公开(公告)号：US06530539B2

公开(公告)日：2003-03-11

申请号：US09780828

申请日：2001-02-09

申请人： Lee M. Goldman ,  Steven R. Collins ,  David B. James ,  David M. Blanchard ,  Steven Wirth

发明人： Lee M. Goldman ,  Steven R. Collins ,  David B. James ,  David M. Blanchard ,  Steven Wirth

IPC分类号： F42B1534

CPC分类号： F41G7/2293 ,  F41G7/2253 ,  F42B15/01 ,  F42B15/34

摘要： An interceptor missile including an infrared radiation detection subsystem and a window assembly in the hull of the missile optically coupled to the infrared radiation detection subsystem. The window assembly includes an inner window, an outer window, and a support subsystem between the inner and the outer windows defining a plurality of infrared transparent fluid flow cooling channels between the inner and outer windows. A source of fluid coupled to the cooling channels for cooling the outer window without adversely affecting the optical properties of either window.

摘要翻译： 一种拦截导弹，包括红外辐射检测子系统和在与红外辐射检测子系统光耦合的导弹的船体中的窗口组件。 窗户组件包括内窗，外窗和位于内外窗之间的支撑子系统，在内窗与外窗之间形成多个红外透明流体流冷却通道。 耦合到冷却通道的流体源，用于冷却外窗，而不会不利地影响任一窗口的光学性质。