초록 ▼

The invention is a rotary launcher system for an aircraft having a weapon bay with an opening in communication with the exterior of the aircraft. The system comprises a plurality of doors which are mounted to the aircraft and movable from an open position to a closed position. In the closed position

The invention is a rotary launcher system for an aircraft having a weapon bay with an opening in communication with the exterior of the aircraft. The system comprises a plurality of doors which are mounted to the aircraft and movable from an open position to a closed position. In the closed position the doors seal off part of the opening and form a portion of the external contour of the aircraft. The rotary launcher is mounted within the weapon bay which includes a frame member rotatively mounted therein. A plurality of weapon mounting assemblies are attached to the frame member at discrete locations and are sequentially alignable with the opening upon rotation of the frame member. Barrier assemblies are mounted to the frame member, which cooperate with the plurality of doors, sealing off the weapon bay from the exterior of the aircraft when any one of the plurality of assemblies is aligned with the opening. Preferably, this system includes at least one cover assembly mounted to the rotary launcher for covering the remaining portion of the opening when at least one of the plurality of missile mounting assemblies is aligned with the opening. The rotary launcher cooperates with the plurality of doors to form a portion of the external contour extending completely over the opening.

대표청구항 ▼

A rotary launcher system for an aircraft having a weapon bay, said weapon bay having an opening in communication with the exterior of the aircraft, the system comprising: a plurality of doors mounted on said aircraft movable from an open position to a closed position sealing off a portion of the ope

A rotary launcher system for an aircraft having a weapon bay, said weapon bay having an opening in communication with the exterior of the aircraft, the system comprising: a plurality of doors mounted on said aircraft movable from an open position to a closed position sealing off a portion of the opening and forming a portion of the external contour of the aircraft over the opening; and a rotary launcher comprising: a frame member rotatively mounted within the weapon bay; a plurality of weapon mounting assemblies mounted to said frame member at discrete locations thereabout and sequentially alignable with the opening upon rotation of said frame member, said weapon mounting assemblies adapted to mount at least one missile; and barrier means mounted to said frame member cooperating with said plurality of doors for sealing off the weapon bay from the exterior of the aircraft when any of said plurality of assemblies is aligned with the opening.