| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed flying vehicle has fuselage (1), wing with outer wing panels (2) and (3) and profiled bracing struts (4 and 5) supporting the wing and having wing profile in section. Bracing struts (4 and 5) are secured to outer wing panels (2 and 3) for turning in spherical joints (6 and 7) and to fuselage (1) by means of cardan joints (8 and 9) whose free ends (10 and 11) are mounted on common shaft (12) provided with lever (13) which is connected with elevator control rod. ^ EFFECT: increase of lifting force due to availability of bracing struts in aerodynamic configuration of flying vehicle. ^ 5 dwg |
