发明名称 METHOD OF BALLISTIC SOLID ROCKET PROPELLANTS
摘要 FIELD: weapons and ammunition.SUBSTANCE: cutting of charge fragment comprises displacing it through preset length, stopping it and cutting off by blade coupled with hydraulic cylinder piston. Piston continues lowering to press at charge fragments left after previous cycle on the grate. Piston extrudes said fragments through the grate to contact with said grate. Thereafter, it moves upward to initial position. Here, first fragment is completely separated and arranged between thrust and charge. In piston upward displacement, second fragment of the charge is cut off. Piston at crown, both fragments move down onto the grate. Then, cycle reiterates.EFFECT: higher process efficiency.5 dwg
申请公布号 RU2499980(C1) 申请公布日期 2013.11.27
申请号 RU20120124391 申请日期 2012.06.13
申请人 FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA SAMARSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET 发明人 CHESNOKOV VJACHESLAV ALEKSANDROVICH;VOLOGIN MIKHAIL FEDOROVICH;KIR'JAKOV GERMAN EVGEN'EVICH;EPIFANOV VLADIMIR BORISOVICH;DUKHINOV VLADISLAV VLADIMIROVICH
分类号 F42B33/06;C06B21/00 主分类号 F42B33/06
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