3-Point Bend Loading and Support Anvils
CP112749 | 3-Point Bend Loading and Support Anvils
3-point bend loading and support anvils set to ISO 14125 & EN2746 (Flexural) and ISO 14130 & EN2377 (ILSS) for use with CP110860 and CP106682. Includes specimen stops for easy specimen location.
Conforms to ISO 14125 for specimen thickness less than 3 mm.
Max Static load: 10 kN (1,000 kgf, 2,200lbf)
Anvil width : 26 mm (1.0 in)
Upper anvil diameter: 10.0 mm (0.4 in)
Lower anvils diameter: 4.0 mm (0.16 in)
Note: Lower anvils have asymmetric form as defined in EN2377 and EN2746.
Temperature range: -70 to +250 °C (-94 to +482 °F)
CP110860 or CP106682 base beam required.
Compatible with CP108199 span setting micrometers
| Description | 3-point bend loading and support anvils set to ISO 14125 & EN2746 (Flexural) and ISO 14130 & EN2377 (ILSS) for use with CP110860 and CP106682. |
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Composites Test Fixture Compression After Impact
The “Airbus CAI” fi xture is used to test the impact resistance of carbon and other fi ber-reinforced plastic (CFRP) composite laminates. These materials are prone to great reduction in compressive strength even when the impact load is insuffi cient to cause visible damage. The post-impact compression test is used widely to assess the relative performance of different composite laminates with different fi ber matrix combinations. In the fi rst part of the test the laminates are subjected to low-velocity impact loading simulating tool drops and fl ying debris. Specimens then undergo a compression after impact(CAI) test on an electromechanical or servohydraulic testing machine.
- ผลิตภัณฑ์
- 6/15/2011
- 98.7 KB