Download or read book Clamp Type Coupling Assemblies for Use with Steam Hoses Rated for Pressures Up to 18 Bar written by British Standards Institute Staff and published by . This book was released on 2006-07-31 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hose connectors, Clamps (mechanical), Flexible pipes, Pipe fittings, Pipe connections, Steam, Water, Pressure, Temperature, Design, Dimensions, Designations, Fasteners
Download or read book DIN EN 14423 Schlaucharmaturen mit Klemmfassung f r Dampf bis 18 bar written by and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book World Translations Index written by and published by . This book was released on 1997 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Clamp Type Coupling Assemblies for Liquefied Petroleum Gas LPG Transfer Hoses written by British Standards Institute Staff and published by . This book was released on 1913-07-31 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hose connectors, Clamps (mechanical), Flexible pipes, Plastics, Rubber, Pipe fittings, Pipe connections, Liquefied petroleum gas, Liquefied natural gas, Natural gas, Materials handling, Pressure, Temperature, Dimensions, Designations, Fasteners, Approval testing
Download or read book Coupling Assembly V Band Sheet Metal Wide Flange Pneumatic Tube written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft pneumatic systems. The coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 °F external ambient to +800 °F internal fluid. This aerospace standard is a departure from the prior qualification practices for the V-band coupling assemblies, AS4751. Prior practice sought to validate this type of assembled coupling design by conducting proof pressure testing but exceeded allowable leakage. AS6369 is to replace AS4751 for future design.
Download or read book Clamp Type Coupling Assemblies for LPG Transfer Hoses written by British Standards Institute Staff and published by . This book was released on 2006-07-31 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hose connectors, Clamps (mechanical), Flexible pipes, Plastics, Rubber, Pipe fittings, Pipe connections, Liquefied petroleum gas, Liquefied natural gas, Natural gas, Materials handling, Pressure, Temperature, Dimensions, Designations, Fasteners, Approval testing
Download or read book COUPLING ASSEMBLY V RETAINER HIGH PRESSURE HIGH TEMPERATURE PNEUMATIC TUBE written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1992 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard establishes the requirements for a grooved clamp coupling, flanges, and seal suitable for joining high pressure and high temperature ducting in aircraft bleed air systems. The rigid coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 to +1200 °F.
Download or read book CLAMP ASSEMBLY SADDLE TYPE CUSHIONED PTFE written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: EXISTING QPL NOTE REVISED TO THE LATEST STANDARDIZED QML REQUIREMENT NOTE. INVENTORIED PARTS DISPOSITION NOTE ADDED. CHANGE BAR NOTE ADDED. GENERAL UPDATES INCLUDED.
Download or read book Couplings Clamp Grooved V Band written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for a V-band grooved clamp couplings that are intended for use on fluid-line tubing joints, tailpipe joints, and accessory mount joints, on flight vehicles or other attachments. The semi-rigid coupling joint assemblies, hereafter referred to as "the joint", shall operate within the temperature ranges specified in their applicable part standards. AS5355B has been reaffirmed to comply with the SAE five-year review policy.
Download or read book CLAMP ASSEMBLY SADDLE TYPE CUSHIONED HIGH TEMPERATURE written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: EXISTING QPL NOTE REVISED TO THE LATEST STANDARDIZED QML REQUIREMENT NOTE. INVENTORIED PARTS DISPOSITION NOTE ADDED. CHANGE BAR NOTE ADDED. GENERAL UPDATES INCLUDED.
Download or read book Coupling Assembly Threadless Flexible Self Locking Fixed Cavity High Conductivity Self Bonding Part Specification written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, high conductive self-bonding coupling assembly which, when installed on defined ferrules, provides a flexible connection for joining ducting and components in pressurized fluid systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for use from -65 to +265 °F at 130 psi nominal operating pressures and for the service life of the aircraft system. FAR 23.954, FAR 25.901, FAR 25.954 and FAR 25.981 certification requirements have identified the need for high current capable flexible fluid assembled couplings. The coupling assembly does not require inspection and maintenance to remain current capable for the life of the aircraft.This specification provides two test philosophies necessary for low pressure couplings: 1EME/lightning testing of assembled couplings to demonstrate electrostatic capabilities are retained through simulated service life test sequences to meet commercial airplane FAR 25.981 certification requirements. 2Grouping and goal posting of coupling test specimens based on size and material similarities.The assembled coupling's intended application and usage is for, but not limited to, commercial and military aircraft. Components defined herein and qualified to the performance capabilities and regulatory compliance requirements will support their use in fuel and other fluid conveyance systems.This specification requires manufactures to be qualified and accredited to Performance Review Institute (PRI)/National Aerospace and Defense Contractors Accreditation Program (Nadcap) requirements. New part specification to supersede AS5830.
Download or read book Coupling Fuel Flexible Variable Cavity Threaded Type With Ferrules written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2006 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits. Revision C' adds QPL/QML requirements and provides a general document update.
Download or read book Coupling Fuel Rigid Threaded Type written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2011 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification defines the requirements for a threaded rigid coupling assembly, which utilizes ferrule type machined tube end fittings, to join tubing and components in aircraft fuel, vent, and other systems. This coupling assembly is designed for use from 65 to 200 °F and at 125 psig operating pressure. Revised to specify lower bending stress for sizes -48 and above, relocated strain gages near the holding clamp, clarified o-ring criteria and revised repeated assembly requirements for sizes -06 thru -12.
Download or read book CLAMP ASSEMBLY SADDLE TYPE CUSHIONED PHOSPHATE ESTER FLUID RESISTANT written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: EXISTING QPL NOTE REVISED TO THE LATEST STANDARDIZED QML REQUIREMENT NOTE. INVENTORIED PARTS DISPOSITION NOTE ADDED. CHANGE BAR NOTE ADDED. GENERAL UPDATES INCLUDED.
Download or read book COUPLING CLAMP GROOVE V BAND FORGED 6 400 9 400 11 400 FLANGE OD written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2012 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: AS977 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. 1THIS STANDARD IS FOR USE WITH STANDARDS FOR DRIVES AND ACCESSORIES AS964, 966, AND 968 THRU 971. 2DIMENSIONS: ALL LINEAR DIMENSIONS ARE IN INCHES. 3BREAK SHARP EDGES 0.0030.015 4SURFACE TEXTURE: ANSI B46.1-1962 5PROVISIONS FOR CLOSING AND LOCKING COUPLING ARE OPTIONAL BUT MUST FALL WITHIN ENVELOPE SHOWN. 6WHEN FULLY OPEN, COUPLING SHALL BE CAPABLE OF PASSING FREELY OVER FLANGES PER AS964, 966, AND 968 THRU 971 OF THE CORRESPONDING SIZE WITHOUT DISENGAGING BOLT. 7COUPLING SHALL OPEN AND CLOSE BY TURNING BOLT. 8BOLT SHALL PIVOT FREELY IN SUCH MANNER THAT NO BENDING MOMENT IS INDUCED IN BOLT AS CLAMP OPENS AND CLOSES. 9BOLT TIGHTENING TORQUE SHALL BE MARKED ON COUPLING. LUBRICANT SHALL BE SPECIFIED IN INSTALLATION INSTRUCTIONS. 10COUPLING SHALL BE CAPABLE OF SUSTAINING RATED AXIAL LOAD WITHOUT PERMANENT DEFORMATION. 11WEIGHT AND OVERHUNG MOMENT OF ATTACHING ACCESSORIES SHALL NOT EXCEED MAXIMUM VALUES SPECIFIED IN AS969, 970, AND 971. 12SEE AIR869 FOR APPLICATION OF V-BAND COUPLINGS.THIS IS A DESIGN STANDARD NOT TO BE USED AS A PART NUMBER.
Download or read book COUPLING CLAMP GROOVE V BAND 6 400 9 400 11 400 FLANGE OD written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2006 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY. THIS IS A DESIGN STANDARD. NOT TO BE USED AS A PART NUMBER. 1THIS STANDARD IS FOR USE WITH STANDARDS FOR DRIVES AND ACCESSORIES AS964, 966, AND 968 THRU 971. 2DIMENSIONS: ALL LINEAR DIMENSIONS ARE IN INCHES. 3REMOVE BURRS AND SHARP EDGES. 4SURFACE TEXTURE: USAS B46.1. 5LATCH ELEMENTS ARE OPTIONAL WITHIN ENVELOPE SHOWN. 6WHEN FULLY OPEN, COUPLING SHALL BE CAPABLE OF DISASSEMBLY FROM FLANGES WITHOUT REMOVAL OF NUT FROM BOLT. 7THE NUT SHALL BE SELF-LOCKING TYPE IN ACCORDANCE WITH MIL-N-25027. 8COUPLING SHALL BE CAPABLE OF SUSTAINING RATED AXIAL LOAD WITHOUT PERMANENT DEFORMATION. WEIGHT AND OVERHUNG MOMENT OF ATTACHING ACCESSORIES SHALL NOT EXCEED THE LARGEST VALUE SPECIFIED IN AS969, AS970, AND AS971. 9FASTENING STRAP TO STRAP END OR STRAP TO RETAINER SEGMENT SHALL BE BY RESISTANCE WELDING OR RIVETING. 10SAE AIR869 FOR APPLICATION OF V-BAND COUPLINGS. 11STRAP ENDS SHALL BE STRAIGHT BETWEEN POINT OF TANGENCY WITH LATCH OR TRUNNION AND POINT OF TANGENCY WITH STRAP AS SHOWN. 12NUT TIGHTENING TORQUE SHALL BE MARKED ON COUPLING. LUBRICANT SHALL BE SPECIFIED IN INSTALLATION INSTRUCTIONS.
Download or read book Coupling Assembly Threadless Flexible Fixed Cavity Current Carrying Self Bonding Procurement Specification written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88).This aerospace specification is a departure from prior qualification practices for assembled couplings. Prior practice sought to validate this type of assembled coupling design by conducting a sequence of tests on sets of coupling assemblies. There were multiple test sequences and each was conducted on a different set of coupling assemblies. Each of these test sequences challenged a particular design feature of the coupling assembly. No single coupling assembly was expected to survive all of the required tests.FAR 23.954, FAR 25.954 and FAR 25.981 certification requirements have identified the need for high-current capable flexible fluid couplings. The coupling assembly does not require inspection and maintenance to remain current capable for the life of the aircraft.It is important to simulate the in-service wear and damage experienced by the assembled coupling if it is to remain capable of carrying current for the life of the aircraft. The test procedures in this specification simulate a worst case wear and damage condition for the assembled couplings.Interchangeability of vendor parts must be qualified by design, test and/or analysis.CAUTION: Although the AS5830 coupling and sleeve will fit on AS1650 ferrules due to the use of common O-rings, the combinations of these parts are not qualified. Using AS5830 parts on AS1650 ferrules may result in leakage and/or premature failure of the joint and does not produce a high current capable joint.WARNING: The use of AS1650 parts with AS5830 ferrules is not qualified. Assembly of worn AS1650 parts with AS5830 ferrules may be possible but could result in leakage and/or premature failure of the joint and does not produce a high current capable joint. AS5830 has been reaffirmed to comply with the SAE five-year review policy.
