发明名称 Indicator for an ejection seat firing mechanism
摘要 An ejection seat firing mechanism has a primary cartridge and a firing pin within a housing. A firing head is outside the housing coaxial with the primary cartridge and the firing pin, and a nut affixes the firing head to the firing pin thereby enclosing the housing. A first bore is formed through the flange of the housing and a second bore is formed in the nut spaced from the housing and aligned with the first bore in spaced parallel relation with the axis. A torquing shaft with an internally threaded axial coupling bore formed therein extends a determined distance into the torquing shaft. A spring is coaxially positioned around the torquing shaft and has a top end abutting the nut and a spaced opposite bottom end biasing the torquing shaft toward the flange. A bolt member extends through the first bore and is threadedly coupled with the torquing shaft via the coupling bore. The bolt provides a visual and sensory indication that the primary cartridge is installed and the firing head is torqued.
申请公布号 US5379675(A) 申请公布日期 1995.01.10
申请号 US19930115447 申请日期 1993.09.01
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 ARONNE, ARMAND J.
分类号 B64D25/10;B64D25/102;(IPC1-7):B64D25/102 主分类号 B64D25/10
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