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    • 1. 发明申请
    • PERFORATING APPARATUS AND METHOD HAVING INTERNAL LOAD PATH
    • 具有内部装载路径的装置和方法
    • US20150240607A1
    • 2015-08-27
    • US14367332
    • 2012-03-02
    • John H. HalesSamuel MartinezJohn P. Rodgers
    • John H. HalesSamuel MartinezJohn P. Rodgers
    • E21B43/117
    • E21B43/117E21B43/119
    • A perforating apparatus for a gun string is presented. The apparatus experiences an axial load and potentially a radial load during use. A central charge-carrier supports shaped-charges and substantially bears the axial load on the apparatus during use. The charge-carrier is positioned within an exterior sleeve and the plurality of shaped-charges, upon detonation, perforate the exterior sleeve. The exterior sleeve does not bear a substantial portion of the axial load on the apparatus and can therefore be thinner and cheaper than in prior art assemblies. An annular space can be defined between the charge-carrier and exterior sleeve. The exterior tubular can bear the radial load due to differential pressure in one embodiment. Alternately, the apparatus includes radial support members extending between the charge-carrier and sleeve for transmitting radial load to the charge-carrier. Alternately, the sleeve and charge-carrier abut one another along a substantial portion of the length of the charge-carrier.
    • 提出了一种用于枪串的穿孔装置。 该设备在使用过程中遇到轴向载荷和潜在的径向载荷。 中央电荷载体支撑成形电荷并且在使用期间基本上承受设备上的轴向载荷。 电荷载体位于外部套筒内,并且多个成形电荷在爆炸时穿透外部套筒。 外部套筒不承受装置上的大部分轴向载荷,因此可以比现有技术的组件更薄和便宜。 可以在电荷载体和外部套筒之间限定环形空间。 在一个实施例中,外管在承受差压的径向载荷。 或者,该装置包括在充电载体和套管之间延伸的径向支撑构件,用于将径向负载传送到电荷载体。 或者,套筒和电荷载体沿着电荷载体的长度的大部分彼此邻接。
    • 5. 发明申请
    • Perforating Apparatus for Enhanced Performance in High Pressure Wellbores
    • 用于提高高压井筒性能的穿孔装置
    • US20100300750A1
    • 2010-12-02
    • US12473569
    • 2009-05-28
    • John H. HalesJohn D. BurlesonJohn P. Rodgers
    • John H. HalesJohn D. BurlesonJohn P. Rodgers
    • E21B43/117E21B43/116
    • E21B43/117
    • A perforating apparatus (50) includes a carrier gun body (52) having a plurality of radially reduced sections (54). The radially reduced sections (54) have a nanocomposite outer layer (72). A charge holder (62) is positioned within the carrier gun body (52). A plurality of shaped charges (56) are supported by the charge holder (62). The shaped charges (56) each have an initiation end and a discharge end. The discharge ends of the shaped charges (56) are disposed proximate the radially reduced sections (54) of the carrier gun body (52) such that the jets formed upon detonation of the shaped charges (56) travel through the radially reduced sections (54). The nanocomposite outer layers (72) of the radially reduced sections (54) enable enhanced performance of the perforating apparatus (50) in high pressure and high temperature wellbores.
    • 穿孔装置(50)包括具有多个径向减小部分(54)的载体枪体(52)。 径向减小的部分(54)具有纳米复合材料外层(72)。 电荷保持器(62)位于载体枪体(52)内。 多个成形电荷(56)由电荷保持器(62)支撑。 成型电荷(56)各自具有起始端和放电端。 成形电荷(56)的放电端设置在载体枪体(52)的径向减小部分(54)附近,使得在成形电荷(56)爆炸时形成的射流行进通过径向减小的部分(54) )。 径向减小部分(54)的纳米复合材料外层(72)能够在高压和高温井筒中提高射孔装置(50)的性能。