FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Aircraft comprises brake flap 10 to extend into surrounding air flow. Said brake flap is mounted on fuselage 12 above the wings wherein local maximum of aerodynamic air pressure exists. Brake flap allows equalise the moments in downward and upward pitches. Proposed method consists in using said brake flap.
EFFECT: creation of aerodynamic resistance without applying extra moment.
8 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| DEVICE AND METHOD TO DESCRIBE LIFT | 2006 |
|
RU2399553C2 |
| METHOD OF IMPROVING AIRCRAFT MANOEUVRING CHARACTERISTICS DURING FINAL STAGE OF RUNWAY APPROACH BEFORE LANDING AND SUBSEQUENT FLAREOUT (VERSIONS) | 2005 |
|
RU2384874C2 |
| METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD | 2010 |
|
RU2539443C2 |
| METHOD OF CREATING SYSTEM OF FORCES OF AIRCRAFT OF AEROPLANE CONFIGURATION AND GROUND-AIR AMPHIBIOUS VEHICLE FOR IMPLEMENTING THIS METHOD | 1998 |
|
RU2127202C1 |
| 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 |
| WING-IN-GROUND-EFFECT CRAFT | 2003 |
|
RU2286268C2 |
| LIGHT FLYING VEHICLE | 1995 |
|
RU2082651C1 |
| AIRCRAFT CONTROL SYSTEM | 2007 |
|
RU2364548C2 |
