Coupling Assembly, V-Band Sheet Metal Wide Flange, Pneumatic Tube


Book Description

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.




Coupling Assembly, V-Band, Sheet Metal Flange, Pneumatic Tube


Book Description

This specification defines the requirements for a grooved clamp coupling and flanges suitable for joining intermediate pressure and temperature ducting in aircraft air systems. The rigid coupling joint assembly, hereafter referred to as "the joint", shall operate within the temperature range of -65 °F to +800 °F. AS1960 has been reaffirmed to comply with the SAE five-year review policy.







COUPLING, SHEET METAL, 40° V-BAND, WIDE, STANDARD LATCH


Book Description

CHANGE A DIMENSION TO INCREASE THE FLANGE-TO-COUPLING GAP FROM .014 INCH TO .028 INCH, PLUS ADDITIONAL ERRORS.













COUPLING ASSEMBLY, V-RETAINER, HIGH PRESSURE HIGH TEMPERATURE, PNEUMATIC TUBE


Book Description

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.




FLANGE, SHEET METAL, WIDE


Book Description

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.




V-Couplings, Including V-Band and V-Retainer Coupling Assemblies, Flange and Seal Design, Application of


Book Description

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.