FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to mid-wing hydroplane. Proposed hydroplane has wings and engines mounted above the wings. Engine nacelles support mid-wing to add to structural strength and stiffness and to improve hydroplane gliding properties. Easily removable mid-wing allows its mounting to increase hydroplane load lifting capacity. Mid-wing length can either be restricted by nacelles or extends beyond them.
EFFECT: improved gliding properties, take-off and landing speed and possibility to arrange extra fuel tank in mid-wing cavity.
2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MINIATURE AIRPLANE | 2006 |
|
RU2327605C1 |
| LONG DISTANCE SEARCH-AND-RESCUE FLOAT AMPHIBIAN SEA-PLANE OF TRIMARAN DESIGN "FREGAT" | 2006 |
|
RU2324627C2 |
| CONTROLLED-LIFT WING | 2007 |
|
RU2380278C2 |
| HEAVY TRANSPORT FLOAT-TYPE SEA PLANE-AMPHIBIAN OF CATAMARAN CONFIGURATION | 2004 |
|
RU2314231C2 |
| TRIPLE-WING AIRCRAFT | 2006 |
|
RU2319642C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| SUPERSONIC AIRCRAFT WITH CLOSED STRUCTURE WINGS | 2015 |
|
RU2591102C1 |
| MODULAR FIGHTER | 2009 |
|
RU2400395C1 |
| SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING | 2016 |
|
RU2632782C1 |
| NACELLE WITH INNER WING | 2009 |
|
RU2389653C1 |
