FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft fuelling systems. Claimed system of fuel tanks comprises the series of multiple fuel tanks coupled by pipeline fittings. Said fittings connected the fuel tanks to ensure the cascade mode of fuel feed from one tank to the other in said series of tanks.
EFFECT: higher safety of system operation.
17 cl, 13 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CATALYTIC INERTING SYSTEM FOR AIRCRAFT WITH SEVERAL FUEL TANKS | 2017 |
|
RU2706753C1 |
| EMERGENCY RESCUE SYSTEM FOR RESCUE OF PASSENGERS, CREW AND CARGOES IN CASE OF IN-FLIGHT ACCIDENT | 1998 |
|
RU2152335C1 |
| TANKER AEROPLANE | 1994 |
|
RU2100257C1 |
| TANKER AEROPLANE | 1994 |
|
RU2142897C1 |
| FLYING VEHICLE FUEL SYSTEM WITH FLIGHT REFUELLING | 1991 |
|
SU1798986A1 |
| FUSELAGE POSITIONING MECHANISM (VERSIONS), AIRCRAFT AND AIRCRAFT BALANCING METHOD (VERSIONS) | 2018 |
|
RU2695754C1 |
| FLYING VEHICLE FUEL SYSTEM INCLUDING FLIGHT REFUELLING | 1990 |
|
SU1828027A1 |
| SYSTEM OF INVERTING AIRCRAFT FUEL TANK | 2013 |
|
RU2640265C2 |
| METHOD OF USE OF FUEL FROM TANK AND FUEL SYSTEM OF AIRCRAFT | 1992 |
|
RU2021168C1 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
