Aircraft fuel system with heating of stored fuel
An aircraft fuel system comprises a fuselage tank and wing fuel tanks each connected to the fuselage fuel tank by a respective fuel line. A first fuel line connects the fuselage fuel tank to a collector fuel tank, which is connected by second fuel lines to aircraft engines in use of the system. Unspent fuel output from the aircraft engines is returned to the collector fuel tank via third fuel lines. A fuel line arrangement is arranged to draw fuel from, and return that fuel to, the wing fuel tanks. Fuel within the third fuel lines is thermally coupled to fuel within the fuel line arrangement by a heat exchanger. Heat energy within unspent fuel output from the aircraft engines is transferred to the wing fuel tanks, reducing the likelihood of fuel freezing within these tanks during extended flying in cold environments.
1. An aircraft fuel system, comprising:
a fuel storage tank arrangement,
a collector fuel tank arrangement,
a first fuel line connecting the fuel storage tank arrangement to the collector fuel tank arrangement, and
a second fuel line connecting the collector fuel tank arrangement to an aircraft engine in use of the aircraft fuel system,
wherein the aircraft fuel system further comprises a first heat-transfer arrangement arranged to transfer heat energy within unspent fuel output from the aircraft engine to fuel within the fuel storage tank arrangement,
wherein a third fuel line is provided that connects the aircraft engine to the collector fuel tank arrangement in use of the system, whereby at least a portion of unspent fuel output by the aircraft engine is returned to the collector fuel tank arrangement, and
wherein the first heat-transfer arrangement comprises:
a fuel line arrangement arranged to draw fuel from, and return that fuel to the fuel storage tank arrangement; and
a heat-exchanger is arranged to thermally couple fuel in the third fuel line to fuel in the fuel line arrangement.
2. The aircraft fuel system according to claim 1 , further comprising a second heat-transfer arrangement arranged to transfer heat energy from aircraft electronic equipment to fuel within the fuel storage tank arrangement.
3. The aircraft fuel system according to claim 2 , wherein the fuel storage tank arrangement comprises a fuselage fuel tank and a wing fuel tank connected by a fuel line, wherein:
the first fuel line connects the fuselage fuel tank to the collector tank arrangement; and
the fuel line arrangement is arranged to draw fuel from, and return that fuel to, the wing fuel tank.
4. The aircraft fuel system according to claim 2 , wherein the second heat transfer arrangement comprises a fuel line arrangement arranged to draw fuel from, and return that fuel to, the fuel storage tank arrangement and a heat exchanger arranged to couple heat from the aircraft electronic equipment to fuel within the fuel line arrangement.
5. The aircraft fuel system according to claim 4 , wherein the heat exchanger is in thermal contact with a compressor arranged to compress a refrigerant fluid within a cooling circuit for cooling the aircraft electronic equipment.
6. The aircraft fuel system according to claim 4 , wherein the fuel storage tank arrangement comprises a fuselage fuel tank and a wing fuel tank connected by a fuel line, wherein:
the first fuel line connects the fuselage fuel tank to the collector tank arrangement; and
the fuel line arrangement is arranged to draw fuel from, and return that fuel to, the wing fuel tank.
7. An aircraft fuel system, comprising:
a fuel storage tank arrangement including a wing tank and a fuselage tank,
a collector fuel tank arrangement,
an aircraft engine,
a first fuel line connecting the fuel storage tank arrangement to the collector fuel tank arrangement,
a second fuel line connecting the collector fuel tank arrangement to the aircraft engine in use of the aircraft fuel system,
a third fuel line connecting the aircraft engine to the collector tank arrangement in use of the system, whereby at least a portion of unspent fuel output by the aircraft engine is returned to the collector fuel tank arrangement,
a fuel line arrangement arranged to draw fuel from the fuel storage tank arrangement, heat the fuel in a recycle fuel line, and return the fuel to the fuel storage tank arrangement, and
a heat-exchanger arranged to thermally couple the unspent fuel output by the aircraft engine in the third fuel line to the fuel in the recycle line, whereby cooled fuel is fed to the collector fuel tank arrangement by the third fuel line and heated fuel is fed to the fuel storage tank arrangement by the recycle fuel line.
8. The aircraft fuel system according to claim 7 , wherein the first fuel line connects the fuselage tank to the collector fuel tank arrangement.
9. The aircraft fuel system according to claim 7 , wherein the recycle line returns the heated fuel directly to the wing tank.