Stratopause airship safety control blasting device
Patent Information
- Application Number
- CN202521816560.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-08-25
- Publication Date
- 2026-08-28
- Estimated Expiration
- 2035-08-25
AI Technical Summary
导爆索与起爆器属于火工品,均为一次性使用产品;在飞艇制造及维护过程中,地面安装后无法对这些火工品进行性能检测和状态监测
[0013]与现有技术相比本实用新型的有益效果为:当飞艇出现安全隐患时,飞控计算机启动安控程序,控制大功率电源向电热丝供电,电热丝在安装通道内部发热,使发热的电热丝对飞艇囊体的蒙皮进行熔断破坏,从而使飞艇囊体内的氦气进行释放,实现飞艇的安全降落,电热丝非火工品,可多次重复触发,且便于在地面进行测试,大幅提升了系统可靠性,电热丝成本仅约为导爆索装置的1/100,降低了飞艇安控系统的制造成本。
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Figure CN224695142U_ABST
Abstract
Claims
1. A stratospheric airship safety control explosive device, comprising an airship body (1), a fastening device (2), an installation channel (3), a heating wire (4), and a high-power power supply (5), characterized in that, An adhesive device (2) is provided on the outer wall of the airship body (1). The adhesive device (2) and the airship body (1) form an installation channel (3). An electric heating wire (4) is installed inside the installation channel (3). Both ends of the electric heating wire (4) are electrically connected to a high-power power supply (5). It also includes a drop protection component. A drop protection component is provided on the outside of the high-power power supply (5).
2. The stratospheric airship safety control blasting device as described in claim 1, characterized in that, The anti-fall component includes an anti-fall shell (6), a shock-absorbing foam layer (7), a first shaft pin (8), a cover plate (9), a buffer pad (10), and a locking assembly. The shock-absorbing foam layer (7) is fitted inside the anti-fall shell (6). The cover plate (9) is hinged to the top of the anti-fall shell (6) through the first shaft pin (8). A buffer pad (10) is provided on the cover plate (9). The high-power power supply (5) is detachably clipped inside the shock-absorbing foam layer (7). A locking assembly is provided between the cover plate (9) and the anti-fall shell (6).
3. The stratospheric airship safety control blasting device as described in claim 2, characterized in that, The locking assembly includes a U-shaped clamping plate (11), a second shaft pin (12), a lead screw (13), and a wing nut (14). The cover plate (9) is provided with a U-shaped clamping plate (11). The lead screw (13) is hinged to the anti-fall shell (6) in cooperation with the second shaft pin (12). The lead screw (13) is threadedly connected to the wing nut (14).
4. The stratospheric airship safety control blasting device as described in claim 1, characterized in that, The heating wire (4) is made of nickel-chromium alloy. The diameter of the heating wire (4) is 2-6 mm and the length is 0.5 m to 10 m. It can be rapidly heated to 300°C within 5 seconds.
5. The stratospheric airship safety control blasting device as described in claim 1, characterized in that, The diameter of the mounting channel (3) is 0.5 mm larger than the diameter of the heating wire (4). The heating wire (4) passes through the mounting channel (3) and fits tightly against the skin of the airship body (1), but is not fixedly connected to the skin. The minimum radius of curvature of the heating wire (4) is 0.1 m.
6. The stratospheric airship safety control blasting device as described in claim 1, characterized in that, The power range of the high-power power supply is 200-5000W.
7. The stratospheric airship safety control blasting device as described in claim 1, characterized in that, The number of heating wires (4) can be set to one or more according to the actual needs of the airship. The fastening device (2) is fixed to the outer surface of the skin of the airship body (1) by sewing or gluing.