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    • 2. 发明授权
    • Optically guided munition control system and method
    • 光导制导控制系统及方法
    • US08450668B2
    • 2013-05-28
    • US11632671
    • 2006-02-07
    • John A. MaynardMark A. CarlsonPaul D. Zemany
    • John A. MaynardMark A. CarlsonPaul D. Zemany
    • F42B15/01F42B10/62F42B15/00F42B10/00
    • F42B15/01F41G7/222F41G7/226F41G7/2293G05D1/12
    • An optically guided munition and control system has a replacement fuse assembly mounted on the front of a munition body or shell casing. An optical seeker subsystem detects an illuminated target and supplies signals to a processor. The processor develops steering commands sent to a flight control subsystem having a plurality of guidance canards which are actuated by drive motors through gear assemblies. The roll of the munition is established and left/right and up/down steering commands are sent to the canard drive motors based upon the optical seeker subsystem detection of the target illuminator. Range adjustment is based upon bore sight lockdown angle and cross range control is based upon left/right centering error. A code is contained in the optical radiation received from the illuminated target which must be validated by a preset code in the system processor to arm the munition.
    • 一个光学导弹的弹药和控制系统具有安装在弹药体或壳体外面的替换保险丝组件。 光学探针子系统检测被照射的目标并向处理器提供信号。 处理器开发发送到飞行控制子系统的转向命令,该飞行控制子系统具有由驱动马达通过齿轮组件驱动的多个导向槽。 建立弹药卷,基于目标照明器的光学引导器子系统检测,左/右上下转向命令被发送到卡车驱动马达。 范围调整基于钻孔视距锁定角度,并且跨距控制基于左/右对中误差。 从被照射的目标接收到的光辐射中包含一个代码,该光辐射必须通过系统处理器中的预设代码进行验证以便弹药。
    • 3. 发明授权
    • Optically guided munition
    • 光导弹
    • US07533849B2
    • 2009-05-19
    • US11629062
    • 2006-02-07
    • Paul D. ZemanyMark A. CarlsonJohn A. Maynard
    • Paul D. ZemanyMark A. CarlsonJohn A. Maynard
    • F41G7/00F42B15/01F42B15/00
    • F41G7/226F41G7/222F41G7/2293F42B10/64F42B15/01
    • An optically guided mortar comprising a three axis canard assembly, an optical seeker, a guidance and control processor, and a fuze mechanism. The optical seeker is a direct replacement for existing standard mortar fuzes. The resulting system significantly improves current mortar circular error probability (CEP) and results in overall reduction of cost of target prosecution, reduction in collateral damage, improved crew survivability, and adds compatibility against limited non-stationary targets. The optical seeker detects an optical illuminator located at a target and supplies signals to the guidance and control processor which through a guidance algorithm supplies steering commands to drive motors of the three axis canard assembly which move a plurality of guidance canards to accurately direct the munition toward a target.
    • 一种光学引导的砂浆,其包括三轴组件,光学探针,引导和控制处理器以及引信机构。 光学探测器直接替代现有的标准砂浆。 所产生的系统显着改善了当前的迫击炮循环误差概率(CEP),并导致目标检测成本的总体降低,减少附带损害,提高了机组的生存能力,并增加了与有限非平稳目标的兼容性。 光学探测器检测位于目标位置的光学照明器,并向引导和控制处理器提供信号,引导和控制处理器通过引导算法提供转向命令来驱动三轴卡车组件的马达,移动多个导向槽,以准确地将弹药导向 一个目标。
    • 4. 发明申请
    • Optically Guided Munition Control System and Method
    • 光导导弹控制系统与方法
    • US20090039197A1
    • 2009-02-12
    • US11632671
    • 2006-02-07
    • John A. MaynardMark A. CarlsonPaul D. Zemany
    • John A. MaynardMark A. CarlsonPaul D. Zemany
    • F42B15/01
    • F42B15/01F41G7/222F41G7/226F41G7/2293G05D1/12
    • An optically guided munition and control system has a replacement fuse assembly mounted on the front of a munition body or shell casing. An optical seeker subsystem detects an illuminated target and supplies signals to a processor. The processor develops steering commands sent to a flight control subsystem having a plurality of guidance canards which are actuated by drive motors through gear assemblies. The roll of the munition is established and left/right and up/down steering commands are sent to the canard drive motors based upon the optical seeker subsystem detection of the target illuminator. Range adjustment is based upon bore sight lockdown angle and cross range control is based upon left/right centering error. A code is contained in the optical radiation received from the illuminated target which must be validated by a preset code in the system processor to arm the munition.
    • 一个光学导弹的弹药和控制系统具有安装在弹药体或壳体外面的替换保险丝组件。 光学探针子系统检测被照射的目标并向处理器提供信号。 处理器开发发送到飞行控制子系统的转向命令,该飞行控制子系统具有由驱动马达通过齿轮组件驱动的多个导向槽。 建立弹药卷,基于目标照明器的光学引导器子系统检测,左/右上下转向命令被发送到卡车驱动马达。 范围调整基于钻孔视距锁定角度,并且跨距控制基于左/右对中误差。 从被照射的目标接收到的光辐射中包含一个代码,该光辐射必须通过系统处理器中的预设代码进行验证以便弹药。
    • 6. 发明申请
    • Method and Device for Unclogging a Drain Assembly
    • 拆卸排水装置的方法和装置
    • US20150007384A1
    • 2015-01-08
    • US13933759
    • 2013-07-02
    • Mark A. Carlson
    • Mark A. Carlson
    • E03C1/308A47K3/00
    • E03C1/308E03C1/244
    • A method and device for unclogging a drain assembly by creating an airtight, watertight seal in the drain assembly. An overflow cover device functions to form a complete seal in the drain assembly, such that no air and water pressure is lost throughout the drain assembly while a plunging device creates pressure and a vacuum over a drain opening. The water pressure generated by the plunging device is maximized to remove a clog in the drain assembly. The overflow cover device includes a front surface, and a mounting surface. The mounting surface includes a cover seal on the peripheral edge for inhibiting the escape of air and water. The mounting surface engages the overflow opening, and secures into place through machine screws that pass through one or two holes in the overflow cover device.
    • 一种用于通过在排放组件中形成气密的防水密封来消除排水组件的方法和装置。 溢流盖装置用于在排放组件中形成完整的密封,使得在泄漏装置在排水口上产生压力和真空时,整个排水组件中没有空气和水的压力损失。 由插入装置产生的水压最大化以消除排水组件中的堵塞。 溢流盖装置包括前表面和安装表面。 安装表面包括在周边边缘上的盖密封件,用于抑制空气和水的逸出。 安装表面接合溢流开口,并通过穿过溢流盖装置中的一个或两个孔的机械螺钉固定到位。