| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed aircraft has fuselage (1) with tail unit, wing (13) and engine with propeller. Arranged in nose section of fuselage (1) is engine nacelle (6) with engine. Mounted underneath fuselage (1) along straight line of its contour (10) are front legs (8) and tail leg (11) of landing gear with castoring tail wheel. Wing (13) reinforced with bracing struts (14) is mounted in upper section of fuselage (1) above crew and passenger cabin (12). Attachment unit of wing (13) lies on one straight line with attachment units securing the landing gear legs to fuselage (1). Upper surface of profile of wing (13) coincides with upper surface of profile of its fuselage (1). ^ EFFECT: enhanced aerodynamic efficiency; reduced takeoff weight. ^ 5 dwg |
