发明名称 RAPID COOLDOWN DEWAR
摘要 <p>A dewar (20) useful in rapidly cooling a sensor (28) supported thereon includes a bore tube assembly having a cylindrical dewar bore tube (22) with an end cap (24) at one end to close the bore tube (22). The bore tube assembly is cooled by directing a stream of coolant at the interior of the end cap (24). The sensor (28) is mounted directly to the exterior surface of the end cap (24). A cold shield (34) partially encloses the sensor (28). A cold shield support bracket (38) mounts the cold shield (34) to the cylindrical side wall of the dewar bore tube (22) at a mounting location (36) axially displaced from the end cap (24) and therefore less effectively cooled than the end cap (24), so that heat is extracted from the support bracket (38) and the cold shield (34) less rapidly than from the sensor (28). From an uncooled starting condition, the sensor (28) is cooled to its operating temperature, and the cold shield (34) is cooled to its operating temperature, in about the same time. <IMAGE></p>
申请公布号 IL101691(D0) 申请公布日期 1992.12.30
申请号 IL19920101691 申请日期 1992.04.26
申请人 HUGHES AIRCRAFT COMPANY 发明人
分类号 F42B15/01;F17C3/08;F25D19/00;G01J1/02;G01J5/02;G01J5/06;G01J5/28;(IPC1-7):F25B/ 主分类号 F42B15/01
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