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    • 2. 发明公开
    • METHOD FOR PACKING FIN-STABILIZED PENETRATORS IN A CARRIER SHELL
    • 方法具有较强的肋骨A CUP获奖穿甲弹包装
    • EP2547980A4
    • 2015-10-14
    • EP11756617
    • 2011-03-10
    • BAE SYSTEMS BOFORS AB
    • THURMAN CHRISTER
    • F42B12/62F42B10/06F42B10/08F42B12/06F42B12/36F42B12/58F42B12/60
    • F42B12/58F42B10/06F42B10/08F42B12/06F42B12/362F42B12/60Y10S102/703
    • The present invention relates to a method for packing fin-stabilized penetrators (8) in a carrier shell (1), which penetrators (8) comprise a front penetrator part (10) and a rear fin part (9, 9′) comprising fin sides (14, 14′), so that the empty space between the penetrators (8) and problems with the penetrators upon the release of the penetrators (8) from the carrier shell (1) are minimized, wherein the penetrators (8) are packed in groups (7) and are joined together to form larger packing units (6), in which each group (7) is arranged with a centrally located penetrator (8) flanked by at least three outer penetrators (8), which outer penetrators (8) are arranged so that their front penetrator parts (10) lie side to side against the fin sides (14, 14′) of the centrally located penetrator (8). The method is characterized in that the rear fin parts (9, 9′) of the penetrators (8) are made shorter than the front penetrator parts (10) of the penetrators (8), and in that the front penetrator parts (10) are made cylindrical for the distribution of load stresses, upon firing of the carrier shell, from the centrally located penetrator (8) rearwards in the direction of firing via the front penetrator parts (10) of the flanking penetrators (8).
    • 本发明涉及一种用于包装尾翼稳定穿透的方法(8)中的载体壳(1)穿透(8)包括前穿透部(10)和后片部(9,9“)包括鳍 边(14,14“),所以在所述穿透器(8)从载体壳(1)的释放做了穿透(8)和与所述穿透问题之间的空的空间被最小化,worin穿透器(8)是 (8)由至少三个外部穿透(8),外侧翼穿透装在基团(7)和被连接在一起以形成较大的包装单元(6),其中,每个组(7)被布置成与位于中央的穿透 (8)被布置为使得没有它们的前穿透部分(10)位于一侧到另一侧抵靠鳍侧位于中央的穿透器(14,14“)(8)。 在DASS的特征在于该方法模具的穿透(8)的后部鳍片部分(9,9“)的比穿透(8)的前部穿透部件(10)变短,并且在没有前穿透部分(10) 由圆筒状的负载应力的分布,在载体外壳的烧成,从位于中央的穿透器(8)在向后方经由穿透侧翼的前端穿透部分(10)焙烧的方向(8)。
    • 4. 发明申请
    • PYROPHORIC ARROWS
    • WO2009104134A3
    • 2009-11-26
    • PCT/IB2009050646
    • 2009-02-17
    • RAFAEL ADVANCED DEFENSE SYSORLEV NAHUMWEITZ AMIR
    • ORLEV NAHUMWEITZ AMIR
    • F42B12/44F42B6/00F42B10/08
    • F42B10/04F42B10/08F42B10/14F42B12/08F42B12/44F42B12/46F42B15/00
    • An arrow-type warhead (100,200,300,400,500,600,700) comprises an envelope (102,202), a filling (108), a hardened head section (104) to promote penetration of the target and a stabilizing mechanism (106,210,302,402,502,602) to stabilize the warhead in flight, hi some embodiments the filling (108) is pyrophoric and undergoes an exothermic reaction with the envelope upon impact. In other embodiments the filling is incendiary and undergoes reaction with the envelope upon impact in an oxygen rich-environment. In yet other embodiments, the filling is explosive. In all embodiments, the warhead may be equipped with a mini-rocket propulsion mechanism (802) for propelling the warhead to the target.
    • 箭头型弹头(100,200,300,400,500,600,700)包括一个信封(102,202),一个填充物(108),一个硬化头部分(104),以促进目标的穿透,以及一个稳定机构(106,210,302,402,502,602)以使飞行中的弹头稳定。 实施例中,填充物(108)是自燃的,并且在碰撞时与包壳发生放热反应。 在其它实施方案中,填充物是燃烧的,并且在富氧环境中冲击时与包络体发生反应。 在其他实施例中,填充物是爆炸性的。 在所有实施例中,弹头可以配备有用于将弹头推进到目标的微型火箭推进机构(802)。
    • 5. 发明申请
    • METHOD FOR PRODUCING A BULLET, BULLET PRODUCED ACCORDING TO SAID METHOD AND AMMUNITION PROVIDED WITH SAID BULLET
    • 生产BULLET的方法,根据SAID BULLET提供的方法和弹药生产的BULLET
    • WO2004046637A1
    • 2004-06-03
    • PCT/RU2003/000501
    • 2003-11-18
    • F42B30/02
    • F42B5/03F42B5/02F42B7/10F42B10/08F42B30/02
    • The invention relates to ammunition for fire and pneumatic smoothbore weapon and can be used for producing bullets for hunting and sporting guns. The inventive method consists in deforming the rear part of a tubular blank in such a way that an aerodynamic empennage is formed and in arranging a core in the front part of said blank. The core is introduced into the tubular blank prior to deforming and is fixed in said blank by deforming the front and rear parts thereof. Deformation is carried out by pressing the blank wall without modifying the thickness thereof. The deformation of the tubular blank can be carried out by longitudinally clamping said blank between two crimping matrixes. Said core is embodied in such a way that an extractor in the form of an aerodynamic needle is formed in the material thereof, the core being inserted when said extractor is disposed outside the internal volume of the blank.
    • 本发明涉及用于火和气动平头武器的弹药,可用于生产用于狩猎和运动枪的子弹。 本发明的方法包括使管状坯件的后部变形,使得形成空气动力学尾翼并且在所述坯料的前部中布置芯。 在变形之前将芯体引入管状坯料中,并且通过使其前部和后部变形而将其固定在所述坯件中。 通过在不改变其厚度的情况下按压坯料壁来进行变形。 管状坯料的变形可以通过在两个压接基体之间纵向夹紧所述坯料来进行。 所述芯部以如下方式实施:使得在其材料中形成空气动力针形式的提取器,当所述提取器设置在坯料的内部容积之外时,芯体被插入。
    • 6. 发明申请
    • FLECHETTE FOR DIRECT FIRE WEAPONS
    • 直升机火炬手
    • US20160363425A1
    • 2016-12-15
    • US14446370
    • 2014-07-30
    • U.S. Army Research Laboratory ATTN: RDRL-LOC-I
    • Michael A. Minnicino, II
    • F42B12/64F42B12/74F42B10/08
    • F42B12/64F41A21/16F42B10/08F42B12/06F42B12/74F42B14/02
    • A flechette for use with a gun barrel having a tapered bore with a diameter at the initial bore section greater than the diameter at the emergent bore. The flechette includes a body constructed of a ductile material and having an elongated axis aligned with the axis of the tapered bore when positioned in the load end of the bore. The body also includes a cylindrical bulkhead as well as a bourrelet that are axially spaced from each other along the flechette and have an outside diameter substantially the same as the diameter at the initial bore section of the tapered bore. An elongated boom is attached at the tail end of the body while a penetrator is attached at the forward end of the body. Upon launch, both the bulkhead and bourrelet are compressed radially inward by the bore reduction so that the body is substantially cylindrical upon exit from the discharge end of the bore.
    • 用于枪筒的指示器,其具有在初始孔部分处的直径大于出口孔处的直径的锥形孔。 该收集器包括由延性材料构成的主体,并且当定位在孔的负载端时具有与锥形孔的轴线对准的细长轴线。 主体还包括一个圆柱形隔板以及一个沿着熔断器彼此轴向隔开并且具有与锥形孔的初始孔部分处的直径基本相同的外径的料槽。 细长的吊杆连接在身体的尾端,而穿透器附接在身体的前端。 在发射时,舱壁和舷窗都通过孔径减小而径向向内压缩,使得当从孔的排出端出来时,主体基本上是圆柱形的。
    • 9. 发明授权
    • Sub projectile or flechette launch system
    • US4210082A
    • 1980-07-01
    • US168504
    • 1971-07-30
    • Jack Brothers
    • Jack Brothers
    • F42B10/08F42B12/60F42B23/00
    • F42B10/08F42B12/60Y10S102/703
    • An explosive flechette launching system which includes a central core expive driver having stacked coaxially thereabout a plurality of disc plates which have layered and sandwiched therebetween for radial launching a multiplicity of flechettes. In one embodiment, the flechettes are oriented and pointed in a radial direction and each are provided with divergent tail piece which is releasably fitted into a mating recess in a driver piston abutting said explosive driver. The fin assembly is provided with a central bore and is slidably carried by the flechette body so that when disposed in said launching system, the fin assembly is positioned at the pointed end thereof and supported by wedge supports along the fins and intermediate the disc plates. The entire assembly is protectively encapsulated or covered with a thin membrane or skin. The explosive driver is designed to provide or generate a radial plane, high pressure wave for launching the flechettes. In the other embodiment the flechettes are oriented, between the plates, transverse to the direction of flight or side launch to provide a relatively large surface area against which the explosive energy can act.