RU2012109862A

RU2012109862A - SAFETY DRIVER

Info

Publication number: RU2012109862A
Application number: RU2012109862/03A
Authority: RU
Original assignee: Шепеленко Виталий Борисович
Priority date: 2012-03-15
Filing date: 2012-03-15
Publication date: 2013-09-20

Abstract

Предохранительно-взводящее устройство, преимущественно для взрывателей снарядов реактивных систем залпового огня, характеризующееся тем, что содержит инерционный замыкатель, электронно-временное устройство, включающее запальный конденсатор, предохранительно-исполнительный механизм, размещенный в корпусе и содержащий ротор, привод вращения ротора с пусковым электровоспламенителем и толкателем, электродетонатор, причем выводы пускового электровоспламенителя соединены с выходом электронно-временного устройства, а контакты инерционного замыкателя соединены с входом электронно-временного устройства, при этом электрическая цепь пускового электровоспламенителя содержит разрядную цепь с размыкателем, замкнутым в исходном положении, установленную параллельно запальному конденсатору, при этом между инерционным замыкателем и размыкателем в указанной разрядной цепи запального конденсатора электровоспламенителя установлена жесткая функциональная связь, обеспечивающая их единовременное замыкание/размыкание.A safety-cocking device, mainly for fuses of rockets of multiple launch rocket systems, characterized in that it contains an inertial contactor, an electronic-temporary device including an ignition capacitor, a safety-actuating mechanism located in the housing and containing a rotor, a rotor drive with an electric igniter and a pusher, an electric detonator, and the conclusions of the starting electric igniter are connected to the output of the electronic-time device, and the contacts are inertial This contactor is connected to the input of the electronic-time device, while the electric circuit of the starting electric igniter contains a discharge circuit with a circuit breaker closed in its initial position, installed parallel to the ignition capacitor, while a rigid functional connection is established between the inertial contactor and the disconnector in the specified discharge circuit of the ignition capacitor of the electric igniter providing their one-time closing / opening.

Claims

A safety-cocking device, mainly for fuses of rockets of multiple launch rocket systems, characterized in that it contains an inertial contactor, an electronic-temporary device including an ignition capacitor, a safety-actuating mechanism located in the housing and containing a rotor, a rotor drive with an electric igniter and a pusher, an electric detonator, and the conclusions of the starting electric igniter are connected to the output of the electronic-time device, and the contacts are inertial This contactor is connected to the input of the electronic-time device, while the electric circuit of the starting electric igniter contains a discharge circuit with a circuit breaker closed in its initial position, installed parallel to the ignition capacitor, while a rigid functional connection is established between the inertial contactor and the disconnector in the specified discharge circuit of the ignition capacitor of the electric igniter providing their one-time closing / opening.