FIELD: aviation.
SUBSTANCE: method is based on airflow formation above the upper planes at the expense of using the upper planes of a louvers arranged so that the air cavities inside the wing are connected through the shutters (controlled synchronously with the louvers) with the suction cavities of jet turbine engines, which sucks airflow through the louvers, forming mobile air mass above the wings of non-moving aircraft. Rear wings are designed so that the air suction through the louvers is provided using the ejection method at the expense of suction action of exhaust gases through controlled shutters between air cavities of back wings and exhaust zone.
EFFECT: increase of aircraft wing lift.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF INCREASING AIRCRAFT WING LIFT | 2013 |
|
RU2515698C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL | 2018 |
|
RU2711760C2 |
| PROPULSOR, DISC CRAFT, DISC CRAFT LARGE CARRYING CAPACITY, UNDERWATER LIFT-PUSHER, PROPULSOR UNDERWATER VEHICLES | 2014 |
|
RU2586180C2 |
| 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 |
| TRANSPORT AIRCRAFT | 2011 |
|
RU2467924C1 |
| AIRCRAFT WING | 2024 |
|
RU2840556C1 |
| AIRCRAFT ENGINE AIR INTAKE | 2024 |
|
RU2833840C1 |
| AIRCRAFT ENGINE AIR INTAKE | 2023 |
|
RU2832863C1 |
| VERTICAL TAKEOFF AND LANDING AIRCRAFT | 2016 |
|
RU2630270C2 |
| FLYING VEHICLE, BOUNDARY LAYER SUCTION CONTROL SYSTEM, CONTROL SYSTEM OF INJECTION TO BOUNDARY LAYER, DEVICE FOR FIXING POSITION OF SHEDDING OF FLOW FROM TRAILING EDGE OF FUSELAGE AND ITS AIR CUSHION ALIGHTING GEAR | 1992 |
|
RU2033945C1 |
