Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This recommended practice establishes the method for qualification testing of tube joints and fittings using the rotary or planar flexure test method described in ARP 1185. This qualification test method requires the determination of S-N type curves except that tube deflections are plotted versus the number of test cycles. This replaces flexure testing to a single stress level as specified in MIL-F-18280, B and C revisions.
QUALIFICATION OF HYDRAULIC TUBE JOINTS TO SPECIFIED FLEXURE FATIGUE REQUIREMENTS
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This recommended practice establishes the method for qualification testing of tube joints and fittings using the rotary or planar flexure test method described in ARP 1185. This qualification test method requires the determination of S-N type curves except that tube deflections are plotted versus the number of test cycles. This replaces flexure testing to a single stress level as specified in MIL-F-18280, B and C revisions.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This recommended practice establishes the method for qualification testing of tube joints and fittings using the rotary or planar flexure test method described in ARP 1185. This qualification test method requires the determination of S-N type curves except that tube deflections are plotted versus the number of test cycles. This replaces flexure testing to a single stress level as specified in MIL-F-18280, B and C revisions.
SAE Aerospace Standards
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 676
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 676
Book Description
Criteria for Current and Advanced Aircraft Hydraulic Tubing
Author: Society of Automotive Engineers. Committee G-3
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Hydraulic Tubing - Qualification Test Requirements
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This international standard establishes flexure and pressure impulse test procedures for determining and classifying the fatigue strengths of bent aircraft hydraulic tubing. The procedures are intended for use with high- and low-pressure system assemblies for evaluation of new materials or for qualification purposes. MA2006 has been reaffirmed to comply with the SAE five-year review policy.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This international standard establishes flexure and pressure impulse test procedures for determining and classifying the fatigue strengths of bent aircraft hydraulic tubing. The procedures are intended for use with high- and low-pressure system assemblies for evaluation of new materials or for qualification purposes. MA2006 has been reaffirmed to comply with the SAE five-year review policy.
The Shock and Vibration Digest
Author:
Publisher:
ISBN:
Category : Shock (Mechanics)
Languages : en
Pages : 594
Book Description
Publisher:
ISBN:
Category : Shock (Mechanics)
Languages : en
Pages : 594
Book Description
Flexure Testing of Hydraulic Tubing Joints and Fittings
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This SAE Aerospace Recommended Practice (ARP) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints.The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 (21Cr-6Ni-9Mn) steel or AMS 4944 (3AL-2.5V) titanium.A mean stress is applied by holding system pressure in the specimens and flexing in a rotary or planar bending test machine. This document has been determined to contain basic and stable technology which is not dynamic in nature.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This SAE Aerospace Recommended Practice (ARP) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints.The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 (21Cr-6Ni-9Mn) steel or AMS 4944 (3AL-2.5V) titanium.A mean stress is applied by holding system pressure in the specimens and flexing in a rotary or planar bending test machine. This document has been determined to contain basic and stable technology which is not dynamic in nature.
Flexure Testing of Hydraulic Tubing Joints and Fittings by Planar Resonant Vibration (Free-Free Beam)
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This Aerospace Information Report (AIR) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints.The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 steel, AMS 4944 titanium and MIL-T-7081 aluminum alloy, mounted as free-free resonant beams.Of particular advantage are the inherent simplicity of test setup, minimum restraint from a test fixture, low power requirements, short test duration, and ease of varying stress level. This document has been determined to contain basic and stable technology which is not dynamic in nature.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This Aerospace Information Report (AIR) establishes flexure test procedures to determine and classify the fatigue strengths of reconnectable or permanent hydraulic tube joints.The procedure is intended for conducting flexure tests of fittings and joints for hydraulic tubing materials such as AMS 5561 steel, AMS 4944 titanium and MIL-T-7081 aluminum alloy, mounted as free-free resonant beams.Of particular advantage are the inherent simplicity of test setup, minimum restraint from a test fixture, low power requirements, short test duration, and ease of varying stress level. This document has been determined to contain basic and stable technology which is not dynamic in nature.
SAE Technical Paper Series
Author:
Publisher:
ISBN:
Category : Automobiles
Languages : en
Pages : 786
Book Description
Online version: Technical papers portion of the SAE Digital Library references thousands of SAE Technical Papers covering the latest advances and research in all areas of mobility engineering including ground vehicle, aerospace, off-highway, and manufacturing technology. Sample coverage includes fuels and lubricants, emissions, electronics, brakes, restraint systems, noise, engines, materials, lighting, and more. Your SAE service includes detailed summaries, complete documents in PDF, plus document storage and maintenance
Publisher:
ISBN:
Category : Automobiles
Languages : en
Pages : 786
Book Description
Online version: Technical papers portion of the SAE Digital Library references thousands of SAE Technical Papers covering the latest advances and research in all areas of mobility engineering including ground vehicle, aerospace, off-highway, and manufacturing technology. Sample coverage includes fuels and lubricants, emissions, electronics, brakes, restraint systems, noise, engines, materials, lighting, and more. Your SAE service includes detailed summaries, complete documents in PDF, plus document storage and maintenance
S.A.E. Transactions
Author: Society of Automotive Engineers
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
Book Description
Beginning in 1985, one section is devoted to a special topic
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 748
Book Description
Beginning in 1985, one section is devoted to a special topic
Automotive Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1270
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1270
Book Description