发明名称 SHUTTER SYSTEM FOR CLOSING OFF THE GAS EXHAUST PIPE OF A MISSILE LAUNCHER
摘要 This shutter system (14) for the barrel of a missile launcher, the launcher (1) comprising at least one container (2, 3) capable of accommodating at least one missile (4, 5) and a pipe (10) for discharging the propulsion gases comprising a gas extraction barrel (11), the container being in communication with the pipe when the missile is fired and the pipe being in communication with the atmosphere (12) via the barrel equipped with the said shutter system, is characterized in that the shutter system comprises at least one panel (12, 13) and a panel retaining means (18, 19), able to move between a closed position and an open position, the retaining means comprising a means (18a) of return from the open position to the closed position and a means (18b) of dissipating the energy resulting from the opening movement and the closing movement.
申请公布号 WO2009138664(A2) 申请公布日期 2009.11.19
申请号 WO2009FR50751 申请日期 2009.04.23
申请人 DCNS;FALIP, ALAIN 发明人 FALIP, ALAIN
分类号 主分类号
代理机构 代理人
主权项
地址