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Rocket Model Launching Experiment Device Using Electrostatic Discharge

机译:静电放电火箭发射实验装置

摘要

The present invention relates to an experimental device that explodes flammable fuel in a rocket model using static electricity generated by inductive charging of triboelectric electricity as ignition energy.;According to the present invention, the aluminum disc 1 is fixed at the end of the acrylic pipe 3, and the two discs are reciprocated by the acrylic slide holder 4 having the same size Teflon disc 2 having a hole in the center. Static electricity is generated between them. The spark generated between the two discharge electrodes 7 is connected to the discharge electrode 7 of the rocket model 6 with a plastic lid through the discharge rod 5 attached to the aluminum disc 1. The present invention relates to a rocket model firing experiment apparatus using an electrostatic discharge, characterized by detonating flammable fuel inside the rocket model 6 and firing the rocket model with the explosive force at this time.
机译:本发明涉及一种实验装置,该实验装置利用由摩擦带电的感应充电产生的静电作为点火能量来爆炸火箭模型中的易燃燃料。根据本发明,铝盘1固定在丙烯酸管的端部。如图3所示,两个盘通过具有相同尺寸的Teflon盘2的丙烯酸滑动保持器4往复运动,Teflon盘2的中心具有孔。它们之间会产生静电。在两个放电电极7之间产生的火花通过附接到铝盘1的放电杆5通过塑料盖连接到带有塑料盖的火箭模型6的放电电极7。静电放电,其特征在于,将火箭模型6内的易燃燃料引爆,并在此时用爆炸力射击火箭模型。

著录项

  • 公开/公告号KR200388190Y1

    专利类型

  • 公开/公告日2005-06-29

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20050010185U

  • 发明设计人 최정애;

    申请日2005-04-13

  • 分类号G09B23/00;G09B23/18;G09B23/06;

  • 国家 KR

  • 入库时间 2022-08-21 22:02:56

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