公开(公告)号：US4377113A

公开(公告)日：1983-03-22

申请号：US232846

申请日：1981-02-09

申请人： John R. Florence

发明人： John R. Florence

IPC分类号： F41A19/00 ,  F41A19/63 ,  F42C19/12

CPC分类号： F41A19/00 ,  F41A19/63

摘要： A rocket firing system comprises a magnetic core, a co-axial driver coil and a sensor coil or coils which are connected to a detector device which detects the presence and the desired state of a further coil which is inductively linked to the magnetic core. In use a low-power signal voltage is first applied to the driver coil. Subject to the detector device indicating the presence and desired state of a firing circuit of a rocket including the further coil, an operating power voltage is then applied to the driver coil to induce a firing voltage in the firing circuit.

摘要翻译： 火箭发射系统包括磁芯，同轴驱动器线圈和传感器线圈或线圈，其连接到检​​测器装置，该检测器装置检测感应地连接到磁芯的另外的线圈的存在和期望状态。 在使用中，首先将低功率信号电压施加到驱动器线圈。 受检测器装置指示包括另外的线圈的火箭的点火电路的存在和期望状态，然后将工作电源电压施加到驱动器线圈以在点火电路中引发点火电压。