发明名称 Imperative chute
摘要 An aircraft emergency landing assist system comprised of a harness to cradle the major stress points of the aircraft. The harness made of lightweight high tension material attached to the aircraft fuselage. The harness works as a sling with straps coming up each side of the aircraft to attach to a parachute system. In an emergency situation when a parachute is deployed said harness will cradle the body of the aircraft and relieve stress from said body. Pedal in cockpit of aircraft within reach of pilots foot. In an emergency situation, the pilot will push said pedal to activate distress signal, lock the fuel gauge in place A safety feature in the event there are intruders in the cockpit Activate dump fuel switch, activate hydraulic doors when doors are opened, they will activate chute deployment rocket. Said rocket will take canopy to it's full extension.
申请公布号 US2007246606(A1) 申请公布日期 2007.10.25
申请号 US20060410077 申请日期 2006.04.25
申请人 LEWIS JEAN A;STOTTS ILENE 发明人 LEWIS JEAN A.;STOTTS ILENE
分类号 B64C30/00 主分类号 B64C30/00
代理机构 代理人
主权项
地址