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SAE International - ARP4146D

Coiled Tubing - Titanium Alloy, Hydraulic Applications, Aerospace

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Organization: SAE International
Publication Date: 21 June 2018
Status: active
description:

This SAE Aerospace Recommended Practice (ARP) addresses the design, installation, and testing of coiled tube assemblies using Ti-3Al-2.5V cold worked, stress relieved (CWSR) tubing per AMS4945. It... View More

Document History

ARP4146D
June 21, 2018
Coiled Tubing - Titanium Alloy, Hydraulic Applications, Aerospace
This SAE Aerospace Recommended Practice (ARP) addresses the design, installation, and testing of coiled tube assemblies using Ti-3Al-2.5V cold worked, stress relieved (CWSR) tubing per AMS4945. It...

References

This document references:
AIR1379 - PRESTRESSING (AUTOFRETTAGING) OF HYDRAULIC TUBING LINES
Published by SAE International on July 1, 1977
This AIR is intended to describe and document a process presently in use for proof testing, which at the same time improves the fatigue life of 304 1/8 hard CRES and 3A1-2.5V CWSR titanium hydraulic...
This document references:
AMS4945 - TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3Al - 2.5V, Texture Controlled, 105,000 psi (724 MPa) Yield Strength
Published by SAE International on January 1, 1989
This specification covers a titanium alloy in the form of seamless, cold worked, stress relieved, and texture controlled (See 8.1 ) tubing.
This document references:
ARP4752 - AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
Published by SAE International on September 1, 1994
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system that is fitted to a commercial transport aircraft.
This document references:
ARP4925 - AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS
Published by SAE International on January 1, 1996
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system fitted to a commercial transport rotorcraft.
This document references:
ARP584 - COILED TUBING
Published by SAE International on March 1, 1960
This recommended practice encompasses design, analysis, fabrication, and installation of pressurized plain metal tubing used in fluid power systems to provide relative motion. Specific data given are...
This document references:
AS4076 - Contractile Strain Ratio Testing of Titanium Hydraulic Tubing
Published by SAE International on January 7, 2013
This SAE Aerospace Standard establishes the requirements and procedures for Contractile Strain Ratio (CSR) testing of cold-worked and stress-relieved titanium tubing such as Ti-3AI-2.5V tubing per...
This document references:
AS4401 - Separable Fittings, Permanent Fittings, Tubing, Fluid Systems 8000 psi Qualification Test Standard For
Published by SAE International on January 7, 2013
This Performance Standard covers the Qualification Test Requirements for separable fittings, permanent fittings, and tubing suitable for use in 8000 psi aerospace fluid power systems. The standard...
This document references:
AS4467 - Standardization, Hydraulic Tube Walls
Published by SAE International on January 7, 2013
This SAE Aerospace Standard (AS) defines a series of standardized tube walls to be used for high pressure hydraulic tubing. These tube walls are applicable to all homogenous tube materials (i.e.,...
This document references:
AS5440 - Hydraulic Systems, Aircraft, Design and Installation Requirements For
Published by SAE International on April 1, 1998
This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
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