FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft fuel tank assy, aircraft incorporating said fuel tank and set of parts for production of said tank. Aircraft fuel tank assembly 101 comprises fuel tank 102, container 11 and fuel pump 103. Fuel pump assy 103 comprises drive motor 104, pump 105 and electronic unit 106. The latter and container 11 are arranged to form dry compartment 115 between electronic unit and container.
EFFECT: improved design thanks to production of dry compartment between electronic unit and container.
14 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CATALYTIC INERTING SYSTEM FOR AIRCRAFT WITH SEVERAL FUEL TANKS | 2017 |
|
RU2706753C1 |
| AIRCRAFT FUEL PUMP | 2016 |
|
RU2712143C2 |
| VALVE OF AIRCRAFT FOR DRAINAGE OF WATER, FUEL TANK OF AIRCRAFT, AIRCRAFT AND PROCEDURE FOR DRAINING WATER FROM FUEL TANK OF AIRCRAFT | 2006 |
|
RU2429399C2 |
| SYSTEM OF INVERTING AIRCRAFT FUEL TANK | 2013 |
|
RU2640265C2 |
| AIRCRAFT FUEL TANK | 2010 |
|
RU2492108C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER PLANT | 2017 |
|
RU2724940C2 |
| SYSTEMS AND METHODS FOR MAINTENANCE OF COMPLIANCE WITH REQUIREMENTS TO STRUCTURAL LOAD OF AIRCRAFT EXTRA FUEL TANK | 2011 |
|
RU2578843C2 |
| RECOVERABLE LAUNCH VEHICLE AND MULTIPLE CONFIGURRATION TRANSPORTATIOON SYSTEM | 1991 |
|
RU2035358C1 |
| AIRCRAFT | 2011 |
|
RU2470834C1 |
| METHOD OF OPERATING AIRCRAFT, METHOD OF FUEL AMOUNT INDICATION, COMPUTER SYSTEM FOR CALCULATION OF FUEL AMOUNT, AIRCRAFT FUEL TANK ASSEMBLY AND FUEL AMOUNT PROCESSOR CONTROL ELEMENT | 2006 |
|
RU2395433C2 |
