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    PULSE MODULATION LASER WRITING SYSTEM
    4.
    发明申请
    PULSE MODULATION LASER WRITING SYSTEM 审中-公开
    脉冲调制激光写字系统

    公开(公告)号：WO2006065557A3

    公开(公告)日：2007-03-29

    申请号：PCT/US2005043691

    申请日：2005-12-05

    Applicant: AEROSPACE CORP

    Inventor： LIVINGSTON FRANK EDWARD ,  HELVAJIAN HENRY

    IPC: B23K26/00 ,  G03C5/56

    CPC classification number: B23K26/0861 ,  B23K26/0626

    Abstract: An embodiment of the invention is described with reference to the figures using reference designations as shown in the figures. Referring to Figure 1, a pulse-modulated laser writing system includes a computer (10) for generating a laser script file and a motion control file. The control file can be a tool path file delineated in computer numerical control (CNC) program code. The motion control file is fed to the motion and position analyzer (12) for generating motion control data. The analyzer (12) functions as a motion controller of the platform and position synchronizer for synchronizing the motion to laser writing processes. The motion control data is fed to a motion-controlled platform (13) for synchronously moving the platform (13) with the script file. The platform (13) is coupled to an XYZ position encoder (14) for providing XYZ position data to the motion and position analyzer (12). The motion and position analyzer (12) may be a three-axis motion control system.

    Abstract translation: 参考使用附图所示的附图标记的附图来描述本发明的实施例。 参考图1，脉冲调制激光写入系统包括用于产生激光脚本文件和运动控制文件的计算机（10）。 控制文件可以是计算机数控（CNC）程序代码中描绘的工具路径文件。 运动控制文件被馈送到用于产生运动控制数据的运动和位置分析器（12）。 分析器（12）用作平台的运动控制器和用于使运动与激光写入过程同步的位置同步器。 运动控制数据被馈送到运动控制平台（13），用于使脚本文件同步移动平台（13）。 平台（13）联接到XYZ位置编码器（14），用于向运动和位置分析器（12）提供XYZ位置数据。 运动和位置分析器（12）可以是三轴运动控制系统。

    INTEGRATED GLASS CERAMIC SYSTEMS
    5.
    发明申请
    INTEGRATED GLASS CERAMIC SYSTEMS 审中-公开
    集成玻璃陶瓷系统

    公开(公告)号：WO2005062786A2

    公开(公告)日：2005-07-14

    申请号：PCT/US2004042401

    申请日：2004-12-16

    Applicant: AEROSPACE CORP

    Inventor： HELVAJIAN HENRY ,  JANSON SIEGFRIED W

    IPC: B64G1/10 ,  B64G1/26 ,  B64G1/36 ,  B64G1/40 ,  B64G1/42 ,  B64G1/44 ,  B64G1/66 ,  C03C10/00 ,  C03C15/00 ,  G02B6/42

    CPC classification number: B64G1/10 ,  B64G1/26 ,  B64G1/361 ,  B64G1/402 ,  B64G1/425 ,  B64G1/443 ,  B64G1/66 ,  C03C10/00 ,  C03C15/00 ,  G02B6/4246

    Abstract: Integrated glass ceramic spacecraft include a plurality of glass ceramic components including molded, tempered, annealed, and patterned glass ceramic components coupled together for forming a support structure or frame or housing through which is communicated optical signals through an optical communications grid and electrical signals through an electrical communications grid, with the optical communications grid and electrical communication grid forming a composite electrooptical communications grid for spacecraft wide intercommunications. The support structure multifunctions as a frame, a housing, a support, a thermal control system, and as part of an electrooptical communications grid while encapsulating a plurality of optical, electronic, electrical, and MEMS devices between which is communicated the electrical and optical signals over the electrooptical communication grid.

    Abstract translation: 集成玻璃陶瓷航天器包括多个玻璃陶瓷部件，包括模制的，回火的，退火的和图案化的玻璃陶瓷部件，所述玻璃陶瓷部件耦合在一起以形成支撑结构或框架或壳体，通过光学通信栅格将光信号传输通过所述支撑结构或框架或壳体， 电子通讯网络，光通讯网格和电子通讯网格形成了复合光电通讯网络，用于航天器的广泛通讯。 作为框架，壳体，支撑件，热控制系统以及作为电光通信栅格的一部分的支撑结构多功能件，同时封装多个光学，电子，电气和MEMS器件，在所述多个光学器件，电子器件，电子器件和MEMS器件之间传送电信号和光信号 通过电光通信网。

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