FIELD: aviation; hang gliders. SUBSTANCE: flying vehicle has wing of closed volumetric profile formed by fabric skin secured on truss formed by two closed circular tubes 1 and 2 having form of ellipse in plan and fin tube 3 connected with circular tube 1 in nose attachment unit and with circular tube 3 in central attachment unit at different angles relative to tube 3 at side view. EFFECT: enhanced aerodynamic efficiency, longitudinal and lateral stability and controllability due to location of stabilizing surfaces beyond wake of lifting surface. 5 dwg
Title | Year | Author | Number |
---|---|---|---|
FLIGHT VEHICLE | 0 |
|
SU1835371A1 |
BALANCED FLYING VEHICLE | 1992 |
|
RU2089462C1 |
FLYING VEHICLE WITH BALANCING CONTROL | 1995 |
|
RU2110447C1 |
WING OF MULTI-PURPOSE SUPERLIGHT FLYING VEHICLE | 2001 |
|
RU2208541C1 |
FLYING VEHICLE | 1997 |
|
RU2148528C1 |
BALANCE-BEAM GLIDER | 0 |
|
SU891501A1 |
DELTAPLANE | 0 |
|
SU1121181A1 |
SUPERLIGHT FLYING VEHICLE | 0 |
|
SU1759728A1 |
MOTOR DELTAPLANE | 1982 |
|
SU1047089A1 |
DELTA-PLANER | 0 |
|
SU1752657A1 |
Authors
Dates
1997-07-10—Published
1993-03-29—Filed