Drain system for an aircraft
View Patent ↗Drain masts of commercial aircraft need to be heated in order to prevent freezing caused by the low outside temperatures when the aircraft travels at a corresponding altitude. An exemplary embodiment described in the application pertains to a drain system for an aircraft that can be used for draining liquids or gases from the aircraft or for drawing air into the aircraft. In this case, the liquids or gases are heated by means of a coolant that receives its thermal energy from a thermal or electrochemical process being carried out on board the aircraft. Consequently, the waste heat produced by the thermal or electrochemical process being carried out on board the aircraft, for example, a fuel cell process, can be carried off outboard via the drain system. In addition, the coolant can be advantageously utilized for cooling the thermal or electrochemical process.
1. A drain system for an aircraft, comprising:
a mast arranged and operable to perform at least one of: (1) drawing ram air into the aircraft, and (2) draining liquids or gases from the aircraft, the mast further being operable to deliver the ram air to a thermal or electrochemical process being carried out on board the aircraft;
a change-over valve operable to deliver cabin air to the thermal or electrochemical process alternatively or additionally to the ram air;
an air compressor operable to compress air to be delivered to the thermal or electrochemical process;
a pressure control unit operable to regulate the pressure of the air to be delivered to the thermal or electrochemical process; and
a tubing containing a coolant; the tubing being positioned and operable to conduct a portion of the heat generated by the coolant to heat the mast; the tubing being further positioned and operable to deliver the coolant to the thermal or electrochemical process; and
the tubing being further positioned and operable to conduct a portion of the heat generated by the thermal or electrochemical process to heat the coolant.
2. The drain system of claim 1 , wherein:
the mast has an end region that is angled relative to the aircraft heading by an angle between approximately 0° and 45° and the mast is operable to draw air into the aircraft such that the air speed of the traveling aircraft causes dynamic pressure to build up in the mast; and
the pressure control unit is operable to regulate a dynamic pressure of the air.
3. The drain system of claim 1 , further comprising:
a cooling surface positioned and operable to cool the coolant by the cooling surface before the coolant is delivered to the thermal or electrochemical process.
4. The drain system of claim 1 ,
wherein liquids to be drained comprise gray water accumulated on board the aircraft during its operation; and
the gases to be drained comprise exhaust air produced by the thermal or electrochemical process.
5. The drain system of claim 1 ,
wherein the mast penetrates a skin of the aircraft; and
at least part of the drain system is arranged outside the aircraft on an underside of the aircraft fuselage.
6. The drain system of claim 1 , further comprising:
an electric heater which is operable to further heat the mast.
7. The drain system of claim 1 , further comprising:
a heat pump operable to be switched on to increase heating power for heating the mast or cooling power for cooling the thermal or electrochemical process.
8. An aircraft comprising a drain system of claim 1 .
9. The drain system of claim 1 , further comprising:
a fuel cell operable to perform the thermal or electrochemical process.
10. The drain system of claim 1 , wherein the tubing forms a closed loop which does not enter or exit a device performing the thermal or electrochemical process.
11. A drain system for an aircraft, comprising:
a mast arranged and operable to perform at least one of: (1) drawing air into the aircraft, and (2) draining liquids or gases from the aircraft, the mast having an end region that is angled relative to the aircraft heading by an angle between approximately 0° and 45° and the mast is operable to draw air into the aircraft such that the air speed of the traveling aircraft causes a dynamic pressure to build up in the mast;
one of a heat exchanger and a tubing containing a coolant and being positioned and operable to heat the mast;
an air compressor operable to generate the dynamic pressure;
a pressure control unit operable to regulate the dynamic pressure; and
a change-over valve operable to switch the air compressor to receive cabin air.