EXOTIC FINAL BROUCHER 2013 Final by Annan
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Aero-Flex Corporation 3147 Jupiter Park Circle Suite 2 Jupiter, Florida 33458 (561) 745-2534
Aero-Flex Corporation 3147 Jupiter Park Circle Suite 2 Jupiter, Florida 33458 (561) 745-2534 QUALITY WITHOUT QUESTION Flexible Metal Hose Assemblies Corrugated Metal Hoses that we offer: Hose Master Hoses OmegaFlex Hoses Penflex Hoses ANNUFLEX 700 Series Abrasion Resistant Tubular Braid for 1SBX Braid for 700 Series Hose Annuflex 700 Series Series 300 Hose- Stainless Steel Bronze Braid T304 Bronzeflex 1100 Series Monel Braid Bronze Tubular Braid for Series 400 ChemKing™ Hose Series 400 Stainless Steel Hose Monel Tubular Braid for Series 500 Series 600 Stainless Steel Braid ChlorSafe™ Hose Series 600 Stainless Steel Hose Series 100 - Helical, Stainless Steel, Series 700 Stainless Steel and Extraflex 9000 Series Standard Pitch Hose Compressed Hose Formaflex 900 Series Series 300 - Annular, Stainless Steel, Series 740 Monel Hose Standard Pitch Hose Series 794 Bronze Hose Hydraflex 9400 Series Series 400 - Annular, Bronze, Standard Pitch Hose Series 800 High Pressure Braid Interflex Series 800 Stainless Steel Hose Series 500 - Annular, Monel, Standard Pitch Hose Series 900 High Pressure Braid Masterflex 500 Series Series 900 Stainless Steel Hose Series 800 - Annular, Stainless Steel, Pressureflex HP High Pressure Hose and Braid Series P3 Stainless Steel Braid PressureMax HP Series P3 Stainless Steel Hose Tubular Braid for Series 100 Hose - Stainless Steel T304, T321 and T316 Stainless Steel Braid for Series Tar and Asphalt 400 Helical Hose Tubular Braid for Series 300 Stainless Steel Standard Braid for Ultraflex Braided Braid for Series 300 Series 700 Hose 1/4 - 12 inch 304, 316, & 321 Stainless Steel Single or Double Braid Why Flex Hose? It is comparatively light weight, temperature resistance, has great pressure retention, and allows for variance in fit up and alignment. -
Elemental Fluorine Product Information (Pdf)
Elemental Fluorine Contents 1 Introduction ............................................................................................................... 4 2.1 Technical Application of Fluorine ............................................................................. 5 2.2 Electronic Application of Fluorine ........................................................................... 7 2.3 Fluorine On-Site Plant ............................................................................................ 8 3 Specifications ............................................................................................................ 9 4 Safety ...................................................................................................................... 10 4.1 Maintenance of the F2 system .............................................................................. 12 4.2 First Aid ................................................................................................................ 13 5.1 Chemical Properties ............................................................................................. 14 5.2 Physical Data ....................................................................................................... 15 6 Toxicity .................................................................................................................... 18 7 Shipping and Transport ........................................................................................... 20 8 Environment ........................................................................................................... -
Stainless Steel Selection Guide
TAContentsBLE OF Discovery of Stainless Steel . .page 2 What is Stainless Steel . .page 3 Stainless Steel Classifications . .page 4 • Austenitic . .page 4 • Ferritic . .page 5 • Duplex . .page 5 • Martensitic . .page 6 • Precipitation Hardening . .page 6 Nickel Based Alloys . .page 7 Strength & Heat Treatment . .page 7 The Basics of Corrosion . .page 8 • General or Uniform Corrosion . .page 9 • Galvanic Corrosion . .page 11 • Pitting Corrosion . .page 11 • Crevice Corrosion . .page 13 • Intergranular Corrosion . .page 14 • Stress Corrosion Cracking . .page 15 • Microbiologically Influence Corrosion . .page 17 Welding Stainless Steel . .page 18 Alloy Selection . .page 22 Wrought Stainless Steel Composition . .page 24 Wrought Nickel Alloy Composition . .page 25 Stainless Steel and Nickel Alloy Filler Metal . .page 26 PR“It’sEF stainlessAC steel,E it shouldn’t rust” This is often the kind of statements heard from individuals when discussing a failure of process piping or equipment. This is also an indication of how little is actually understood about stainless steel and the applications where it is used. For years the food, beverage and pharmaceutical industries have used stainless steels in their process piping systems. Most of the time stainless steel components provide satisfactory results. Occasionally a catastrophic failure will occur. The purpose of the information contained within this document is to bring an understanding to stainless steel, it’s uses, and why it will fail under certain conditions. In the following pages we will discuss the different classes of stainless steel, heat treatment, corrosion, welding, and finally material selection. As with any failure, it is imperative the cause of the failure be identified before a proper fix can be recognized. -
Impact of Synthesis Conditions on the Morphology and Crystal Structure of Tungsten Nitride Nanomaterials
RSC Advances View Article Online PAPER View Journal | View Issue Impact of synthesis conditions on the morphology and crystal structure of tungsten nitride Cite this: RSC Adv.,2021,11, 28198 nanomaterials Olivia Wenzel, *a Viktor Rein,b Milena Hugenschmidt, ac Frank Schilling,d Claus Feldmann b and Dagmar Gerthsena Nanocrystalline tungsten nitride (WNx) aggregates and nanosheets are synthesized with a new alkylamine- based synthesis strategy for potential applications in nanoelectronics and catalysis. These applications preferentially require crystalline materials with controlled morphology, which has been rarely demonstrated for WNx nanomaterials in the past. In the synthesis approach presented in this work, the morphology of nanoscale WNx is controlled by long-chained amines that form lyotropic or lamellar phases depending on the surfactant concentration. The structural and chemical properties of the WNx nanomaterials are studied in detail using different electron microscopic techniques in combination with Creative Commons Attribution-NonCommercial 3.0 Unported Licence. electron spectroscopic analyses. Material synthesis and sample preparation for transmission electron microscopy (TEM) were performed in an argon atmosphere (Schlenk line and glovebox). The samples were inserted into the electron microscope via an air-tight TEM transfer holder to protect the material from hydrolysis and oxidation. From the lyotropic phase nanocrystalline WNx aggregates were obtained, which consist of 2.4 Æ 0.8 nm small crystallites of the cubic WNx phase with a composition of WN0.7. The lamellar phase with a higher surfactant concentration yields WNx nanosheets with lateral dimensions up to 500 nm and a mean thickness of 2.1 Æ 1.1 nm. The nanosheets are N rich with a composition Received 8th June 2021 WN – and occur in the hexagonal crystal structure. -
Research a He Edge of Sp Ce Contents I Mission and Accomplishmen Ts
https://ntrs.nasa.gov/search.jsp?R=19640004493 2020-03-11T17:07:03+00:00Z RESEARCH A HE EDGE OF SP CE CONTENTS I MISSION AND ACCOMPLISHMEN TS . .. 1 II EARLIER RESEARCH AIRCRAFT ................. 5 III CONCEPT, HISTORY, AND TECH NICAL CONSIDERATIONS ... 11 IV THE X-15 FLIGH T PROGRAM ................. _ 19 V FUTURE ......... ................... _ 31 ~O';).,IOOO Q. ~ !y f) S 1+) tJ~'(j 1;"v -' ~,I!.-. RESEARCH AT THE EDGE OF SPACE I (/1 5 E F_ '!) CPO ' ~ () I 3 D -1: 1 For sale by the Superintendpnt of Documents, U.S. Government Printing Office 1. ~ ~ : ashington, D.C ., 20402- PriceToCeiits -.-, NASA Ep·9 - - ------- -.--------~~- ~--- .- - -- MISSION AND ACCOMPLISHMENTS , l_ - .-- -- ------ ---- - - I In the fall of 1963, the X-IS completed a series of dental to the goals of the program. The real mis flights at speeds and altitudes never before attained sion of the X-IS is a quest for knowledge. In carry by any vehicle fully controlled by a pilot from launch ing out this mission, the X-IS has made a number to landing on the ground. In the process of making of substantial contributions to the advancement of almost 100 successful flights, it had essentially aerospace science. completed its original program of fli ght research Although primarily an aeronautical vehicle with and had begun to carry out additional aerospace wings and aerodynamic controls, the aircraft travels experiments. well beyond the effective atmosphere on most of its From conception through the phases of design, flights_ At extreme altitudes, the pilot controls the construction, test, and operation, it had rounded out X-IS by reaction jets, like a spacecraft; he is some 11 years of exploring a variety of technological weightless for brief periods, and the research plane and scientific problems. -
Stainless Steel Fasteners – a Systematic Approach to Their Selection
STAINLESS STEEL FASTENERS – A SYSTEMATIC APPROACH TO THEIR SELECTION A DESIGNERS’ HANDBOOK SERIES NO 9003 Produced by Distributed by AMERICAN IRON NICKEL AND STEEL INSTITUTE INSTITUTE STAINLESS STEEL FASTENERS – A SYSTEMATIC APPROACH TO THEIR SELECTION A DESIGNERS’ HANDBOOK SERIES NO 9003 Originally, this handbook was published in 1976 by the Committee of Stainless Steel Producers, American Iron and Steel Institute. The Nickel Institute republished the handbook in 2020. Despite the age of this publication the information herein is considered to be generally valid. Material presented in the handbook has been prepared for the general information of the reader and should not be used or relied on for specific applications without first securing competent advice. The Nickel Institute, the American Iron and Steel Institute, their members, staff and consultants do not represent or warrant its suitability for any general or specific use and assume no liability or responsibility of any kind in connection with the information herein. Nickel Institute [email protected] www.nickelinstitute.org CONTENTS Introduction ................................................3 Fastener Materials ..........................................3 Stainless Steels Identification ................................5 Choosing the Right Type .....................................8 Stainless Steel Fastener Properties ...........................13 Tensile & Yield Strength Shear Strength High- and Low-Temperature Service ..........................16 Magnetic and -
Containing Alloys in Hydrochloric Acid, Hydrogen Chloride and Chlorine (Ceb-3)
CORROSION RESISTANCE OF NICKEL AND NICKEL- CONTAINING ALLOYS IN HYDROCHLORIC ACID, HYDROGEN CHLORIDE AND CHLORINE (CEB-3) A PRACTICAL GUIDE TO THE USE OF NICKEL-CONTAINING ALLOYS NO 279 Distributed by Produced by NICKEL INCO INSTITUTE CORROSION RESISTANCE OF NICKEL AND NICKEL-CONTAINING ALLOYS IN HYDROCHLORIC ACID, HYDROGEN CHLORIDE AND CHLORINE (CEB-3) A PRACTICAL GUIDE TO THE USE OF NICKEL-CONTAINING ALLOYS NO 279 This handbook was first published prior to 1985 by INCO, The International Nickel Company, Inc. Today this company is part of Vale S.A. The Nickel Institute republished the handbook in 2020. Despite the age of this publication the information herein is considered to be generally valid. Material presented in the handbook has been prepared for the general information of the reader and should not be used or relied on for specific applications without first securing competent advice. The Nickel Institute, their members, staff and consultants do not represent or warrant its suitability for any general or specific use and assume no liability or responsibility of any kind in connection with the information herein. Nickel Institute [email protected] www.nickelinstitute.org Nickel-clad steel jacketed reactor used for organic chlorinations. It was built in accordance with the A.P.I. A.S.M.E. code for unfired pressure vessels and operates at a temperature of 650° F, and pressures of 25 lb. per sq. in in the body and 125 Ib per sq. in. in the jacket. Page 2 Resistance of Nickel and High Nickel Alloys to Corrosion by Hydrochloric Acid, Hydrogen Chloride and Chlorine† CONTENTS HYDROCHLORIC ACID ................................................. -
Enghandbook.Pdf
785.392.3017 FAX 785.392.2845 Box 232, Exit 49 G.L. Huyett Expy Minneapolis, KS 67467 ENGINEERING HANDBOOK TECHNICAL INFORMATION STEELMAKING Basic descriptions of making carbon, alloy, stainless, and tool steel p. 4. METALS & ALLOYS Carbon grades, types, and numbering systems; glossary p. 13. Identification factors and composition standards p. 27. CHEMICAL CONTENT This document and the information contained herein is not Quenching, hardening, and other thermal modifications p. 30. HEAT TREATMENT a design standard, design guide or otherwise, but is here TESTING THE HARDNESS OF METALS Types and comparisons; glossary p. 34. solely for the convenience of our customers. For more Comparisons of ductility, stresses; glossary p.41. design assistance MECHANICAL PROPERTIES OF METAL contact our plant or consult the Machinery G.L. Huyett’s distinct capabilities; glossary p. 53. Handbook, published MANUFACTURING PROCESSES by Industrial Press Inc., New York. COATING, PLATING & THE COLORING OF METALS Finishes p. 81. CONVERSION CHARTS Imperial and metric p. 84. 1 TABLE OF CONTENTS Introduction 3 Steelmaking 4 Metals and Alloys 13 Designations for Chemical Content 27 Designations for Heat Treatment 30 Testing the Hardness of Metals 34 Mechanical Properties of Metal 41 Manufacturing Processes 53 Manufacturing Glossary 57 Conversion Coating, Plating, and the Coloring of Metals 81 Conversion Charts 84 Links and Related Sites 89 Index 90 Box 232 • Exit 49 G.L. Huyett Expressway • Minneapolis, Kansas 67467 785-392-3017 • Fax 785-392-2845 • [email protected] • www.huyett.com INTRODUCTION & ACKNOWLEDGMENTS This document was created based on research and experience of Huyett staff. Invaluable technical information, including statistical data contained in the tables, is from the 26th Edition Machinery Handbook, copyrighted and published in 2000 by Industrial Press, Inc. -
ESMA Tech Talk
ESMA Tech Talk August 2006 Volume 103 In This Issue ESMA Opens A New Branch in Deira - Dubai ESMA Industrial Enterprises has a new location in • ESMA Opens A New the heart of the trading zone of Deira. This location, Branch in Deira - which is strategically located close to the Hardware Dubai Market, Electrical Market and Refrigeration Market, is located close to Al Maktoum Hospital. This facility • Parker Extends Its shall cater for the immediate requirements of the Unique ‘Snap- customers unable to visit Jebel Ali. They shall stock Together’ Tubing the standard range of items for a faster response and Clamp Range better service with full access to the main stocks held in their Central Warehouse. For details, please contact them on 04-2293545. • Exotic Material Manifolds Provide Optimal Solutions for Parker Extends Its Unique ‘Snap-Together’ Tubing Aggressive Media Applications Clamp Range ESMA has extended the versatility of its novel one-piece clamp for instrumentation tubing, Snap-Trap®, with a new Contact Us fitting tool and accessories from Parker Instrumentation. ESMA Industrial Enterprises Jebel Ali Free Zone, Snap-Trap® clamps can be fitted in seconds, reducing Dubai – U.A.E. installation time by up to 80% compared with some Tel: +971 4 8839100 alternative systems which require the assembly of up to 12 Fax: +971 4 8839495 parts. Email: [email protected] Already widely used in the Norwegian sector, the clamps are highly resistant to ESMA Industrial Enterprises corrosion and comply with the NORSOK offshore standard. Just two sizes of Snap- Mussafah Indl Area, Trap® handle the spectrum of metric and imperial instrumentation tubing diameters Abu Dhabi – U.A.E. -
Gasket CRITERIA
Gasket CRITERIA. designcriteria 04-14_inside 3/24/2016 1:46 PM Page 1 GasketDesignCriteria TableofContents Page ManufacturingUnits 2 Introduction 3 SectionI-GasketSelection 4 Change Gasket ................................................................................................................................ 6 Sheet Materials ................................................................................................................................ 8 Thermiculite® .................................................................................................................................... 9 PTFE Products - Sigma® ................................................................................................................... 12 PTFE Products - Fluoroseal .............................................................................................................. 14 Flexitallic Flexicarb® .......................................................................................................................... 15 Compressed Fiber Gasket ................................................................................................................ 16 Core4 Sheet Products ...................................................................................................................... 17 Sheet Materials Chemical Compatibility Chart ................................................................................. 18 Insulating Sets ................................................................................................................................. -
High-Performance Alloys for Resistance to Aqueous Corrosion
High-Performance Alloys for Resistance to Aqueous Corrosion Wrought nickel products The INCONEL® Ni-Cr, Ni-Cr-Fe & Ni-Cr-Mo Alloys The INCOLOY® Fe-Ni-Cr Alloys The MONEL® Ni-Cu Alloys 63 Contents Corrosion Problems and Alloy Solutions 1 Corrosion-Resistant Alloys from the Special Metals Group of Companies 4 Alloy Selection for Corrosive Environments 11 Corrosion by Acids 12 Sulfuric Acid 12 Hydrochloric Acid 17 Hydrofluoric Acid 20 Phosphoric Acid 22 Nitric Acid 25 Organic Acids 26 Corrosion by Alkalies 28 Corrosion by Salts 31 Atmospheric Corrosion 35 Corrosion by Waters 37 Fresh and Process Waters 37 Seawater and Marine Environments 38 Corrosion by Halogens and Halogen Compounds 40 Fluorine and Hydrogen Fluoride 40 Chlorine at Ambient Temperature 41 Chlorine and Hydrogen Chloride at High Temperatures 41 Metallurgical Considerations 44 Appendix 49 Corrosion Science and Electrochemistry 50 References 60 Publication number SMC-026 Copyright © Special Metals Corporation, 2000 INCONEL, INCOLOY, MONEL, INCO-WELD, DURANICKEL, 625LCF, 686CPT, 725, 864 and 925 are trademarks of the Special Metals group of companies. Special Metals Corporation www.specialmetals.com Corrosion Problems and Alloy Solutions Due to their excellent corrosion resistance and good mechanical properties, the Special Metals nickel-based alloys are used for a broad range of applications in an equally broad range of industries, including chemical and petrochemical processing, pollution control, oil and gas extraction, marine engineering, power generation, and pulp and paper manufacture. The alloys' versatility and reliability make them the prime materials of choice for construction of process vessels, piping systems, pumps, valves and many other applications designed for service in aqueous and high-temperature environments. -
NASA Facts National Aeronautics and Space Administration
NASA Facts National Aeronautics and Space Administration Dryden Flight Research Center P.O. Box 273 Edwards, California 93523 Voice 661-276-3449 FAX 661-276-3566 [email protected] FS-2003-11-031 DFRC Research Airplane Program X-3 (center) and, clockwise from left: X-1A, D-558-1, XF-92A, X-5, D-558-2, and X-4. NASA photo E-2889. The Research Airplane Program was a joint research effort by the National Aeronautics and Space Administration (NASA--formerly the National Advisory Committee for Aeronautics or NACA) and the military services. It was con- ceived near the end of World War II to perform flight studies with a series of specially-constructed research aircraft in the then-unexplored transonic to low-supersonic characteristics of full-scale aircraft in flight. Although supersonic flight was first achieved in 1947, further research in the program resulted in notable increases in knowledge about the dynamics of piloted flight in winged aircraft at speeds up to and in excess of 4,500 miles per hour and at altitudes up to and greater than 350,000 feet. 1 Yeager was also the pilot when the X-1 reached its maxi- Two general categories of aircraft were obtained for the mum speed, 957 mph. Another Air Force pilot, Lt. Col. research airplane program: (1) those needed to explore new Frank Everest Jr., was credited with taking the X-1 to its areas of performance, such as the X-1, D-558-1, D-558-2, maximum altitude of 71,902 feet. Eighteen pilots in all flew X-1A, X-1B, X-1E, X-2, and X-15; and (2) those required the X-1s.