| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to maneuvering aircraft and their control systems. Maneuvering aircraft comprises fuselage, swept wing, front wing-root extensions, control components and undercarriage. Said front wing-root extensions are arranged in fuselage head-to-tail joint and equipped with controlled rotary airfoils. Wing-root extension controlled surface turn axes are perpendicular or angularly to aircraft wing surface.EFFECT: higher safety and combat efficiency, better relationship between lift and drag.3 dwg |
