FIELD: aviation technique. SUBSTANCE: aircraft has a wing with a span relative to a length L of the aeroplane, equal to 1, 43; propellers with diameter, consisting 1,4 of mean aerodynamic chord of wings. An area of the wing, being blown by propellers, consists 39%, skew angle of a fuselage β is equal to 13%. The wing has a center section and quickly releasable outer cells, providing simplified exploitation of the aeroplane upon it transportation and storage. Airflow of the wing provides lowered take-off run length and launching distance due to increased lift at taking-off. EFFECT: simplified storage and transportation of a the aircraft. 3 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE | 2000 |
|
RU2187444C2 |
FLYING VEHICLE | 2003 |
|
RU2311317C2 |
VERTICAL TAKE-OFF AND LANDING FLYING VEHICLE | 1997 |
|
RU2132289C1 |
AIRCRAFT (VERSIONS), TAKEOFF-LANDING GEAR (VERSIONS) AND METHOD OF LIFTING AIRCRAFT IN AIR (VERSIONS) | 2012 |
|
RU2588198C2 |
LONG DISTANCE SEARCH-AND-RESCUE FLOAT AMPHIBIAN SEA-PLANE OF TRIMARAN DESIGN "FREGAT" | 2006 |
|
RU2324627C2 |
HEAVY TRANSPORT FLOAT-TYPE SEA PLANE-AMPHIBIAN OF CATAMARAN CONFIGURATION | 2004 |
|
RU2314231C2 |
AVIATRANSFORMER | 2010 |
|
RU2444445C1 |
METHOD OF SERVICING COSMIC ARTICLES AND SHUTTLE AEROSPACE SYSTEM FOR ITS IMPLEMENTATION | 2007 |
|
RU2342288C1 |
ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
Authors
Dates
1994-11-30—Published
1992-10-08—Filed