Liquid propellant weapon system专利检索- .使用液体疏松粉末或气体燃料例如双组份火箭燃料燃烧的导弹推进器专利检索查询-专利查询网

Liquid propellant weapon system
申请号	JP31662588	申请日	1988-12-16	公开(公告)号	JPH024197A	公开(公告)日	1990-01-09
申请人	General Electric Co ;			发明人	MERUBUIN JIYON BARUMAN;
摘要	PURPOSE: To avoid strong feedback by performing additionally accelerating a mass integrating a traveling charge and a projectile through combustion of charged propellant and moving the mass forward along the cavity of barrel thereby performing controlled ignition and combustion. CONSTITUTION: A regeneration piston 34 is pushed forward by combustion gas generated in the rear combustion chamber 56 at the head thereof to push an initial propellant interposed between both heads. Consequently, the piston head separates from the conical face of head at the idle bottom to make an annular gap 56A and a stationary propellant flows through an injection port 56A into the chamber 56 thus sustaining or increasing the combustion gas pressure. When the pressure being applied to a moving propellant exceeds a propulsion starting level, the propellant and a projectile bring to accelerate while passing through a fixed center inclining face under influence of first stage liquid pressure of regeneration system. COPYRIGHT: (C)1990,JPO
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