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ISO 11119-3:2020

Current

Current

The latest, up-to-date edition.

Gas cylinders Design, construction and testing of refillable composite gas cylinders and tubes Part 3: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with non-load-sharing metallic or non-metallic liners or without liners

Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

23-11-2020

€165.00
Excluding VAT

This document specifies minimum requirements for the material, design, construction and workmanship, manufacturing processes, examination and testing at time of manufacture for:

type 4 composite fully wrapped cylinders or tubes with a non-load sharing liner and composite reinforcement on both the cylindrical portion and the dome ends;

type 5 fully wrapped cylinders or tubes without liners and with a test pressure of less than 60 bar and composite reinforcement on both the cylindrical portion and the dome ends;

water capacities up to 450 l;

for the storage and conveyance of compressed or liquefied gases;

cylinders and tubes with composite reinforcement of carbon fibre, aramid fibre or glass fibre (or a mixture thereof) within a matrix;

a minimum design life of 15 years.

Cylinders and tubes manufactured and tested according to this document are not intended to contain toxic, oxidizing or corrosive gases.

This document does not address the design, fitting and performance of removable protective sleeves.

NOTE 1 References to cylinders in this document include composite tubes if appropriate.

NOTE 2 ISO 11439 applies to cylinders intended for use as fuel containers on natural gas vehicles and ISO 11623 covers periodic inspection and re-testing of composite cylinders.

DocumentType
Standard
Pages
48
ProductNote
THIS STANDARD ALSO REFERS:CGA C14
PublisherName
International Organization for Standardization
Status
Current
Supersedes

Standards Relationship
DS/ISO 11119-3:2020 Identical
BS ISO 11119-3:2020 Identical

SAE AS6858 Installation of Fuel Cell Systems in Large Civil Aircraft

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