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    • 6. 发明申请
    • STAND-OFF PANEL THERMAL PROTECTION SYSTEM AND METHOD OF FABRICATING THE SAME
    • 固定面板热保护系统及其制造方法
    • US20160362199A1
    • 2016-12-15
    • US14738314
    • 2015-06-12
    • The Boeing Company
    • Michael J. BestThomas R. PinneyJonathan D. Embler
    • B64G1/58B64G1/62B64G1/14
    • B64G1/58B64G1/14B64G1/62F16B33/006
    • A stand-off panel thermal protection system is disclosed. The system comprises a sandwich panel comprising: a first ceramic matrix composite facesheet and a second ceramic matrix composite facesheet. A ceramic matrix composite core is positioned between the first ceramic matrix composite facesheet and the second ceramic matrix composite facesheet. The ceramic matrix composite core has a perimeter. The first ceramic matrix composite facesheet and the second ceramic matrix composite facesheet extend past the perimeter to form a gap between the first ceramic matrix composite facesheet and the second ceramic matrix composite facesheet surrounding the ceramic matrix composite core. A plurality of orifices are formed through the sandwich panel. The thermal protection system further comprises a soft goods seal positioned in the gap; a plurality of insulation components; a plurality of stand-off brackets; and a plurality of fasteners positionable through the plurality of orifices to couple the sandwich panel to the plurality of brackets.
    • 公开了一种间隔板热保护系统。 该系统包括夹层板,其包括:第一陶瓷基质复合面和第二陶瓷基复合面。 陶瓷基复合芯位于第一陶瓷基复合面和第二陶瓷基复合面之间。 陶瓷基复合材料芯具有周长。 第一陶瓷基复合面板和第二陶瓷基复合面板延伸穿过周边,以在第一陶瓷基体复合面和围绕陶瓷基复合芯的第二陶瓷基复合面之间形成间隙。 多个孔通过夹层板形成。 热保护系统还包括位于间隙中的软货物密封件; 多个绝缘部件; 多个支架; 以及可通过所述多个孔定位的多个紧固件,以将所述夹芯板耦合到所述多个托架。
    • 8. 发明申请
    • METAL ATTACHMENT
    • 金属附件
    • US20160169262A1
    • 2016-06-16
    • US14906258
    • 2014-07-21
    • LISI AEROSPACE
    • Benoit RegnardJulien GoyerMartial Broucke
    • F16B33/06B64D45/02F16B25/00
    • F16B33/06B64D45/02C25D11/022F16B25/0021F16B33/006
    • The invention concerns a metal attachment for providing an electrically conductive surface through the entire thickness of structural elements to be assembled. The attachment thereby comprises a head (12)and a smooth shank (14) extending along an axis of revolution, characterized in that the shank comprising at least one conductive portion (24) and one lubricating portion (22) disposed along the axis of revolution of the attachment along at least one length of the shank. The attachment according to the invention provides a conductive surface through the entire thickness of the structure in which it is installed. The attachment according to the invention is intended, in particular, for aeronautical applications.
    • 本发明涉及一种用于通过要组装的结构元件的整个厚度提供导电表面的金属附件。 附件因此包括头部(12)和沿着旋转轴线延伸的光滑柄(14),其特征在于,柄部包括至少一个导电部分(24)和沿旋转轴线设置的一个润滑部分(22) 沿着柄的至少一个长度的附件。 根据本发明的附件通过安装其中的结构的整个厚度来提供导电表面。 本发明的附件特别用于航空应用。