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    • 31. 发明专利
    • AT493630T
    • 2011-01-15
    • AT01924182
    • 2001-03-16
    • ENSIGN BICKFORD AEROSPACE & DEFENSE COMPANY
    • BOUCHER CRAIGMARSHALL PAULNOVOTNEY DAVID
    • F42B3/10F42C19/12B60R21/26F41H5/007F42C15/40F42D1/05
    • An ordnance system of the present invention may include or feature any one or more of: a control unit, one or more effectors (detonators, initiators, shaped charges and the like), and a two-,three- or four-wire communication bus between the control unit and the effectors; and addressable system in which all the effectors can be connected to the same communication bus and the control unit can issue coded signals on the bus addressed to a specific effector; inductive coupling between the effectors and the communication bus; and a multi-voltage level communication system in which communication signals are carried at a first voltage and arming signals are provided at a second, higher voltage. Other features may include two-way communication between effectors and the control unit and the de-centralization of firing control so that the control unit does not have exclusive control over whether the effectors function. As a result, the individual effects possess decision-making ability and, for purposes of the invention, may be referred to as "intelligent" effectors. To participate in the decision-making process, effects of this invention may be equipped with sensors or other diagnostic circuitry whose condition is checked for satisfactory output before functioning is permitted to occur.
    • 37. 发明公开
    • ORDNANCE FIRING SYSTEM
    • ORNOANCE燃烧系统
    • EP1497608A2
    • 2005-01-19
    • EP01924182.7
    • 2001-03-16
    • Ensign-Bickford Aerospace & Defense Company
    • BOUCHER, Craig, J.MARSHALL, Paul, N.NOVOTNEY, David, B.
    • F42C19/12F42B3/10F42C15/40
    • F42C15/40B60R2021/26029F41H5/007F42D1/05
    • An ordnance system of the present invention may include or feature any one or more of: a control unit, one or more effectors (detonators, initiators, shaped charges and the like), and a two-,three- or four-wire communication bus between the control unit and the effectors; and addressable system in which all the effectors can be connected to the same communication bus and the control unit can issue coded signals on the bus addressed to a specific effector; inductive coupling between the effectors and the communication bus; and a multi-voltage level communication system in which communication signals are carried at a first voltage and arming signals are provided at a second, higher voltage. Other features may include two-way communication between effectors and the control unit and the de-centralization of firing control so that the control unit does not have exclusive control over whether the effectors function. As a result, the individual effects possess decision-making ability and, for purposes of the invention, may be referred to as "intelligent" effectors. To participate in the decision-making process, effects of this invention may be equipped with sensors or other diagnostic circuitry whose condition is checked for satisfactory output before functioning is permitted to occur.
    • 本发明的军械系统可以包括或具有以下特征中的任何一个或多个:控制单元,一个或多个效应器(雷管,启动器,成形装药等)以及二线,三线或四线通信总线 在控制单元和效应器之间; 以及可寻址的系统,其中所有的效应器可以连接到相同的通信总线,并且控制单元可以在总线上发布寻址到特定效应器的编码信号; 效应器与通信总线之间的电感耦合; 以及多电压电平通信系统,其中通信信号以第一电压传送,并且布防信号以第二较高电压提供。 其他功能可能包括效应器和控制单元之间的双向通信以及发射控制的解集中,使得控制单元不能独享控制效应器是否起作用。 结果,个人效果具有决策能力,并且为了本发明的目的,可以将其称为“智能”效应器。 为了参与决策过程,本发明的效果可以配备传感器或其他诊断电路,在允许发生功能之前检查其状态是否满意输出。
    • 39. 发明公开
    • SPACECRAFT DEVICE INITIATIONSYSTEM
    • 航天器设备启动系统
    • EP3293122A1
    • 2018-03-14
    • EP17190741.3
    • 2017-09-13
    • Ensign-Bickford Aerospace & Defense Company
    • NOVOTNEY, DavidKACZYNSKI, GeoffBOUCHER, Craig
    • B64G1/22B64G1/42
    • B64G1/22B64G1/222B64G1/428G05B19/0423G05B19/409G05B2219/40513G05F1/66
    • One aspect of the present invention involves a networked initiation system having one or more non-energetic hold-down and release mechanisms ("HDRMs"), a control unit and an interface bus connected between all of the HDRMs and the control unit. Other aspects of the present invention involve networked initiation systems having one or more of each of non-energetic HDRMs, energetic HDRMs and other (generic) energetic devices. The systems also include a control unit and an interface bus connected between all of the HDRMs and/or energetic devices and the control unit. The system may be used on a spacecraft for holding various elements in place on the spacecraft during launch, and then activating the HDRMs and/or energetic devices at selected points in time after launch to release the elements for movement, e.g., into orbit or beyond.
    • 本发明的一个方面涉及一种联网启动系统,其具有一个或多个非能量压制和释放机构(“HDRM”),控制单元和连接在所有HDRM和控制单元之间的接口总线。 本发明的其他方面涉及具有非能量HDRM,能量HDRM和其他(通用)能量装置中的每一个的一个或多个的联网启动系统。 该系统还包括控制单元和连接在所有HDRM和/或高能设备与控制单元之间的接口总线。 该系统可以在航天器上用于在发射期间将各种元件保持在航天器上,然后在发射后的选定时间点激活HDRM和/或高能设备以释放用于移动的元件,例如进入轨道或超出 。
    • 40. 发明公开
    • Semiconductor bridge initiator
    • Halbleiterbrückenzünder
    • EP2241853A2
    • 2010-10-20
    • EP10159491.9
    • 2010-04-09
    • Ensign-Bickford Aerospace & Defense Company
    • Martinez-Tovar, BernardoBoucher, Craig J.
    • F42B3/13
    • F42B3/13F42B3/12F42B3/124
    • A semiconductor bridge die (200) may have an "H-design" or "trapezoidal" configuration in which a center bridge segment (204) is flanked by one or more angled walls (206) on each side of the bridge segment (204). Each wall (216) is plated with a conductive material, thereby providing a continuous conductive path across the top surface of the die. A bottom surface of the die may be connected to a top surface of a header by epoxy in various configurations. The plated angled walls (216) facilitate the solderable connection of the walls to a plated top surface of each of several pins on a top surface (112) of the header (100), thereby providing a continuous electrical connection between the pins (108) and the die (200). Also, a method is provided for manufacturing a semiconductor bridge die (200) in accordance with the various embodiments of the die.
    • 半导体桥模具(200)可以具有“H设计”或“梯形”构造,其中中心桥段(204)在桥段(204)的每一侧上由一个或多个成角度的壁(206) 。 每个壁(216)镀有导电材料,从而提供穿过模头顶表面的连续导电路径。 模具的底表面可以通过环氧树脂以各种构造连接到集管的顶表面。 电镀的倾斜壁(216)有助于将壁的可焊接连接到集管(100)的顶表面(112)上的多个销中的每一个的镀覆顶表面,由此在销(108)之间提供连续的电连接, 和模具(200)。 而且,提供了一种用于制造根据模具的各种实施例的半导体桥模(200)的方法。