FIELD: aircraft engineering.
SUBSTANCE: miniature remote-control aircraft comprises airfoil (17), two screw propellers (12, 13) and weight (20), its position being varied to vary the centre of gravity of miniature aircraft (10). Airfoil (17) is located above the plane defined by rotational axes of screw propellers (12, 13) to develop the lift. Airfoil (17) is composed of a top airfoil (17) arranged above bottom airfoil (18). This miniature aircraft represents a flying wing design. Aircraft in-flight position with respect to lengthwise axis (25) and/or aircraft (10) vertical axis (11) can be adjusted by the difference in propulsion, preferably between rpm of screw propellers (12, 13). If used as a reconnaissance plane it can be equipped with monitoring means.
EFFECT: compact and durable structure with perfected flight characteristics.
11 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRBORNE MICRODEVICE | 2007 |
|
RU2339543C1 |
DEVICE FOR INTERCEPTION OF UNMANNED AERIAL VEHICLES | 2020 |
|
RU2738383C2 |
AIRCRAFT CAPABLE OF VERTICAL TAKE-OFF | 2016 |
|
RU2704771C2 |
VERTICAL TAKEOFF AND LANDING AIRCRAFT | 2016 |
|
RU2627220C1 |
DEVICE FOR AERODYNAMIC LIFTING OF THE PAYLOAD | 2021 |
|
RU2765196C2 |
COMBINED AIRCRAFT | 2005 |
|
RU2380276C2 |
UNMANNED INTERCEPTOR | 2020 |
|
RU2741142C2 |
MODULAR UNMANNED AERIAL VEHICLE WITH TRACTION PROPELLERS PROTECTION SYSTEM | 2020 |
|
RU2752110C1 |
UNMANNED AERIAL VEHICLE-INTERCEPTOR | 2024 |
|
RU2825353C1 |
HEAVY HIGH-SPEED ROTARY-WING AIRCRAFT | 2016 |
|
RU2608122C1 |
Authors
Dates
2015-04-20—Published
2012-02-08—Filed