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ISO 7257:2016 PDF

Aircraft — Hydraulic tubing joints and fittings — Rotary flexure test

First page of standard ISO 7257:2016Open preview (PDF)Aircraft — Hydraulic tubing joints and fittings — Rotary flexure test
Title (English):
ISO 7257:2016

Aircraft — Hydraulic tubing joints and fittings — Rotary flexure test

Document status:
Active
Format:
Electronic (PDF)
Number of pages:
12
Publication date:
May 31, 2016
Edition:
ISO IS 7257 edition 2 version 1
ICS:
49.080
Description (English):

ISO 7257:2016 specifies a flexure test procedure 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 with high-strength hydraulic tubes of various alloys such as corrosion resistant steel, Nimonic?[1], titanium and aluminium alloy hydraulic tube for use on commercial and military aircraft. A mean stress is applied by holding system pressure in the specimens and then flexing in a rotary bending test machine. [1] Nimonic? is the trademark of a product supplied by Special Metals Corporation. This information is given for the convenience of users of this document and does not constitute an endorsement by ISO of the product named. Equivalent products can be used if they can be shown to lead to the same results.

Technical details

Technical committee
ISO/TC 20/SC 10 - Aerospace fluid systems and components
SKU
ISO 7257:2016

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