FIELD: flying vehicle equipment.
SUBSTANCE: proposed aircraft has fuselage, lifting wing, power engines, supply system for these engines and landing gear. Fuselage has floor with compartments for detachable tanks which is located behind landing gear and in front of it. Each compartment is provided with hatches, mechanisms and units for securing the detachable tanks, connecting them to fuel supply system and disconnecting them from this system and jettisoning them.
EFFECT: enhanced safety of flight; improved aerodynamic characteristics.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
| HEAVY HIGH-SPEED ROTARY-WING AIRCRAFT | 2016 |
|
RU2608122C1 |
| TOURIST AIRCRAFT | 2002 |
|
RU2247681C2 |
| METHOD OF SERVICING COSMIC ARTICLES AND SHUTTLE AEROSPACE SYSTEM FOR ITS IMPLEMENTATION | 2007 |
|
RU2342288C1 |
| AMPHIBIA | 1999 |
|
RU2174080C2 |
| PILOTLESS AIRCRAFT | 2008 |
|
RU2380286C1 |
| MULTIPURPOSE LAND-BASED AIRCRAFT, METHOD OF ITS OPERATION AND INCIDENCE INDICATION SYSTEM | 2010 |
|
RU2443603C1 |
| MEDIUM AIRLINE AIRCRAFT | 1992 |
|
RU2078715C1 |
| LIGHT TWIN-ENGINED MULTI-PURPOSE AIRCRAFT LADOGA-9 FOR GROUND AND WATER BASES | 1994 |
|
RU2132290C1 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
