Invention Grant
- Patent Title: Parachute inlet control system and method
- Patent Title (中): 降落伞入口控制系统及方法
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Application No.: US13325344Application Date: 2011-12-14
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Publication No.: US08210479B2Publication Date: 2012-07-03
- Inventor: Roy L. Fox, Jr.
- Applicant: Roy L. Fox, Jr.
- Agency: Snell & Wilmer L.L.P.
- Main IPC: B64D17/62
- IPC: B64D17/62

Abstract:
A parachute inlet control system is configured to provide an improved inflation profile for solo and/or clustered parachutes. An inlet parachute is coupled to a main parachute via a plurality of lacing loops and/or reefing rings. The lacing loops may be passed through the reefing rings and/or may be routed around one or more of the main parachute suspension lines. The inlet parachute is located in the inlet area of the main parachute, and causes the inlet of the main parachute to rapidly form a desirable shape. The inlet parachute and lacing loops function as a reefing means, and prevent full inflation of the main parachute until a reefing cutter has functioned. In this manner, parachute failures, such as those due to leading and/or lagging parachutes in a parachute cluster, may be reduced or eliminated.
Public/Granted literature
- US20120080561A1 PARACHUTE INLET CONTROL SYSTEM AND METHOD Public/Granted day:2012-04-05
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