公开(公告)号：US5954296A

公开(公告)日：1999-09-21

申请号：US25479

申请日：1998-02-18

申请人： Hendrick E. Jahsman ,  Kevin Mark Hopwood

发明人： Hendrick E. Jahsman ,  Kevin Mark Hopwood

IPC分类号： B64C1/32 ,  B64C1/00

CPC分类号： B64C1/32

摘要： An aircraft canopy fracturing system includes a canopy having fore and aft portions and a region that is severable from the canopy to provide an opening therethrough for the egress of aircraft occupants. The severable region has a shape that inhibits passage of the severable region through the opening created in the canopy once the severable region is freed from the canopy and is displaced aftward relative to the canopy. The canopy fracturing system also may include one or more mechanisms that will impart an aftward impulse to the severable region of the canopy once it has been severed and freed from the remainder of the canopy.

摘要翻译： 飞机冠层压裂系统包括具有前部和后部的顶盖以及可与篷盖分离的区域，以为飞机乘员的出口提供穿过其的开口。 可分割区域具有禁止可分割区域穿过冠层中产生的开口的形状，一旦可分割区域离开树冠并相对于顶盖向后移动。 冠层压裂系统还可以包括一个或多个机构，其将一旦被切断并且从冠层的其余部分中释放就会向顶篷的可分割区域赋予后向冲击。