FIELD: aeronautical engineering; design of light single-engine multi-purpose aeroplanes. SUBSTANCE: aircraft includes wing with flaps, front and rear horizontal tail units and power plant with pusher propeller. Front horizontal tail unit is mounted above wing and is provided with flaps operated by common drive with flaps. Projection of rear horizontal tail unit on plane of rotation of pusher propeller intersects propeller area. EFFECT: reduced dependence of longitudinal stability of aircraft controllability on its CG position; improved dynamic characteristics and ease of piloting. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| VTOL AIRCRAFT | 2006 |
|
RU2350510C2 |
| HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
| PASSENGER AEROPLANE OF TRIPLANE CONFIGURATION | 1998 |
|
RU2132291C1 |
| LONG DISTANCE SEARCH-AND-RESCUE FLOAT AMPHIBIAN SEA-PLANE OF TRIMARAN DESIGN "FREGAT" | 2006 |
|
RU2324627C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| UNMANNED HIGH-SPEED HELICOPTER-AIRPLANE | 2017 |
|
RU2664024C2 |
| TRAINER AEROPLANE | 1996 |
|
RU2100251C1 |
| MULTIPURPOSE HELICOPTER AIRPLANE WITH REMOTE CONTROL | 2008 |
|
RU2370414C1 |
| MULTIROTOR HIGH-SPEED HELICOPTER-AIRCRAFT | 2017 |
|
RU2658736C1 |
| UNMANNED FLYING VEHICLE (VARIANTS) | 2002 |
|
RU2213024C1 |
