发明名称 Sensor window compliant mounting assembly
摘要 A sensor window compliant mounting assembly (42), such as used in a missile (20) to protect a sensor (40), has a truncated hemispherical sensor dome window (52) and a dome mount housing (60). The dome mount housing (60) includes a hollow tube (62) with an opening (64), an internal circumferential thread (66) adjacent to the opening (64), and an integral bezel retainer ring (68) extending circumferentially around the opening (64). The bezel retainer ring (68) engages and retains the exterior surface (56) of the dome base (54). A spanner nut (72) is threadably engaged to the internal circumferential thread (66) of the dome mount housing (60), and a partially compressed fiber metal washer (74) reacts between the spanner nut (72) and the lower surface (58) of the dome base (54) to bias the sensor dome window (52) toward the bezel retainer ring (68).
申请公布号 US5366178(A) 申请公布日期 1994.11.22
申请号 US19930110525 申请日期 1993.08.23
申请人 HUGHES AIRCRAFT COMPANY 发明人 HSIONG, WILLIAM;MARSHALL, THOMAS P.
分类号 F42B15/00;F41G7/22;F42B10/46;F42B15/01;F42B15/34;H01Q1/28;H01Q1/42;(IPC1-7):F42C13/00 主分类号 F42B15/00
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