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ASD-STAN PREN 3264

Aerospace series - Pipe coupling 8°30' in titanium alloy - Thrust wire nuts

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Organization: ASD-STAN
Publication Date: 1 December 2016
Status: active
Page Count: 7
scope:

This standard specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium alloy, for aerospace applications.

Nominal pressure: up to 28 000 kPa

Temperature range: - 55 °C to 135 °C

Document History

ASD-STAN PREN 3264
December 1, 2016
Aerospace series - Pipe coupling 8°30' in titanium alloy - Thrust wire nuts
This standard specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: – 55...
PREN 3264
October 31, 2009
Aerospace series Pipe coupling 8 degrees 30' in titanium alloy Thrust wire nuts
A description is not available for this item.
PREN 3264
March 1, 1995
Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Swivel Nuts
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 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 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 4032 - Aerospace Series - Pipe Coupling 8 Degrees 30´ in Titanium Alloy - Thrust Wire
Published by CEN on September 1, 2001
A description is not available for this item.
This document references:
EN 9133 - Aerospace series - Quality Management Systems - Qualification Procedure for Aerospace Standard Products
Published by CEN on June 1, 2018
General This document defines a system for the qualification of standard products for aviation, space, and defenc applications. It defines the principles that shall be adhered to when carrying out...
This document references:
DIN EN 3314 - Luft- und Raumfahrt - Titanlegierung TI-P64001 - Loesungsgeglueht und ausgelagert - Stangen zum Zerspanen - D ≤ 75 mm; Deutsche und Englische Fassung EN 3314:2019
Published by DIN on July 1, 2019
A description is not available for this item.
This document references:
ISO 286-2 - Geometrical product specifications (GPS) - ISO code system for tolerances on linear sizes - Part 2: Tables of standard tolerance classes and limit deviations for holes and shafts TECHNICAL CORRIGENDUM 1
Published by ISO on August 1, 2013
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.
This document references:
ISO 8788 - Aerospace — Nuts, metric — Tolerances of form and position
Published by ISO on May 1, 2020
This document defines the tolerances of form and position of metric nuts meant for aerospace construction. These tolerances comply with ISO 1101, ISO 2692 and ISO 5459.
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