发明名称 Deployment brake release for a parachute
摘要 A deployment brake release system for use with an airborne guidance unit (AGU) of a parachute suitable for precision cargo delivery. The parachute includes deployment brake lines secured at one end to the edge of the canopy and connected at the other end through looped ends to motor control lines. The motor control lines are, in turn, engaged with the motor of the AGU. The deployment brake release system includes at least one hook mount having a hook secured to the AGU frame. The looped ends of the deployment brake lines are engaged with the hook during rigging so that, upon deployment, opening forces are applied to the hook mount rather than the motor. After full canopy inflation, the motor, via the motor control lines, pulls on the brake line looped ends to disengage them from the hook, transferring subsequent canopy loads to the AGU motor for the remainder of the flight. A method for releasing the deployment brake lines is also disclosed.
申请公布号 US2008149775(A1) 申请公布日期 2008.06.26
申请号 US20060645029 申请日期 2006.12.26
申请人 DUNKER STORM;GILBERT MARTIN 发明人 DUNKER STORM;GILBERT MARTIN
分类号 B64D17/62 主分类号 B64D17/62
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