Test Fixtures for AITM 1-0010 Model: G-AITM-1-0010
This Airbus Test Method determines the residual compressive strength of a composite laminate after it has sustained barely visible impact damage (BVID). This simulates real-world scenarios like bird strikes or tool drops on aircraft structures.
Standards
G818
Technical Specifications
| Specification | Value |
|---|---|
| Model | G-AITM-1-0010 |
| Industry Std | AITM 1-0010 |
| Test Type | Standards |
| Family Id | G818 |
| Compat Machine If | GLUM |
| Interface Description | Optimized for TestResources Load Frames; universal adapters available for legacy systems. |
| Fixture If Gender | GLUF |
Interface & Compatibility
Optimized for TestResources Load Frames; universal adapters available for legacy systems.
Expert Commentary
An Airbus Technical Method for Tensile Testing of Carbon Fiber Reinforced Plastics (CFRP). This is a high-stakes aerospace standard. Our systems must offer precise alignment (Class 1 or better) and thermal chambers capable of −55∘C to +150∘C. The commentary here emphasizes the need for advanced strain measurement, typically via non-contact Video Bolt Extensometry (AVE), to avoid premature specimen failure at the knife-edge interface.