Base Support for for Anti-Buckling Support Jigs/Plates to Boeing BSS 7260
CP114249 | Base Support for for Anti-Buckling Support Jigs/Plates to Boeing BSS 7260
(ASTM D 695 modified) / SACMA SRM 1 / prEN 2850
Locates between compression platens.
Upper Interface: Requires compression platen diameter 100 mm (4 in) or larger. Lockable spherical seat recommended to ensure parallelism.
Lower Interface: Requires fixed compression platen diameter 100 mm (4in) or larger.
Platens not included.
For use with S4931A, CP108932, CP114221, CP114215, CP115010, CP115011 Anti-Buckling jigs/plates (Required not included).
Max. Load : 100 kN (10,000 kgf, 22,000 lbf)
Temperature range : -100 to +350 °C (-148 to +662 °F)
Includes storage case.
| アクセサリ高さ | 100 mm (3.94 in) |
|---|---|
| アクセサリ重量 | 1 kg (2.2 lb) |
| アクセサリ幅 | 50 mm (1.97 in) |
| 荷重容量 | 100 kN (22,000 lbf) |
| 下側取り付け | Requires platen 100 mm (4 in) or larger |
| 温度速度 | -100 to +350°C (-148 to +662°F) |
| 試験規格 | As per support jig |
| 上側取り付け | Requires platen 100 mm (4 in) or larger |
Composites Test Fixtures- Compression Anti-Buckling
The anti-buckling fixture was originally designed for rigid plastics per ASTM D 695, reinforced plastics per ASTM D 3846. It was also extended and used for high-modulus composites. Boeing then adapted the fixture so that it would be self supported between two platens to ensure consistent perpendicularity of the fixture. The SACMA standard followed the Boeing design with an added alternative support fixture with a cutout, which would allow bonded strain gages to be used at the center of the specimen for a more precise strain measurement.
- 製品
- 8/25/2014
- 0.5 MB