it better with exclusive low cost options available only from Randal Data Systems. Exclusive options such as: TWX ALTERNATE - lets you use a DEC­ writer in a TWX or computer network. ~CDJ ====-=='==---------===-:t ~0 ~ ANSWER-BACK - 'I I up to 32 characters available for identifica­ ~\_=-----=-:,:~~ , ' tion response. ::--.J I I! TOP-OF-FORM- :' I I I I "Form Feed" code ad­ vances paper to top of '/ next form page. II At Randal Data Systems we HORIZONTAL TAB - II I have a full product line of the II "HT" code provides for best data terminals on the 'I columnar output. market. We deliver off-the-shelf, i I at very favorable purchase or : I lease prices, and provide com­ The DECwriter II is plete customer service.
    [Show full text]
  • Before the Pyramids Oi.Ucicago.Edu
    oi.ucicago.edu Before the pyramids oi.ucicago.edu before the pyramids baked clay, squat, round-bottomed, ledge rim jar. 12.3 x 14.9 cm. Naqada iiC. oim e26239 (photo by anna ressman) 2 oi.ucicago.edu Before the pyramids the origins of egyptian civilization edited by emily teeter oriental institute museum puBlications 33 the oriental institute of the university of chicago oi.ucicago.edu Library of Congress Control Number: 2011922920 ISBN-10: 1-885923-82-1 ISBN-13: 978-1-885923-82-0 © 2011 by The University of Chicago. All rights reserved. Published 2011. Printed in the United States of America. The Oriental Institute, Chicago This volume has been published in conjunction with the exhibition Before the Pyramids: The Origins of Egyptian Civilization March 28–December 31, 2011 Oriental Institute Museum Publications 33 Series Editors Leslie Schramer and Thomas G. Urban Rebecca Cain and Michael Lavoie assisted in the production of this volume. Published by The Oriental Institute of the University of Chicago 1155 East 58th Street Chicago, Illinois 60637 USA oi.uchicago.edu For Tom and Linda Illustration Credits Front cover illustration: Painted vessel (Catalog No. 2). Cover design by Brian Zimerle Catalog Nos. 1–79, 82–129: Photos by Anna Ressman Catalog Nos. 80–81: Courtesy of the Ashmolean Museum, Oxford Printed by M&G Graphics, Chicago, Illinois. The paper used in this publication meets the minimum requirements of American National Standard for Information Service — Permanence of Paper for Printed Library Materials, ANSI Z39.48-1984 ∞ oi.ucicago.edu book title TABLE OF CONTENTS Foreword. Gil J.
    [Show full text]