公开(公告)号：US3669385A

公开(公告)日：1972-06-13

申请号：US3669385D

申请日：1970-10-08

Applicant: FAIRCHILD INDUSTRIES

Inventor： GLANTZ EARL ,  MCCOMAS JEAN W

IPC: B64C1/00 ,  B64C39/02 ,  B64D5/00 ,  B64C1/26

CPC classification number: B64D5/00 ,  B64C1/00 ,  B64C39/024 ,  B64C2001/0045 ,  B64C2201/048 ,  B64C2201/104 ,  B64C2201/128 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/167 ,  B64C2201/185

Abstract: An aircraft of improved of simplified construction having forward and aft generally cylindrical and substantially identical fuselage sections that are connected to a central fuselage section that houses an engine that has an inlet located above the forward fuselage section for powering the aircraft in flight. The central long axis of the aft fuselage section is located above the central long axis of the forward fuselage section. Wings are connected to the central fuselage section and a tail assembly is connected to the aft portion of the aft fuselage section. Many of the component parts of the aircraft are interchangeable and the aircraft is especially suited for use as a drone for towing aerial targets.

Abstract translation: 具有改进的简化结构的飞机具有前后大体上圆柱形和基本相同的机身部分，其连接到中央机身部分，该中央机身部分容纳具有位于前机身部分上方的入口的发动机，用于为飞行器提供动力。 后部机身部分的中心长轴位于前机身部分的中心长轴上方。 翼连接到中央机身部分，尾部组件连接到后机身部分的后部。 飞机的许多组成部分是可互换的，飞机特别适用于作为无人驾驶用于拖曳空中目标的飞机。