FIELD: aeronautical engineering.
SUBSTANCE: aerodynamic control of the aircraft includes an upper surface and a lower surface containing a tangential air blowing nozzle. The upper surface of the aerodynamic control additionally contains at least one air blowing nozzle located on the upper side of the surface of the aerodynamic control opposite the tangential blowing nozzle.
EFFECT: aerodynamic control of the aircraft has been developed, which ensures reduced magnitude of the hinge moment.
4 cl, 6 dwg
| Title |
Year |
Author |
Number |
| METHOD FOR CHANGING CHARACTERISTICS OF AERODYNAMIC CONTROL ELEMENT OF UNMANNED AERIAL VEHICLE |
2022 |
- Pavlenko Olga Viktorovna
- Kornushenko Aleksandr Vyacheslavich
|
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| 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 |
- Maksimov Nikolaj Ivanovich
|
RU2349505C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL |
2018 |
- Sychev Vladimir Borisovich
- Ambrozhevich Aleksandr Vladimirovich
- Pshichenko Dmitrij Viktorovich
- Kartashev Andrej Sergeevich
- Kornev Aleksej Vladimirovich
- Karavaev Nikolaj Andreevich
- Sychev Sergej Vladimirovich
- Kulikov Boris Mikhajlovich
- Grishchenko Aleksandr Vladimirovich
- Migalin Konstantin Valentinovich
- Sidenko Aleksej Ilich
- Sereda Vladislav Aleksandrovich
|
RU2711760C2 |
| CONTROL SURFACE |
2018 |
- Pavlenko Olga Viktorovna
- Barinov Vladimir Akindinovich
|
RU2702480C2 |
| HYBRID AIRSHIP |
1995 |
|
RU2092381C1 |
| FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS |
2010 |
- Maksimov Nikolaj Ivanovich
|
RU2466061C2 |
| METHOD OF CREATING SYSTEM OF FORCES OF AIRCRAFT OF AEROPLANE CONFIGURATION AND GROUND-AIR AMPHIBIOUS VEHICLE FOR IMPLEMENTING THIS METHOD |
1998 |
|
RU2127202C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
1999 |
|
RU2162809C2 |
| AIRCRAFT |
2007 |
- Bykovskij Sergej Ivanovich
- Pavlov Viktor Andreevich
|
RU2378156C2 |
| 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 |
- Shchukin L.N.
- Savitskij A.I.
- Shchukin I.L.
- Mass A.M.
- Karelin V.G.
- Shibanov A.P.
- Sobko A.P.
- Ermishin A.V.
- Khutsishvili V.G.
- Pushkin R.M.
- Fishchenko S.V.
|
RU2033945C1 |
