FIELD: aviation.
SUBSTANCE: proposed aircraft has fuselage, two half-wings, jet engine, vertical and horizontal stabilizers and landing gear. Each half-wing has through passages of rectangular section which are parallel relative to each other along half-wing span. Each through passage has lower passage whose inlet hole is located on lower surface of half-wing; upper passage is narrower as compared with lower passage and its outlet hole is located on upper surface of half-wing.
EFFECT: increased lifting force of half-wing.
8 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| TRANSPORT AIRCRAFT | 2005 | 
 | RU2284948C1 | 
| AIRCRAFT WITH PLATE-TYPE WING | 2000 | 
 | RU2190557C2 | 
| TRANSPORT AIRCRAFT | 1995 | 
 | RU2086478C1 | 
| AEROPLANE WITH JET WINGS | 2007 | 
 | RU2331549C1 | 
| TRANSPORT AIRCRAFT | 2006 | 
 | RU2305651C1 | 
| TRANSPORT AIRCRAFT | 2019 | 
 | RU2703324C1 | 
| INCREASE-LIFT-WING AIRCRAFT | 2008 | 
 | RU2385259C1 | 
| COMBINED CONFIGURATION AIRCRAFT WITH GAS-TURBINE ENGINE | 2000 | 
 | RU2190558C2 | 
| AIRCRAFT WITH LIFTING FUSELAGE | 1999 | 
 | RU2168446C2 | 
| AIRCRAFT | 1999 | 
 | RU2160211C2 | 
Authors
Dates
2006-11-20—Published
2005-04-26—Filed