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aluminium alloy changes alloy aluminum alloy materials plates introduction core changes key performance indicators performance comparison gas fuel heating value propolis products indicator tubes scopethis standard
GB/T 29503-2020 in English

GB/T 29503-2020 in English

VALID

Aluminium alloy stretched plates

  • Issued on:2020-06-02
  • Implemented on:2021-04-01
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $450.00
$437.00

《GB/T 29503-2020铝合金预拉伸板》由TC243(全国有色金属标准化技术委员会)归口,TC243SC1(全国有色金属标准化技术委员会轻金属分会)执行,主管部门为中国有色金属工业协会。


Introduction

Core changes in the standard revision

Technical dimension GB/T29503-2013 GB/T29503-2020 Impact of changes
Alloy grade 5 types including 2017/7A04 8 types including 2D12/7055 Expand the scope of applicable materials for aerospace
Hydrogen content control Not specified New liquid/solid hydrogen measurement requirements Improve material metallurgical quality
Fracture toughness 3 indicators New LT/TL/SL three-dimensional tests Improve crack growth resistance evaluation

Detailed explanation of key performance indicators

Performance comparison of typical grades

7050T7451 plate has a longitudinal fracture toughness KIC requirement of ≥25.0 MPa·m1/2 in the thickness range of 152-178mm, which is 12% higher than the 2013 version. The newly added 7055T7751 has a compressive yield strength of 593MPa in the thickness range of 12-38mm, making it suitable for high-load structural parts.


Implementation suggestions

  1. The stress corrosion sensitivity factor (SCF) requirements of 7xxx series alloys should be clearly marked when purchasing materials
  2. Fractograph inspection must be carried out on plates with a thickness of >25mm
  3. In the design of new models, priority should be given to newly added high-strength corrosion-resistant alloys such as 2D70/7A85

Technology evolution analysis

This standard reflects three development directions of aluminum alloy materials: 1) Improving metallurgical quality by controlling hydrogen content; 2) Introducing a three-dimensional fracture toughness evaluation system; 3) Strengthening environmental adaptability indicators (newly added corrosion test methods in Appendix B/C). The conductivity requirement of 7475T7351 is increased to ≥23.2MS/m, corresponding to 40%IACS, meeting the electromagnetic compatibility requirements of the new generation of aircraft.

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