发明名称 |
Internal fluid cooled window assembly |
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.
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申请公布号 |
US6530539(B2) |
申请公布日期 |
2003.03.11 |
申请号 |
US20010780828 |
申请日期 |
2001.02.09 |
申请人 |
RAYTHEON COMPANY |
发明人 |
GOLDMAN LEE M.;COLLINS STEVEN R.;JAMES DAVID B.;BLANCHARD DAVID M.;WIRTH STEVEN |
分类号 |
F41G7/22;F42B15/01;F42B15/34;(IPC1-7):F42B15/34;F41G7/00 |
主分类号 |
F41G7/22 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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