The invention discloses an aircraft provided with strake wings. The aircraft comprises the strake wings, an elastic body and a spring pin, two convex circular truncated cones are arranged at the bottom ends of the edging wings, and pin holes are formed in the side walls of the circular truncated cones; two sides of the projectile body are respectively milled to form a plane, round holes are respectively formed in the planes, and the two convex circular truncated cones are respectively assembled with the round holes in the planes milled on the two sides; an open hole is formed in the side wall of the round hole, and a spring pin is fixed between the pin hole and the open hole. The range of the aircraft can be increased, and a certain guidance effect on reduction of engine charge is achieved.
本公开的安装有边条翼的飞行器,包括边条翼、弹体和弹簧销;边条翼底端设置有两个凸起的圆台,圆台侧璧设有销孔;弹体的两侧分别铣出一平面,平面上分别设有圆孔,两个凸起的圆台分别与两侧铣出的平面上的圆孔相装配;圆孔侧壁上设有开孔,所述销孔和所述开孔之间固定有弹簧销。能够提升了飞行器的射程,对降低发动机装药也有一定制导作用。
Aircraft provided with strake wings
一种安装有边条翼的飞行器
2022-01-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Approximate Analysis of Strake Wings at Low Speeds
AIAA | 1979
|Hinged Strake Aircraft Control System
NTIS | 1982
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