MH/T 3022-2011
Infrared thermography for composite component of aircraft (English Version)

Standard No.
MH/T 3022-2011
Language
Chinese, Available in English version
Release Date
2011
Published By
Professional Standard - Civil Aviation
Status
Latest
MH/T 3022-2011
Scope
This standard specifies the requirements and quality control for near-surface defects in civil aircraft composite components using infrared thermal imaging (hereinafter referred to as thermal imaging detection). This standard is applicable to the use of infrared thermal imaging methods to detect delamination, debonding, voids, foreign matter and liquid intrusion in composite components (including laminated panels, honeycomb structures and sandwich structures) and the joints between panels and support structures in civil aircraft. Detection of defects. This standard does not apply to the detection of damage to the sandwich layer and defects in the joint between the sandwich layer and the other side of the laminate (away from the testing equipment).

MH/T 3022-2011 Referenced Document

  • GB/T 12604.9 Non-destructive testing—Terminology—Infrared thermography*2021-08-20 Update
  • GB/T 20737 Non-destructive testing-General terms and definitions
  • MH/T 3001 Qualification and certification of personnelin aircraft for nondestructive testing*2012-04-26 Update

MH/T 3022-2011 history

  • 2011 MH/T 3022-2011 Infrared thermography for composite component of aircraft
Infrared thermography for composite component of aircraft



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