Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 12,24 MB
Release : 2014
Category :
ISBN :
This SAE Aerospace Information Report (AIR) is intended to inform users of the proper use, application, and installation of V-Couplings, which will perform satisfactorily only if they are properly installed. This document informs the user of the correct manner of applying and installing V-Couplings and also cautions against improper use. Many of the referenced standards have been replaced by new SAE and other standards.More information and expanded explanations have been added.
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 31,37 MB
Release : 2006
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ISBN :
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.
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 46,65 MB
Release : 2012
Category :
ISBN :
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.
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 18,13 MB
Release : 2017
Category :
ISBN :
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.
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 18,82 MB
Release : 2015
Category :
ISBN :
This SAE Aerospace Standard establishes the requirements for a V-retainer 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. This standard was revised to include PRI-QPL requirements and to update specification and standard references.
Author :
Publisher :
Page : 860 pages
File Size : 35,34 MB
Release :
Category : United States
ISBN :
Author : Jon R. Mancuso
Publisher : CRC Press
Page : 616 pages
File Size : 32,83 MB
Release : 1999-04-23
Category : Technology & Engineering
ISBN : 9780824799502
"Second Edition provides new material on coupling ratings, general purpose couplings versus special purpose couplings, retrofitting of lubricated couplings to nonlubricated couplings, torsional damping couplings, torquemeter couplings, and more."
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 50,39 MB
Release : 2013
Category :
ISBN :
AS1895/21A HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 18,90 MB
Release : 1994
Category :
ISBN :
Author : G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher :
Page : 0 pages
File Size : 48,63 MB
Release : 2013
Category :
ISBN :
AS1895/22B HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
