发明名称 METHOD FOR DISPOSAL PROPELLANT CHARGES OF SOLID-FUEL ROCKET ENGINES
摘要 FIELD: methods of ammunition disposal. ^ SUBSTANCE: the method consists in extracting charges from an engine , their mechanical longitudinal cutting into uniform sticks with a maximum cross-section size not exceeding 100 m, placing said charge sticks vertically one over another into oil producing and injection wells filled with fluid and their burning in the near-wellbore zone. Charge sticks are delivered to the burning zone by means of a wire-line in a cylindrical container perforated with holes for products effluence in the central portion of the side face at a distance of 1/4 of the length from the both end faces, and then the sticks are burnt over their outer surfaces inflaming them by sending electric pulses simultaneously to the both igniters disposed on the bottom end face of the bottom stick and on the top end face of the top stick. According to the second variant, the container is perforated over its entire side face. The charge sticks are burnt over their end faces from top downward, by inflaming the top end face of the top stick. ^ EFFECT: ensuring reduction of disposal costs, enhancing technological effectiveness and environmental safety of the process. ^ 2 cl, 3 dwg
申请公布号 RU2326340(C2) 申请公布日期 2008.06.10
申请号 RU20060106004 申请日期 2006.02.26
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH MATERIALOV" 发明人 KUSAKIN JURIJ NIKOLAEVICH;KUTSENKO GENNADIJ VASIL'EVICH;USTJUZHANIN ANATOLIJ ALEKSANDROVICH
分类号 F42B33/06;E21B43/18;E21B43/25 主分类号 F42B33/06
代理机构 代理人
主权项
地址