首页> 外国专利> A BASE BLEED UNIT FOR INCREASING THE RANGE OF FIRE AND FOR DECREASING THE TIME OF FLIGHT FOR SHELLS AND PROJECTILES

A BASE BLEED UNIT FOR INCREASING THE RANGE OF FIRE AND FOR DECREASING THE TIME OF FLIGHT FOR SHELLS AND PROJECTILES

机译:一个基本的放血单元,用于增加火力范围并减少炮弹和弹丸的飞行时间

摘要

pA base bleed unit arranged to increase the range of fire or to reduce the time of flight for shells and projectiles includes a housing (1) surrounding a fuel charge (6) and associated igniter (4), extending from the rear portion of a projectile body (2) and including at least one outlet nozzle (5, 5', 5'') for combustion gases, which by means of a mass flow, and possibly combustion adjacent to the base plane, reduce existing base drag. According to an embodiment of the invention, the housing (1) comprises a caseshaped member 1 attachable against a projectile body (2), having at least one igniter (4) arranged adjacent to an internal plane of a restricting wall surface at the housing (1), located in an opposed relationship to the portion of the housing (1) attachable against a projectile body (2). The combustion flame of the igniter (4) is hereby maintained directed towards the fuel charge (6) and away from the outlet nozzle/nozzles (5, 5', 5''). Advantageously, a number of outlet nozzles (5, 5', 5'') are used, arranged spaced in an annular relationship to each other, and preferably inclined towards the outer peripheral portion of the restricting wall surface. A number of igniters (4) are advantageously used, located in recesses or blind holes taken up by the inside plane of the restricting wall surface. It is further advantageous to arrange the open portion of each igniter (4) partly covered by a covering means, thus accomplishing a reduced outlet area. According to a second embodiment, the housing (1) may also be formed by attachment of a bottom member to a projectile body (2) having a rearwardly open projectile extension, said bottom member including one or a number of igniters (4)./p[SE8603737D0]
机译:>布置成增加射击范围或减少炮弹和弹丸飞行时间的基础放气单元,包括从后部延伸的外壳(1),包围着燃料(6)和相关的点火器(4)。包括至少一个用于燃烧气体的出口喷嘴(5、5',5'')的弹体(2)的出口,该出口喷嘴通过质量流并可能在邻近基础平面处的燃烧减少了现有的基础阻力。根据本发明的实施例,壳体(1)包括可附接到弹体(2)的壳形构件1,其具有至少一个点火器(4),该至少一个点火器(4)邻近于壳体处的限制壁表面的内平面布置。 1),与壳体(1)的可抵靠弹体(2)的部分相对。因此,点火器(4)的燃烧火焰被保持朝向燃料(6),并远离出口喷嘴(5、5',5'')。有利地,使用多个出口喷嘴(5、5',5”),它们以环形关系彼此间隔地布置,并且优选地朝向限制壁表面的外周部分倾斜。有利地使用多个点火器(4),它们位于由限制壁表面的内平面占据的凹口或盲孔中。进一步有利的是,将每个点火器(4)的开口部分部分地被覆盖装置覆盖,从而实现减小的出口面积。根据第二实施例,壳体(1)还可以通过将底部构件附接到具有向后开口的弹丸延伸部的射弹体(2)而形成,所述底部构件包括一个或多个点火器(4)。 / p> [SE8603737D0]

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