FIELD: air transport.
SUBSTANCE: aircraft is equipped with aircraft engines in engine nacelles attached to the aircraft symmetrically relative to its longitudinal axis. Aerodynamic channel is made in hull aft body the end hull aft there made is though the end of which is connected to the hole made in the hull aft body. Bottom of fuselage aft part is provided with an opening closed with bottom gates with detachable shutters suspended on lateral sides of the opening ending with the hole made on the hull end. Aircraft flight method is characterised by aircraft purpose.
EFFECT: decreasing noise level.
6 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TAIL SECTION OF AEROPLANE AND METHOD FOR REDUCING THE AIR FLOW SWIRLINGS | 2002 |
|
RU2274584C2 |
| TRANSFORMER WITH INCREASED DISSIPATION | 1991 |
|
RU2025810C1 |
| HIGH-VOLTAGE TRANSFORMER | 0 |
|
SU838769A1 |
| TRANSFORMER | 0 |
|
SU1046785A1 |
| TRANSFORMER | 0 |
|
SU815778A1 |
| MULTISTATION UNIT FOR SUPPLING POWER TO LOAD | 0 |
|
SU804279A1 |
| STEALTH SHORT TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2705416C2 |
| AIR-CUSHION VEHICLE - THE VEHICLES CARRIER | 2017 |
|
RU2658545C1 |
| SUPERSONIC LOW-VISIBILITY AIRCRAFT-HELICOPTER | 2018 |
|
RU2692742C1 |
| SUPERSONIC AIRCRAFT (VERSIONS) | 2007 |
|
RU2391254C2 |
