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    • 4. 发明授权
    • Assembly for attaching fasteners to a belt
    • 用于将紧固件连接到皮带的组件
    • US06311393B1
    • 2001-11-06
    • US09382859
    • 1999-08-25
    • James M. Garner
    • James M. Garner
    • B23P1100
    • F16G3/16F16G3/04Y10T29/5343Y10T29/53713
    • An assembly for attaching U-shaped belt fasteners to the end of an elongated flat belt in which each belt fastener has first and second opposed leg portions with an integral bight portion therebetween and with at least one fastening wire extending from the first leg portion and a wire receiving opening in the second leg portion, the assembly including an elongated alignment member having a forward face with openings therein to receive the fastening wires of a plurality of belt fasteners and to hold the belt fasteners in an open position allowing the end of a belt to be inserted between the legs of the plurality of belt fasteners and an elongated anvil member having a forward face configured so that when the anvil member is displaced towards the alignment member the legs of the belt fasteners are bent towards each other to capture the belt therebetween, openings being provided in the alignment member to receive a punch by which the fastening wires can be driven through the belt.
    • 一种用于将U形带紧固件附接到细长扁平带的端部的组件,其中每个带紧固件具有第一和第二相对的腿部,其间具有整体的弯曲部分,并且具有从第一腿部部分延伸的至少一个紧固线, 所述组件包括细长对准构件,所述对准构件的前面具有开口,用于容纳多个带紧固件的紧固线,并且将带固定件保持在打开位置,从而允许带的端部 被插入在多个带紧固件的腿部和细长的砧座构件之间,该砧座构件具有构造成使得当砧座构件朝向对准构件移位时,带紧固件的腿朝向彼此弯曲以在其间捕获带 在对准构件中设置开口,以容纳冲头,通过该冲头可以将紧固线驱动穿过皮带。
    • 5. 发明授权
    • Fin disengagement device for limiting projectile range
    • 翅片分离装置,用于限制射弹范围
    • US06540176B2
    • 2003-04-01
    • US09756003
    • 2001-01-08
    • Bradford S. DavisJames M. GarnerJerry L. WatsonJames F. Newill
    • Bradford S. DavisJames M. GarnerJerry L. WatsonJames F. Newill
    • F42B1000
    • F42B10/06F42B10/48
    • A fin disengagement device for limiting the range of a projectile uses an electronic safe and arm circuit to sense launch and spin levels. Once armed, the stored energy from the electronic safe and arm circuit is dumped into an initiator or directly to explosive bolts. The initiator ignites an energetic material to separate the fin from the projectile in-flight at a predetermined time. Alternatively, the explosive bolts separate the fin from the projectile in-flight at a predetermined time. In the embodiments using an initiator and energetic material, an opening or cavity in the rear portion of the projectile body or rod adapter acts as a pressure chamber. When enough pressure has built up from the burning of the energetic material, the front hub of the fin section expands enough to disengage the threads and separates the fin section from the projectile body.
    • 用于限制射弹的范围的翅片脱离装置使用电子安全和臂电路来感测发射和旋转水平。 一旦武装,来自电子安全和手臂电路的储存能量被倾倒到引爆器或直接爆炸螺栓。 起动器在预定时间内点燃高能材料以将飞溅物从飞行中分离出来。 或者,爆炸螺栓在预定时间将飞溅物与飞行中的飞行物分开。 在使用引发器和高能材料的实施例中,射弹体或杆接头的后部中的开口或空腔用作压力室。 当从能量材料的燃烧形成足够的压力时,翅片部分的前轮毂足够扩张以使螺纹脱离并将翅片部分与射弹体分开。