Table 2 Tensile test values of the first to fifth groups of crimping samples and the corresponding failure types of crimping assembly.
From: Mathematical model for the tensile strength of the crimping assembly of aviation wiring harness end
Gear (#) | Maximum tensile strength (N) | Average (N) | Type of destruction |
|---|---|---|---|
1 | 73.2/76.4/74.5/73.8/76.1 | 74.8 | Complete break |
2 | 80.1/82.3/81.5/81.1/82.1 | 81.4 | Complete break |
3 | 83.3/83.7/83.6/82.8/83.5 | 83.4 | Partial break |
4 | 78.5/78.9/79.6/78.8/79.1 | 79.0 | Partial break |
5 | 24.7/25.3/24.7/25.8/26.1 | 25.3 | Disengage |
