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BSI - BS EN 3084

Pipe Couplings 8 Degrees 30' in Titanium Alloy - Unions, Welded End Threaded for Repair

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Organization: BSI
Publication Date: 18 October 2001
Status: active
Page Count: 10
ICS Code (Aerospace fluid systems and components): 49.080

Document History

BS EN 3084
October 18, 2001
Pipe Couplings 8 Degrees 30' in Titanium Alloy - Unions, Welded End Threaded for Repair
A description is not available for this item.

References

This document references:
EN 2424 - Aerospace series - Marking of aerospace products
Published by CEN on May 1, 2008
A description is not available for this item.
This document references:
EN 2491 - Aerospace series - Molybdenum disulphide dry lubricants - Coating methods
Published by CEN on June 1, 2011
This European Standard defines the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion...
This document references:
EN 3274 - Aerospace series - Pipe coupling 8 degrees 30' - Thread end - Geometric configuration
Published by CEN on October 1, 2010
This standard specifies the characteristics of the thread end for 8°30' pipe couplings, nominal pressure up to 28 000 kPa, for aerospace applications.
This document references:
EN 3275 - Aerospace series - Pipe coupling 8°30' up to 28 000 kPa Dynamic beam seal - Metric series - Technical specification
Published by CEN on May 1, 2019
This European standard specifies the required characteristics, inspection and test methods, quality assurance and procurement requirements for metric series 8°30’ dynamic beam seal pipe couplings,...
This document references:
EN 2656 - Aerospace Series - Pipe Coupling - Coupling End, Welded - Geometric Configuration
Published by CEN on September 1, 2001
A description is not available for this item.
This document references:
EN 3311 - Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bars for machining - D < 300 mm - 900 MPa ≤ Rm ≤ 1 160 MPa
Published by CEN on December 1, 2023
This document specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Bars for machining D ≤ 300 mm 900 MPa ≤ Rm ≤ 1 160 MPa for aerospace applications.
This document references:
EN 3314 - Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm
Published by CEN on April 1, 2019
This document specifies the requirements relating to: Titanium alloy TI-P64001 Solution treated and aged Bar for machining D ≤ 75 mm for aerospace applications.
This document references:
ISO 5855-3 FRENCH - Aéronautique et espace - Filetage MJ - Partie 3: Dimensions limites pour raccordements de systèmes de fluides
Published by ISO on October 15, 1999
A description is not available for this item.
This document references:
ISO 5855-3 - Aerospace - MJ Threads - Part 3: Limit Dimensions for Fittings for Fluid Systems
Published by ISO on October 15, 1999
This part of ISO 5855 specifies limit dimensions of MJ threads for fluid systems fittings for aerospace construction.
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