FIELD: aviation. SUBSTANCE: wing includes primary structure assembled from flexible spars interconnected by means of transversal strainers and bracket with flange. Wing tip is provided with weighting material for dampening breaking vibrations. Bracket is provided with set of load-bearing tubes rigidly secured on flange; ends of spars are telescopically inserted in ends of these tubes. Provision is made for change of wing profile to profile of propeller blade. EFFECT: enhanced efficiency. 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE | 1999 |
|
RU2155144C1 |
| FLYING VEHICLE WING MOTION DRIVE | 1998 |
|
RU2151715C1 |
| DRAGON-FLY FLYING VEHICLE | 1993 |
|
RU2083437C1 |
| AIRCRAFT CREATING LIFTING FORCE | 2015 |
|
RU2621780C1 |
| AEROSTAT TRAJECTORY CONTROL SYSTEM | 1999 |
|
RU2238217C2 |
| FLAPPING DIAPHRAGM-TYPE PROPULSOR (VERSIONS) AND FLAPPING AIRCRAFT ON ITS BASE | 1996 |
|
RU2123455C1 |
| METHOD OF STRAIGHT-AND-LEVEL FLAPPING FLIGHT | 1996 |
|
RU2129506C1 |
| METHOD OF PREPARING REMOTE COMBAT OPERATIONS | 2023 |
|
RU2812501C1 |
| FLYING VEHICLE WITH ENGINE IN FORM OF FLAPPING WINGS | 2002 |
|
RU2217355C1 |
| UAV FROM UNIFIED PARTS AND ASSEMBLIES MANUFACTURED BY INJECTION MOLDING, AND METHOD OF ITS MANUFACTURING | 2023 |
|
RU2814641C1 |
