FIELD: engines and pumps.
SUBSTANCE: proposed biplane consists of fuselage, wings, engines, control cabin, tail assembly, landing gear, ailerons and flaps. Wing with air spreaders is mounted atop the fuselage to secure flaps and ailerons thereto. Trough wings are arranged at fuselage bottom to carry turbojet engines attached atop said wings. Reduced pressure and flow density are created inside said wing.
EFFECT: increased airlift, speed and range.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2005 |
|
RU2288137C1 |
| AIRCRAFT | 2008 |
|
RU2364547C1 |
| AIRCRAFT | 2005 |
|
RU2283261C1 |
| AIRCRAFT WING | 2009 |
|
RU2409503C1 |
| AIRCRAFT WING | 2015 |
|
RU2601093C1 |
| AIRCRAFT WING | 2014 |
|
RU2555079C1 |
| AIRCRAFT WING | 2012 |
|
RU2533771C2 |
| AIRCRAFT WING | 2013 |
|
RU2551829C2 |
| AIRCRAFT WING | 2011 |
|
RU2465172C1 |
| METHOD OF CREATING AIRCRAFT LIFT (VERSIONS), METHOD OF FLIGHT, NON-AERODYNAMIC ALL-WEATHER VTOL AIRCRAFT "MAXINIO" (VERSIONS), METHODS OF TAKE-OFF AND LANDING, AICRAFT CONTROL METHOD AND SYSTEM, FUSELAGE, WING (VERSIONS), THRUST REVERSE AND METHOD OF ITS OPERATION, LANDING GEAR SYSTEM, GAS SEPARATION AND DISTRIBUTION SYSTEM | 2007 |
|
RU2349505C1 |
