T/TMAC 205-2025 Active Group standards

T/TMAC 205-2025 Aeroengine blade made of nickel-based high-temperature alloy

Publish Date: 1970-01-01 Implement Date: 1970-01-01 For services related to genuine standard inquiry, procurement, translation, and other related services in China, please Contact Us

Price: $ 29.00

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Basic Information

Standard Code: T/TMAC 205-2025

Standard Type: Group standards

Standard Status: Active

is_force_gb: no

CCS Name: -

ICS Name: -

Publish Date: 1970-01-01

Implement Date: 1970-01-01

Scope

This document specifies the technical requirements, test methods, quality assessment, inspection rules, marking, packaging, transportation, and storage for nickel-based high-temperature alloys used in aero-engine blades. This document is applicable to the design, production, inspection, and use of nickel-based high-temperature alloys for aero-engine blades.

Development Information

Word Count: 15 Thousand words

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