FIELD: various aeroplanes for running-type take-off and landing. SUBSTANCE: aircraft is provided with auxiliary surfaces at relative thickness of 20 to 60 percent over which intensive slotted jets flow at jet pulse coefficient more than 1.5. Aircraft is also provided with engine thrust vector deflection system or additional auxiliary high- lift surfaces for balancing nose-up moment created by extensible aerodynamic surfaces. EFFECT: reduction of additional weight losses for bases not provided with aerodromes at short poorly prepared areas by 5 to 10 times as compared with vertical take-off and landing aircraft at similar performance. 3 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ENHANCING LIFT QUALITIES OF WINGS | 1995 |
|
RU2104220C1 |
| SHORT TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2728017C2 |
| ACTIVE SYSTEM FOR CONTROL OF LIFTING FORCE | 1994 |
|
RU2086469C1 |
| FAIRING OF EXTENSION AND RETRACTION MECHANISM FOR EXTENSION FLAPS | 1995 |
|
RU2085441C1 |
| MULTI-PURPOSE TWIN-ENGINED SEA-BASED AND LAND- BASED AIRCRAFT OF SHORT TAKEOFF AND LANDING | 2001 |
|
RU2196707C2 |
| SILENCING NOZZLE OF AIR-JET ENGINE | 1993 |
|
RU2092708C1 |
| HIGH SPEED AND MANEUVERABILITY ROTORCRAFT | 2012 |
|
RU2480379C1 |
| TWIN-ENGINED MANEUVERABLE AEROPLANE CONTROL SYSTEM | 1996 |
|
RU2099244C1 |
| AIRCRAFT | 1993 |
|
RU2076826C1 |
| MULTI-SCREW UNMANNED ROTORCRAFT | 2016 |
|
RU2611480C1 |
