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The power output employs a high-power hollow-shaft servo direct drive motor.
Customizable upon customer request.
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| The fuselage adopts an “O”-shaped (closed-loop) structure. | The power output employs a high-power hollow-shaft servo direct drive motor. | The entire fuselage has undergone high-temperature tempering in an electric furnace. |
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| Panasonic Motor (RTEX bus model) | Secondary positioning device | The fuselage is equipped with a mold storage cabinet. |
| Project | Parameter | Unit |
|---|---|---|
| Punching force | 300 (30) | KN (T) |
| Rack structure | “O”-type closed frame | — |
| Maximum workpiece size for single positioning | X-axis 2500, Y-axis 1250/1500/2000 | mm |
| Maximum sheet size for processing | 6 | mm |
| Maximum diameter of a single punch hole | Φ88.9 (customizable) | mm |
| Maximum stamping frequency | 1800 | hpm |
| Maximum punching cycles | 800 | hpm |
| Number of control axes | 5 (X, Y, T, C, R) | one |
| Mold type | Long-guide 85-series international standard mold | — |
| Turret Station Distribution | 16A, 11B, 3C, 2D (including rotary stations 1B and 1C) | Standard configuration |
| Repositioning cylinder | 2 | set |
| Number of clamps | 3 | one |
| Maximum shipping speed | X-axis 80, Y-axis 80 | m/min |
| Workbench Structure | Brush/Universal Steel Ball Composite Tabletop | — |
| Maximum turret speed | 40 | rpm |
| Machining accuracy | ±0.1 | mm |
| Maximum load capacity | 150 | Kilogram |
| Combined power usage | 6 | KW |
| External dimensions | Length × Width × Height: 6500 × 5200 × 2100 | mm |