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    • 3. 发明申请
    • PROGRAMMED SHELL CASING EJECTOR APPARATUS FOR AUTOMATIC CANNON
    • 用于自动CANNON的编程壳体喷射装置
    • WO1980002065A1
    • 1980-10-02
    • PCT/US1980000305
    • 1980-03-21
    • ARES INC
    • ARES INCSTONER E
    • F41C15/14
    • F41A15/14
    • Programmed shell casing ejector apparatus (10), for an automatic cannon (18), includes an ejector member (14) axially slidably mounted to an axially reciprocating bolt assembly (24), a pair of cam tracks (12) symmetrically fixed to a cannon mount (36) and a pair of cam track followers (16) pivotally mounted to the bolt assembly (24) to engage the ejector member (14) and, when the bolt assembly recoils after firing, also to engage the cam tracks (12). Ejection of a shell casing (180), held to a bolt face (80) by an extractor (84) occurs when the ejector member (14) is moved forwardly, relative to the recoiling bolt assembly (24), by the cam track followers (16) sliding along the cam tracks (12). Casing ejection timing and velocity is programmed to prevent cannon malfunction due to improper ejection, by relatively configuring the cam tracks (12) and followers (16) so that the ejector member (14) moves forwardly relative to the bolt assembly (24) at a controlled, increasing ejection velocity which is substantially less than bolt recoil velocity.
    • 用于自动炮(18)的编程壳体外壳喷射器装置(10)包括轴向可滑动地安装到轴向往复运动的螺栓组件(24)上的顶出件(14),对称地固定在大炮上的一对凸轮轨道 安装件(36)和一对可枢转地安装到螺栓组件(24)上以接合顶出件(14)的凸轮轨道从动件(16),并且当螺栓组件在点火之后反冲时也与凸轮轨道(12)接合, 。 当喷射器构件(14)相对于反弹螺栓组件(24)向前移动时,通过凸轮跟随器件(84)向外移动由抽出器(84)保持在螺栓面(80)上的外壳壳体(180)的喷射 (16)沿着凸轮轨道(12)滑动。 通过相对配置凸轮轨道(12)和从动件(16)使得喷射器构件(14)相对于螺栓组件(24)向前移动,通过相对于螺栓组件(24)向前移动,由于喷射正时和速度被编程以防止由于不正确的喷射引起的炮弹故障 控制的,增加的喷射速度基本上小于螺栓反冲速度。
    • 4. 发明申请
    • TWO STAGE SHELL FEEDING APPARATUS WITH SHELL FEEDING PATH CONTROL
    • 两阶段进料装置与壳体进给路径控制
    • WO1981001328A1
    • 1981-05-14
    • PCT/US1980001412
    • 1980-10-23
    • ARES INC
    • ARES INCGILLUM R
    • F41D10/04
    • F41A9/49F41A7/02F41A9/02F41A9/30F41A17/40
    • Shell feeding apparatus (20) for reciprocating bolt-type automatic guns, comprise a first stage rotor (76) having a plurality of shell holding cavities (78), rotatably mounted between a shell supply (24) and a shell pick up position (48), such that when one of the rotor cavities (78) is in the shell pickup position (48), another rotor cavity (78) is positioned for receiving shells (22) from the shell supply (24). During bolt recoil after firing, barrel gas pressure causes partial rotation of the rotor (76) to index a next shell (22) into the pick up position (48). Second stage means (62) then transfer another shell (22) from the shell supply (24) into an aligned rotor cavity (78) before the next firing. Means (92) mounted rearwardly of a shell (22) in the pick up position (48) cause shell acceleration before bolt-shell impact. The rotor cavities (78) and feed lips (86, 88) and deflector (90) are configured to control loading of shells (22) from the pick up position (48) into the gun breech (52).@00
    • 用于往复式螺栓式自动枪的壳体进给装置(20)包括具有多个壳体保持腔(78)的第一级转子(76),可旋转地安装在壳体供给装置(24)和壳体拾起位置(48)之间 ),使得当所述转子腔(78)中的一个处于壳拾取位置(48)时,定位另一个转子空腔(78)以用于从壳体供应(24)接收壳体(22)。 在燃烧后的螺栓反冲期间,机筒气体压力导致转子(76)的部分旋转以将下一个壳体(22)分配到拾取位置(48)。 第二级装置(62)然后在下次点火之前将另一个壳体(22)从壳体供应装置(24)转移到对准的转子空腔(78)中。 在拾取位置(48)的壳体(22)的后方安装的装置(92)在螺栓 - 壳体撞击之前引起壳体加速。 转子空腔(78)和进料嘴(86,88)和偏转器(90)被配置成控制壳体(22)从拾取位置(48)到枪后膛(52)的装载。
    • 5. 发明申请
    • OPEN-FRAMEWORK RECEIVER AUTOMATIC CANNON
    • 开放式接收器自动CANNON
    • WO1980002067A1
    • 1980-10-02
    • PCT/US1980000303
    • 1980-03-21
    • ARES INC
    • ARES INCSTONER E
    • F41D11/12
    • F41A3/82F41A11/02F41A25/12
    • An open-framework receiver cannon (10) comprises a barrel (12) and a breech ring (20) mounting the barrel. Intermediate regions of two elongate, rigid tubular support members (14, 16) are received through opposite sides of the ring (20) with longitudinal axes parallel to, equally spaced to sides of, and coplanar with, a barrel bore axis (52). Forward ends of the members (14, 16) are rigidly interconnected with the barrel (12) by a barrel support (22); rearward ends of the members are rigidly interconnected by a detachable recoil buffer (18). Disposed in the members (14, 16) are drive springs (192) for driving an associated bolt assembly (26) forwardly on unsearing, recoil apparatus (46) for causing recoil of a bolt carrier (152) in response to firing to enable unlocking of a bolt (154) from the breech (20) and a plurality of inertia weights (270) for reducing bolt carrier bounce from the breech block (20) on forward impact. Recoil cylinders (28, 30), containing a number of springs (300, 302), are mounted around the members (14, 16).