Outgassing of Technical Polymers PEEK, Kapton, Vespel & Mylar
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Arxiv:1810.10187V3 [Physics.Ins-Det] 10 Jan 2019 to Minimize Longitudinal Heat flow While Satisfying One’S Electrical Impedance and Shape (E.G
Properties of selected structural and flat flexible cabling materials for low temperature applications M. Daala,∗, N. Zobrista, N. Kellarisd,e, B. Sadouletb, M. Robertsonc aDepartment of Physics, University of California, Santa Barbara CA 93106-9530 bDepartment of Physics, University of California, Berkeley CA 94720-7300 cDepartment of Physics, University of California, Davis CA 95616-8677 dDepartment of Mechanical Engineering, University of Colorado Boulder, 80309-0427 eMaterials Science and Engineering Program, University of Colorado, Boulder, 80309-0596 Abstract We present measurements of the low temperature thermal conductivity for materials useful in the construction of cryogenic supports for scientific instrumentation and in the fabrication of flat flexible cryogenic cabling. The materials we measure have relatively low thermal conductivity. We present a method for measuring the heat transfer coefficient of flat cabling and show, using an example, that the thermal conductivity of a flex cable is reasonably well predicted by composing the thermal conductivities of its constituent material layers. Room temperature physical and mechanical data is given for the materials studied, as well as an overview of relevant materials science and manufacturing details. Materials include Timet Ti 15-3 and Ti 21S, Materion alloy vit105 (LM105) in amorphous state, ATI Metals Nb-47Ti, Johnson Matthey nitinol (NiTi), Mersen graphite grade 2020, DuPont Pyralux coverlay and Vespel SCP-5050, and Fralock Cirlex polyimide sheets. All data is in the temperature range 0:05 to 2 K, and up to 5 K for SCP-5050. Keywords: Thermal conductivity, Heat transfer coefficient, Cryogenic, Structural materials, Support structures, Flat flexible cables, Superconducting cables, Low temperature, Titanium alloys, Bulk metallic glass, vit105, LM105, Cirlex, Vespel, Pyralux, NbTi, Ti 15-3-3-3, Ti 21S, Nitinol, NiTi, Transition Temperature 1. -
DUPONT DATA BOOK SCIENCE-BASED SOLUTIONS Dupont Investor Relations Contents 1 Dupont Overview
DUPONT DATA BOOK SCIENCE-BASED SOLUTIONS DuPont Investor Relations Contents 1 DuPont Overview 2 Corporate Financial Data Consolidated Income Statements Greg Friedman Tim Johnson Jennifer Driscoll Consolidated Balance Sheets Vice President Director Director Consolidated Statements of Cash Flows (302) 999-5504 (515) 535-2177 (302) 999-5510 6 DuPont Science & Technology 8 Business Segments Agriculture Electronics & Communications Industrial Biosciences Nutrition & Health Performance Materials Ann Giancristoforo Pat Esham Manager Specialist Safety & Protection (302) 999-5511 (302) 999-5513 20 Corporate Financial Data Segment Information The DuPont Data Book has been prepared to assist financial analysts, portfolio managers and others in Selected Additional Data understanding and evaluating the company. This book presents graphics, tabular and other statistical data about the consolidated company and its business segments. Inside Back Cover Forward-Looking Statements Board of Directors and This Data Book contains forward-looking statements which may be identified by their use of words like “plans,” “expects,” “will,” “believes,” “intends,” “estimates,” “anticipates” or other words of similar meaning. All DuPont Senior Leadership statements that address expectations or projections about the future, including statements about the company’s strategy for growth, product development, regulatory approval, market position, anticipated benefits of recent acquisitions, timing of anticipated benefits from restructuring actions, outcome of contingencies, such as litigation and environmental matters, expenditures and financial results, are forward looking statements. Forward-looking statements are not guarantees of future performance and are based on certain assumptions and expectations of future events which may not be realized. Forward-looking statements also involve risks and uncertainties, many of which are beyond the company’s control. -
Dupont™ Kalrez® KVSP™ Valve Stem Packing Technical Guidelines and Design to Improve Process Control and Minimize Fugitive Emissions
DuPont™ Kalrez® KVSP™ Valve Stem Packing Technical Guidelines and Design to Improve Process Control and Minimize Fugitive Emissions Technical Information—Rev. 4, March 2019 Introduction DuPont™ Kalrez® Valve Stem Packing (KVSP™) systems can help to significantly reduce fugitive emissions and improve process control through the innovative use of Kalrez® perfluoroelastomer parts combined with other proven packing materials. Graphite packing systems can meet fugitive emissions requirements but restrict valve movement, leading to inconsistent process control. Polytetrafluoroethylene (PTFE) has excellent process control response characteristics but cannot contain fugitive emissions when temperature cycling is involved in conjunction with operational cycling. Kalrez® packing systems overcome these deficiencies, as well as reducing leak rates to near-bellows performance. Kalrez® is chemically an elastomeric PTFE derived from tetrafluoroethylene (TFE), the same base monomer. It provides a unique combination of chemical resistance and inertness like PTFE, but with a higher temperature service limit and no tendency to cold flow. The chemical structure remains cross-linked and stable at high temperatures and does not move under load or deformation. Its resiliency and memory provide improved sealing for control valve stems. Using Kalrez® V-rings backed up with more rigid components of carbon fiber-reinforced PTFE (DuPont™ Vespel® CR-6100) has proven to be a major advancement in improving process control and reducing leakage to less than 1 ppm, or below the plant’s background level. Kalrez® perfluoroelastomer packing systems increase a valve’s ability to react quickly and smoothly to process changes (Figure 1). Kalrez® KVSP™ reduces process control variability to the control system’s capability, resulting in improvements to both yield and product quality on specification. -
Space Environment Exposure Results from the Misse 5 Polymer Film Thermal Control Experiment on the International Space Station
SPACE ENVIRONMENT EXPOSURE RESULTS FROM THE MISSE 5 POLYMER FILM THERMAL CONTROL EXPERIMENT ON THE INTERNATIONAL SPACE STATION Sharon K.R. Miller(1), Joyce A. Dever(2) (1)NASA Glenn Research Center, 21000 Brookpark Rd. MS 309-2, Cleveland, OH, 44135, U.S.A., Phone: 1-216-433- 2219, E-mail: [email protected] (2)NASA Glenn Research Center, 21000 Brookpark Rd. MS 106-1, Cleveland, OH, 44135, U.S.A., Phone: 1-216-433- 6294, E-mail: [email protected] ABSTRACT Station Experiment (MISSE) 1, was designed to expose tensile specimens of a small selection of polymer films It is known that polymer films can degrade in space on ram facing and non-ram facing surfaces of MISSE 1 due to exposure to the environment, but the magnitude [2]. A more complete description of the NASA Glenn of the mechanical property degradation and the degree Resarch Center MISSE 1-7 experiments is contained in to which the different environmental factors play a role a publication by Kim de Groh et al [3]. The PFTC was in it is not well understood. This paper describes the expanded and flown as one of the experiments on the results of an experiment flown on the Materials nadir facing side of MISSE 5 in order to examine the International Space Station Experiment (MISSE) 5 to long term effects of the space environment on the determine the change in tensile strength and % mechanical properties of a wider variety of typical elongation of some typical polymer films exposed in a spacecraft polymers exposed to the anti-solar or nadir nadir facing environment on the International Space facing space environment. -
Application of Polyimide Actuator Rod Seals
(NASA-CR- 120878) APPLICATION OF POLYIiIDE N72-245306 ACTUATOR ROD SEALS AoH. Hatermann, et al (Boeing Co,, Seattle, Wash,) 30 Jan. 1972 177 p CSCL 11A Unclas G3/15 28867 I CR-I 20878 D6-54351 A A~ APPLICATION OF POLYIMIDE ACTUATOR ROD SEALS by A. W. Waterman, B. F. Gay, E. D. Robinson, S. K. Srinath, W. G. Nelson THE BOEING COMPANY prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Lewis Research Center Contract NAS3-14317 ! William F. Hady, Project Manager 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. CR- 120878 4. Title and Subtitle 5. Report Date APPLICATION OF POLYIMIDE ACTUATOR ROD SEALS January 30, 1972 6. Performing Organization Code 7. Author(s) A. W. Waterman, B. F. Gay, E. D. Robinson, 8. Performing Organization Report No. S. K. Srinath, and W. G. Nelson D6-54351 9. Performing Organization Name and Address 10. Work Unit No. YON 1347 The Boeing Company, Commercial Airplane Group 11. Contractor Grant No. P.O. Box 3707, Seattle, Washington 98124 NAS3-14317 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address CONTRACTOR REPORT National Aeronautics and Space Administration 7/1/70-1/30/72 Washington, D.C. 20546 14. Sponsoring Agency Code 15. Supplementary Notes Project Manager: W. F. Hady, Fluid System Component Division, NASA Lewis Research Center, Cleveland, Ohio 16. Abstract Development of polyimide two-stage hydraulic actuator rod seals for application in high-performance aircraft was accomplished. The significant portion of the effort was concentrated on optimization of the chevron and K-section second-stage seal geometries to satisfy the requirements for operation at 4500K (3500F) with dynamic pressure loads varying between 1.379 x 106 N/m2 (200 psig) steady-state and 1.043 x 107 N/m2 (1500 psig) impulse cycling. -
DE-FOA-0001954 Modification 20
FINANCIAL ASSISTANCE FUNDING OPPORTUNITY ANNOUNCEMENT ADVANCED RESEARCH PROJECTS AGENCY – ENERGY (ARPA-E) U.S. DEPARTMENT OF ENERGY SOLICITATION ON TOPICS INFORMING NEW PROGRAM AREAS SBIR/STTR Announcement Type: Modification 19 20 Funding Opportunity No. DE-FOA-0001954 CFDA Number 81.135 FOA Issue Date: December 20, 2018 FOA Close Date: Open continuously until otherwise amended. Application Due Date: See Targeted Topics Table for topic-specific application due dates. Total Amount to Be Awarded Approximately $114.75 million, subject to the availability of appropriated funds to be shared between FOAs DE-FOA-0001953 and DE-FOA-0001954. See Targeted Topics Table for topic-specific information. Anticipated Awards ARPA-E may issue one, multiple, or no awards under this FOA. Awards may vary between $100,000 and $3,721,115 . See Targeted Topics Table for topic-specific award amount requirements. • For eligibility criteria, see Section III.A – III.D of the FOA. • For cost share requirements under this FOA, see Section III.E of the FOA. • To apply to this FOA, Applicants must register with and submit application materials through ARPA-E eXCHANGE (https://arpa-e-foa.energy.gov/Registration.aspx). For detailed guidance on using ARPA-E eXCHANGE, see Section IV.F.1 of the FOA. • Applicants are responsible for meeting the submission deadline associated with each Targeted Topic. Applicants are strongly encouraged to submit their applications at least 48 hours in advance of the Targeted Topic submission deadline. • For detailed guidance on compliance and responsiveness criteria, see Sections III.F.1 through III.F.3 of the FOA. Questions about this FOA? Check the Frequently Asked Questions available at http://arpa-e.energy.gov/faq . -
Materials Matter™
MATERIALS MATTER™ Lower Levelized Cost of Energy (LCOE) through DuPont Innovation MATERIALS MATTER™ FOR BETTER LONG-TERM PV SYSTEM PERFORMANCE AND HIGHER FINANCIAL RETURNS DuPont has a rich heritage of innovation and leadership in the PV industry. It all began more than 55 years ago when our scientists created the first purified silicon for Bell Labs for use in the PV market. Since then, our broad and growing portfolio of materials has enabled significant leaps in module efficiency, reliability and overall system cost reduction. We are committed to continually driving technology innovation and have been granted nearly 200 PV worldwide patents since 2008, with more than 1,300 patent applications currently pending. In 2011, DuPont spent $2 billion U.S. dollars on research and development, with a significant portion focused on advancing the efficiency, lifetime and cost competitiveness of solar energy. We’ve also invested hundreds of millions of U.S. dollars in supply expansions over the past few years to support long-term industry growth. Today, DuPont offers the broadest materials portfolio time-tested for decades in more than five trillion in PV and provides six of the eight most critical materials panel-hours of outdoor PV field installations all around for manufacturing solar modules. These materials are the world. That’s trillions more hours of real PV exposure not only innovative, they have delivered demonstrable than other material providers in the industry. results, including: nearly doubling cell efficiency over 12 years; providing greater reliability and extending Looking ahead, we aim to increase efficiency well beyond system lifetime—with 30+ years of proven backsheet 20% and extend system lifetime toward 40 years, while performance; and reducing overall system cost with increasing system safety and reducing cost. -
Material Safety Data Sheet
Du Pont Page 1 Material Safety Data Sheet ---------------------------------------------------------------------- "VESPEL" POLYIMIDE PARTS AND SHAPES ALL IN SYNONYM LIST VSP001 VSP001 Revised 26-JAN-2007 Printed 02/11/2009 ---------------------------------------------------------------------- Substance ID :130000026921 ---------------------------------------------------------------------- CHEMICAL PRODUCT/COMPANY IDENTIFICATION ---------------------------------------------------------------------- Material Identification "VESPEL" is a registered trademark of DuPont. Corporate MSDS Number : DU003855 Tradenames and Synonyms "VESPEL" SP-1, "VESPEL" SP-3, "VESPEL" SP-21, "VESPEL" SP-22, "VESPEL" SP-26 "VESPEL" SP-101, "VESPEL" SP-102, "VESPEL" SP-202 # "VESPEL" SP-211, "VESPEL" SP-214, "VESPEL" SP-215, "VESPEL" SP-221, "VESPEL" SP-224, "VESPEL" SP-262, "VESPEL" SP-2515, "VESPEL" SP-2624 "VESPEL" ST-2010, "VESPEL" ST-2010G, "VESPEL" ST-2010H, "VESPEL" ST-2030, Company Identification MANUFACTURER/DISTRIBUTOR DuPont Engineering Polymers 1007 Market Street Wilmington, DE 19898 PHONE NUMBERS Product Information : 1-800-441-7515 Transport Emergency : 1-800-424-9300 Medical Emergency : 1-800-441-3637 ---------------------------------------------------------------------- COMPOSITION/INFORMATION ON INGREDIENTS ---------------------------------------------------------------------- Components Material CAS Number % Du Pont VSP001 Page 2 Material Safety Data Sheet POLY-N,N'-(p,p'-OXYDIPHENYLENE) 25038-81-7 30-100 PYROMELLITIMIDE GRAPHITE 7782-42-5 0-65 -
Material Chemical & Physical Properties Tensile
THIS GUIDE IS Go to INTERACTIVE ePlastics.com CLICK ON EACH ITEM TO GO TO ITS DESCRIPTION MATERIAL COST CHEMICAL & PHYSICAL TENSILE STRENGTH PROPERTIES UV RESISTANCE & FLEXURAL STRENGTH VISIBLE LIGHT TRANSMISSION IMPACT STRENGTH CHEMICAL RESISTANCE & HARDNESS MAXIMUM HEAT DEFLECTION DIELECTRIC PROPERTIES OPERATING TEMPERATURE TEMPERATURE EXPRESS DISCLAIMER: THE INFORMATION PRESENTED IN OUR MATERIAL SELECTION GUIDE AND OUR WEB SITES IS BASED ON OUR 99 YEARS PROVIDING PLASTIC MATERIALS AND SOLUTIONS. WE SINCERELY HOPE YOU FIND THE INFORMATION HELPFUL IN YOUR SEARCH FOR ANSWERS. THE INFORMATION SOURCES ARE FROM THE WIDE SELECTION OF PLASTIC MANUFACTURERS THAT WE DISTRIBUTE FOR. THERE ARE MANY MORE PLASTICS AVAILABLE THAN LISTED HEREIN AND MAY CONTAIN ADDITIVES THAT CAN ALTER THE PHYSICAL PROPERTIES. THE EXPRESS INTENTION OF RIDOUT PLASTICS IS TO HELP YOU NARROW YOUR SEARCH, NOT TO PRESCRIBE A "FITNESS OF USE" FOR ANY PARTICULAR USE. AS WITH ALL NEW APPLICATIONS, ONE MUST TEST THE PLASTIC FOR THE USE AND THEN MAKE APPROVALS OF YOUR OWN. SEPT 2013 VER. 1 CHEMICAL & PHYSICAL BACK TO NEXT PROPERTIES START PAGE THERMOPLASTIC/ THERMOPLASTIC THERMOSET THERMOSET AMORPHOUS FIBERGLASS/HIGH PRESSURE AMORPHOUS SEMI-CRYSTALLINE POLYAMIDE-IMIDES LAMINATES Advantages Advantages Advantages Advantages . High Temperature resistance . Softens over a wide . Opaque . Highest temperature (+200°F) temperature range with no . Better chemical resistance resistance (+400°F) . Fire retardant class 1 sharp melting point . Better resistance to stress . High chemical resistance . Strength to weight ratio Good adhesive bonding cracking . High weight-bearing abilities . Dimensionally Stable Good formability . Better fatigue resistance and mechanical stability under . Thermal Conductivity . Ease of machining . Good for structural weight- high pressure and temperature Disadvantages . -
Report of Contributions
MT25 Conference 2017 - Timetable, Abstracts, Orals and Posters Report of Contributions https://indico.cern.ch/e/MT25-2017 MT25 Conferenc … / Report of Contributions 3D Electromagnetic Analysis of Tu … Contribution ID: 5 Type: Poster Presentation of 1h45m 3D Electromagnetic Analysis of Tubular Permanent Magnet Linear Launcher Tuesday, 29 August 2017 13:15 (1h 45m) A short stroke and large thrust axial magnetized tubular permanent magnet linear launcher (TPMLL) with non-ferromagnetic rings is presented in this paper. Its 3D finite element (FE) models are estab- lished for sensitivity analyses on some parameters, such as air gap thickness, permanent magnet thickness, permanent magnet width, stator yoke thickness and four types of permanent magnet material, ferrite, NdFeB, AlNiCO5 and Sm2CO17 are conducted to achieve greatest thrust. Then its 2D finite element (FE) models are also established. The electromagnetic thrusts calculated by 2D and 3D finite element method (FEM) and got from prototype test are compared. Moreover, the prototype static and dynamic tests are conducted to verify the 2D and 3D electromagnetic analysis. The FE software FLUX provides the interface with the MATLAB/Simulink to establish combined simulation. To improve the accuracy of the simulation, the combined simulation between the model of the control system in Matlab/Simulink and the 3D FE model of the TPMLL in FLUX is built in this paper. The combined simulation between the control system and the 3D FE modelof the TPMLL is built. A prototype is manufactured according to the final designed dimensions. The photograph of the developed TPMLL prototype with thrust sensor and the magnetic powder brake as the load are shown. -
2 0 0 1 a N N U a L R E P O
2001 ANNUAL REPORT DuPont at 200 In 2002, DuPont celebrates its 200th anniversary. The company that began as a small, family firm on the banks of Delaware’s Brandywine River is today a global enterprise operating in 70 countries around the world. From a manufacturer of one main product – black powder for guns and blasting – DuPont grew through a remarkable series of scientific leaps into a supplier of some of the world’s most advanced materials, services and technologies. Much of what we take for granted in the look, feel, and utility of modern life was brought to the marketplace as a result of DuPont discoveries, the genius of DuPont scientists and engineers, and the hard work of DuPont employees in plants and offices, year in and year out. Along the way, there have been some exceptional constants. The company’s core values of safety, health and the environment, ethics, and respect for people have evolved to meet the challenges and opportunities of each era, but as they are lived today they would be easily recognizable to our founder. The central role of science as the means for gaining competitive advantage and creating value for customers and shareholders has been consistent. It would be familiar to any employee plucked at random from any decade of the company’s existence. Yet nothing has contributed more to the success of DuPont than its ability to transform itself in order to grow. Whether moving into high explosives in the latter 19th century, into chemicals and polymers in the 20th century, or into biotechnology and other integrated sciences today, DuPont has always embraced change as a means to grow. -
Heat Set Creases in Polyethylene Terephthalate (PET) Sheets to Enable Origami-Based Applications
Smart Materials and Structures PAPER Heat set creases in polyethylene terephthalate (PET) sheets to enable origami-based applications To cite this article: Brandon Sargent et al 2019 Smart Mater. Struct. 28 115047 View the article online for updates and enhancements. This content was downloaded from IP address 128.187.112.27 on 23/10/2019 at 15:35 Smart Materials and Structures Smart Mater. Struct. 28 (2019) 115047 (13pp) https://doi.org/10.1088/1361-665X/ab49df Heat set creases in polyethylene terephthalate (PET) sheets to enable origami-based applications Brandon Sargent1 , Nathan Brown1, Brian D Jensen1, Spencer P Magleby1, William G Pitt2 and Larry L Howell1 1 Department of Mechanical Engineering, Brigham Young University, Provo, UT, 84602, United States of America 2 Department of Chemical Engineering, Brigham Young University, Provo, UT, 84602, United States of America E-mail: [email protected] Received 7 May 2019, revised 26 August 2019 Accepted for publication 1 October 2019 Published 24 October 2019 Abstract Polyethylene terephthalate (PET) sheets show promise for application in origami-based engineering design. Origami-based engineering provides advantages that are not readily available in traditional engineering design methods. Several processing methods were examined to identify trends and determine the effect of processing of PET sheets on the crease properties of origami mechanisms in PET. Various annealing times, temperatures, and cooling rates were evaluated and data collected for over 1000 samples. It was determined that annealing temperature plays the largest role in crease response. An increase in the crystallinity of a PET sheet while in the folded state likely increases the force response of the crease in PET sheets.