Stress Corrosion Cracking Control Measures
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Engine Components and Filters: Damage Profiles, Probable Causes and Prevention
ENGINE COMPONENTS AND FILTERS: DAMAGE PROFILES, PROBABLE CAUSES AND PREVENTION Technical Information AFTERMARKET Contents 1 Introduction 5 2 General topics 6 2.1 Engine wear caused by contamination 6 2.2 Fuel flooding 8 2.3 Hydraulic lock 10 2.4 Increased oil consumption 12 3 Top of the piston and piston ring belt 14 3.1 Hole burned through the top of the piston in gasoline and diesel engines 14 3.2 Melting at the top of the piston and the top land of a gasoline engine 16 3.3 Melting at the top of the piston and the top land of a diesel engine 18 3.4 Broken piston ring lands 20 3.5 Valve impacts at the top of the piston and piston hammering at the cylinder head 22 3.6 Cracks in the top of the piston 24 4 Piston skirt 26 4.1 Piston seizure on the thrust and opposite side (piston skirt area only) 26 4.2 Piston seizure on one side of the piston skirt 27 4.3 Diagonal piston seizure next to the pin bore 28 4.4 Asymmetrical wear pattern on the piston skirt 30 4.5 Piston seizure in the lower piston skirt area only 31 4.6 Heavy wear at the piston skirt with a rough, matte surface 32 4.7 Wear marks on one side of the piston skirt 33 5 Support – piston pin bushing 34 5.1 Seizure in the pin bore 34 5.2 Cratered piston wall in the pin boss area 35 6 Piston rings 36 6.1 Piston rings with burn marks and seizure marks on the 36 piston skirt 6.2 Damage to the ring belt due to fractured piston rings 37 6.3 Heavy wear of the piston ring grooves and piston rings 38 6.4 Heavy radial wear of the piston rings 39 7 Cylinder liners 40 7.1 Pitting on the outer -
Leak Test Requirements
METRIC/SI (ENGLISH) NASA TECHNICAL STANDARD NASA-STD-7012 Office of the NASA Chief Engineer Approved: 2019-03-05 LEAK TEST REQUIREMENTS APPROVED FOR PUBLIC RELEASE – DISTRIBUTION IS UNLIMITED NASA-STD-7012 DOCUMENT HISTORY LOG Status Document Change Approval Date Description Revision Number Baseline 2019-03-05 Initial Release APPROVED FOR PUBLIC RELEASE – DISTRIBUTION IS UNLIMITED 2 of 54 NASA-STD-7012 FOREWORD This NASA Technical Standard is published by the National Aeronautics and Space Administration (NASA) to provide uniform engineering and technical requirements for processes, procedures, practices, and methods that have been endorsed as standard for NASA programs and projects, including requirements for selection, application, and design criteria of an item. This NASA Technical Standard is approved for use by NASA Headquarters and NASA Centers and Facilities, and applicable technical requirements may be cited in contract, program, and other Agency documents. It may also apply to the Jet Propulsion Laboratory (a Federally Funded Research and Development Center (FFRDC)), other contractors, recipients of grants and cooperative agreements, and parties to other agreements only to the extent specified or referenced in applicable contracts, grants, or agreements. This NASA Technical Standard establishes uniform use of leak test requirements for NASA vehicles, subsystems and their components, and payloads. This NASA Technical Standard was developed by the Johnson Space Center (JSC) Requirements, Test, and Verification Panel (RTVP) supported by JSC Engineering. To provide additional technical expert guidance, the RTVP established a Technical Discipline Working Group that involved many known space industry experts in leak testing from Glenn Research Center, Kennedy Space Center, Langley Research Center, and Marshall Space Flight Center (MSFC) in particular. -
Outside Diameter Initiated Stress Corrosion Cracking Revised Final White Paper", Developed by AREVA and Westinghouse Under PWROG Program PA-MSC-0474
Program Management Office PWROG 102 Addison Road Connecticut 06095 q .Windsor, ko'ners-- PA-MSC-0474 Project Number 694 October 14, 2010 OG-10-354 U.S. Nuclear Regulatory Commission Document Control Desk Washington, DC 20555-0001 Subject: PWR Owners Group For Information Only - Outside Diameter Initiated Stress Corrosion Crackin2 Revised Final White Paper, PA-MSC-0474 This letter transmits two (2) non-proprietary copies of PWROG document "Outside Diameter Initiated Stress Corrosion Cracking Revised Final White Paper", developed by AREVA and Westinghouse under PWROG program PA-MSC-0474. This document is being submitted for information only. No safety evaluation (SE) is expected and therefore, no review fees should be incurred. This white paper summarizes the recent occurrences of ODSCC of stainless steel piping identified at Callaway, Wolf Creek and SONGS. Available operating experience (OE) at units that have observed similar phenomena is summarized as well to give a better understanding of the issue. Each of the key factors that contribute to ODSCC was considered along with the reported operating experience to perform a preliminary assessment of areas that may be susceptible to ODSCC. Also a qualitative evaluation was performed to determine whether ODSCC of stainless steel piping represents an immediate safety concern. This white paper is meant to address the issue of ODSCC of stainless steel systems for the near term. I&E guidelines are currently being developed through the PWROG to provide long term guidance. Correspondence related to this transmittal should be addressed to: Mr. W. Anthony Nowinowski, Manager Owners Group, Program Management Office Westinghouse Electric Company 1000 Westinghouse Drive, Suite 380 Cranberry Township, PA 16066 U.S. -
Tech Spotlight
impact.qxd 3/12/04 11:25 AM Page 1 TECH SPOTLIGHT Impact Testing notched side by the moving striker by the metrology of the parts that are Wayne Hayward pendulum, and the energy needed to subject to the most wear and tear, and Tinius Olsen Testing Machine Co. break off the free end is the measure some machines were manufactured Horsham, Pennsylvania of the impact strength. This article before strict adherence to the specifi- discusses the equipment, calibration, cations in ASTM E23 was deemed to and procedures for Charpy testing. be critical. Accurate results are not pos- he purpose of impact testing is to sible if the equipment is not operating Tdetermine the toughness of a ma- Impact testing equipment according to the specification; there- terial by measuring the amount of en- Instruments for impact testing of fore, it is strongly recommended that ergy absorbed by a specimen as it frac- metals have been manufactured com- the impact tester be calibrated and/or tures while being struck by a striker mercially since the 1900’s, and several verified by an accredited calibration pendulum moving at high speed. The manufacturers of testing equipment service at regular intervals. impact strength is defined as the max- meet the requirements of ASTM E23, imum amount of energy that can be “Standard Test Methods for Notched Instrument calibration absorbed by the specimen without Bar Impact Testing of Metallic Mate- A calibration swing is performed to fracture. rials.” The standard provides dimen- ensure that energy losses due to In the Charpy impact test, a notch sion and tolerance requirements for windage and friction in the bearings is placed in the specimen. -
Fracture Control Plan for Jsc Space-Flight Hardware
JSC 25863C FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE JSC Fracture Control Board Public Release Statement: This document has been reviewed for Proprietary, SBU, and Export Control (ITAR/EAR) and has been determined to be nonsensitive. It has been released to the public via the NASA Scientific and Technical Information (STI) Process DAA NF 1676 TN56113. March 2018 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas 77058 Verify correct revision before use at https://qmsmasterlist.jsc.nasa.gov/Home.aspx/Organization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igitally signed by MARY SCHWARTZ MARY SCHWARTZ Date: 2018.04.26 08:14:22 -05'00' ($.HYLQ:LQGRZ 'DWH 'LUHFWRU(QJLQHHULQJ 6HHFRYHUIRUIXOOGLVFORVXUH9HULI\FRUUHFWUHYLVLRQEHIRUHXVHDW KWWSVTPVPDVWHUOLVWMVFQDVDJRY+RPHDVS[2UJDQL]DWLRQ 3DJHRI JSC 25863, FRACTURE CONTROL PLAN FOR JSC SPACE-FLIGHT HARDWARE, REVISION C March 30, 2018 DOCUMENT HISTORY LOG Document Date Originator Approval Description Revision Fracture Control Plan Basic May 1992 for JSC Flight Hardware Fracture Control Plan August A for JSC Flight 1998 Hardware Fracture Control Plan April B for JSC 2009 Space-flight Hardware Moe Shoeb Per EA-CCB- Changes reflect the CR/D-0239 Fracture Control March methodology of latest C 2018 release of NASA-STD 5019A and SSP 52005F. -
Forms of Corrosion Uniform Corrosion
Chapter 4 Forms of corrosion Uniform corrosion In such type of corrosion there is a uniform decrease in the volume of the metal due to direct contact with the surrounding environment. Examples Dissolvation of Zn, Al metal in acids and Pb metal in base. Atmospheric corrosion Atmospheric corrosion take place due to direct contact between metal and atmosphere Types of atmosphere: Gas type: contain mainly oxygen gas( 23% W / W) and water vapor. Liquid type: contain mainly water and dissolved oxygen. iron rust Atmospheric corrosion involve formation of metal oxide layer when metal in direct contact with its surrounding environment. Example: Formation of iron rust due to contact with air Fe + air, H2O Fe(OH)2 Fe2O3 Fe2O3 .3H2O is Iron rust (reddish brown ppt.) Oxide layers Protective Non Protective Non active active Non porous porous Ex: Zn, Al, Ni Ex: iron rust Rate of atmospheric corrosion depends on Nature of metal or alloy. Nature of oxide layer. Factors affecting atmospheric corrosion: Type of metal or alloy. Type of atmosphere (dust, humidity, pollutant. Water vapor, gases,…) Temperature( as T increase as rate increase) Time: The extent of corrosion increases with increased time Surface Condition: more roughness, more corrosion The presence of foreign matter influence the speed of corrosion PLAY ACTIVE FIGURE Galvanic corrosion Take place due to the contact between bimetallic couple exposed to the same environment due to the potential difference. Mechanism of galvanic corrosion: For two different metals M1 and M2 when exposed to the same corrosive environment, if M1 is more active than M2 M1 M2 Anodic reaction: M M n+ + ne- (n=1, 2, 3, …) Anodic metal will be corroded. -
Introduction to Corrosion Your Friendly TSC Corrosion Staff
Introduction to Corrosion Your Friendly TSC Corrosion Staff: Daryl Little Ph.D. Materials Science & Engineering [email protected] 303-445-2384 Lee Sears Ph.D. Materials Science & Engineering [email protected] 303-445-2392 Jessica Torrey Ph.D. Materials Science & Engineering [email protected] 303-445-2376 Roger Turcotte, PE, CPS Materials Engineer [email protected] 303-445-2383 What is Corrosion? CORROSION IS DEFINED AS THE DETERIORATION OF A MATERIAL AND/OR ITS PROPERTIES CAUSED BY A REACTION WITH ITS ENVIRONMENT. Why is Corrosion a Major Concern? First and Most Important- Public Safety! • June 28, 1983: Mianus River Bridge, Greenwich, CT (TIME photo archive) • Northbound 3-lane section of I-95 bridge collapsed, killing 3 people • “Pin and Hanger” design was compromised when pin was displaced due to extensive corrosion of load-bearing components, amplified by salt from road maintenance. • Inadequate maintenance procedures were also cited as a contributing factor. • Subsequent to this failure, extensive inspections were conducted on this type of bridge across the country, and design modification were made to prevent catastrophic failures of this kind. First and Most Important- Public Safety! • April 28,1988, Aloha Airlines 737 Accident • 18 feet of cabin skin ripped off, resulting in the death of a flight attendant and many injuries • Attributed to corrosion fatigue Reclamation Case Study- Folsom Dam • Spillway gate No. 3 was damaged beyond repair, but no flooding occurred. • Replacement of No. 3 and repair of other gates cost ~$20 million and required 40% drainage of reservoir • Cause of failure: Increasing corrosion at the trunnion pin-hub interface raised the coefficient of friction and, therefore, the bending stress in the strut and the axial force in the brace exceeded limits. -
Leak Detection in Natural Gas and Propane Commercial Motor Vehicles Course
Leak Detection in Natural Gas and Propane Commercial Motor Vehicles Course July 2015 Table of Contents 1. Leak Detection in Natural Gas and Propane Commercial Motor Vehicles Course ............................................... 1 1.1 Introduction and Overview ............................................................................................................................ 1 1.2 Welcome ........................................................................................................................................................ 1 1.3 Course Goal .................................................................................................................................................... 1 1.4 Training Outcomes ......................................................................................................................................... 1 1.5 Training Outcomes (Continued) ..................................................................................................................... 2 1.6 Course Objectives .......................................................................................................................................... 2 1.7 Course Topic Areas ........................................................................................................................................ 2 1.8 Course Overview ............................................................................................................................................ 2 1.9 Module One: Overview of CNG, LNG, -
Deep Sea Dive Ebook Free Download
DEEP SEA DIVE PDF, EPUB, EBOOK Frank Lampard | 112 pages | 07 Apr 2016 | Hachette Children's Group | 9780349132136 | English | London, United Kingdom Deep Sea Dive PDF Book Zombie Worm. Marrus orthocanna. Deep diving can mean something else in the commercial diving field. They can be found all over the world. Depth at which breathing compressed air exposes the diver to an oxygen partial pressure of 1. Retrieved 31 May Diving medicine. Arthur J. Retrieved 13 March Although commercial and military divers often operate at those depths, or even deeper, they are surface supplied. Minimal visibility is still possible far deeper. The temperature is rising in the ocean and we still don't know what kind of an impact that will have on the many species that exist in the ocean. Guiel Jr. His dive was aborted due to equipment failure. Smithsonian Institution, Washington, DC. Depth limit for a group of 2 to 3 French Level 3 recreational divers, breathing air. Underwater diving to a depth beyond the norm accepted by the associated community. Limpet mine Speargun Hawaiian sling Polespear. Michele Geraci [42]. Diving safety. Retrieved 19 September All of these considerations result in the amount of breathing gas required for deep diving being much greater than for shallow open water diving. King Crab. Atrial septal defect Effects of drugs on fitness to dive Fitness to dive Psychological fitness to dive. The bottom part which has the pilot sphere inside. List of diving environments by type Altitude diving Benign water diving Confined water diving Deep diving Inland diving Inshore diving Muck diving Night diving Open-water diving Black-water diving Blue-water diving Penetration diving Cave diving Ice diving Wreck diving Recreational dive sites Underwater environment. -
Liquid Copper™ Block Seal Intake & Radiator Stop Leak
RISLONE TECHNICAL BULLETIN Tech Bulletin #: TB-31109-2 Page 1 of 2 st Date 1 Issued: February 13, 2009 Date Revised: November 10, 2016 Rislone® Liquid Copper™ Block Part #: 31109 ISO 9001 CERTIFIED Seal Intake & Radiator Stop Leak ™ LIQUID COPPER BLOCK SEAL INTAKE & RADIATOR STOP LEAK Rislone® Liquid Copper™ Block Seal Intake & Radiator Stop Leak seals larger leaks regular stop leaks won’t. One step formula permanently repairs leaks in gaskets, radiators, heater cores, intake manifolds, blocks, heads and freeze plugs. Use on cars, trucks, vans, SUV’s and RV’s. One “1” Step Sealer contains an antifreeze compatible sodium silicate liquid glass formula, so no draining of the cooling system is required. It will not harm the cooling system when used properly. Use with all types of antifreeze including conventional green or blue (Silicate- based ) and extended life red/orange or yellow (OAT / HOAT) coolant. NOTE: Cooling systems that are dirty or partially clogged should be flushed before usage. DIRECTIONS: 1. Allow engine to cool. Ensure your engine is cool enough so radiator cap can safely be Part Number: 31109 removed. UPC Item: 0 69181 31109 1 2. Shake well. Pour LIQUID COPPER™ BLOCK UPC Case: 1 00 69181 31109 8 SEAL directly into radiator. If using in a small Bottle Size: 510 g cooling system, such as 4 cylinders with no air Bottle Size (cm): 6,6 x 6,6 x 18,8 conditioning, install ½ of bottle. Bottle Cube: 819 TIP: When you don’t have access to the Case Pack: 6 bottles per case radiator cap: for quickest results remove top Case Size (cm): 20,6 x 14 x 20,1 hose where it connects to the top of the Case Cube: 5797 radiator and install product in hose. -
Galvanic Corrosion
10 GALVANIC CORROSION X. G. ZHANG Teck Metals Ltd., Mississauga, Ontario, Canada A. Introduction graphite, are dispersed in a metal, or on a ship, where the B. Definition various components immersed in water are made of different C. Factors in galvanic corrosion metal alloys. In many cases, galvanic corrosion may result in D. Material factors quick deterioration of the metals but, in other cases, the D1. Effects of coupled materials galvanic corrosion of one metal may result in the corrosion D2. Effect of area protection of an attached metal, which is the basis of cathodic D3. Effect of surface condition protection by sacrificial anodes. E. Environmental factors Galvanic corrosion is an extensively investigated subject, E1. Effects of solution as shown in Table 10.1, and is qualitatively well understood E2. Atmospheric environments but, due to its highly complex nature, it has been difficult to E3. Natural waters deal with in a quantitative way until recently. The widespread F. Polarity reversal use of computers and the development of software have made G. Preventive measures great advances in understanding and predicting galvanic H. Beneficial effects of galvanic corrosion corrosion. I. Fundamental considerations I1. Electrode potential and Kirchhoff’s law I2. Analysis B. DEFINITION I3. Polarization and resistance I4. Potential and current distributions When two dissimilar conducting materials in electrical con- References tact with each other are exposed to an electrolyte, a current, called the galvanic current, flows from one to the other. Galvanic corrosion is that part of the corrosion that occurs at the anodic member of such a couple and is directly related to the galvanic current by Faraday’s law. -
Code of Practice 32
CODE OF PRACTICE 32 THE SAFE FILLING OF BEVERAGE GAS CYLINDERS REVISION 2: 2014 CODE OF PRACTICE 32 THE SAFE FILLING OF BEVERAGE GAS CYLINDERS Revision 2: 2014 Copyright © 2014 by British Compressed Gases Association. First printed as BCGA Guidance Note 4, 1997. All rights reserved. No part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, without permission from the publisher: BRITISH COMPRESSED GASES ASSOCIATION Registered office: 4a Mallard Way, Pride Park, Derby, UK. DE24 8GX Company Number: 71798, England Website: www.bcga.co.uk ISSN 0260 - 4809 BCGA CP 32 – Revision 2 PREFACE The British Compressed Gases Association (BCGA) was established in l971, formed out of the British Acetylene Association, which existed since l901. BCGA members include gas producers, suppliers of gas handling equipment and users operating in the compressed gas field. The main objectives of the Association are to further technology, to enhance safe practice, and to prioritise environmental protection in the supply and use of industrial gases, and we produce a host of publications to this end. BCGA also provides advice and makes representations on behalf of its Members to regulatory bodies, including the UK Government. Policy is determined by a Council elected from Member Companies, with detailed technical studies being undertaken by a Technical Committee and its specialist Sub-Committees appointed for this purpose. BCGA makes strenuous efforts to ensure the accuracy and current relevance of its publications, which are intended for use by technically competent persons. However this does not remove the need for technical and managerial judgement in practical situations.