Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system
The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system ( 2 ), the aircraft electronics cooling system providing a thermal coupling between an electronic device ( 40 a , 40 b , 40 c , 40 d , 42, 44 ) to be cooled and the liquid cooling system ( 2 ) of the aircraft. A coolant delivered by the liquid cooling system ( 2 ) may flow through a board of the electronic device ( 40 a , 40 b , 40 c , 40 d ), through a heat sink on which the electronic device ( 42 ) is arranged and/or through a housing in which the electronic device ( 44 ) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.
1. An aircraft electronics cooling apparatus onboard an aircraft, the apparatus comprising:
a liquid cooling system onboard the aircraft, including a coolant circulating therein;
an electronic device to be cooled, mounted on a first member; and
a cooling conduit operatively connecting the first member to the liquid cooling system,
wherein the first member includes a circuit board that the electronic device is mounted upon, and wherein the board is in the form of a heat exchanger that is supplied with coolant from the liquid cooling system by a feed line of the cooling conduit and that discharges coolant to the liquid cooling system by a return line of the cooling conduit, thereby causing the coolant exiting the liquid cooling system to pass through the first member to cool the electronic device.
2. The aircraft electronics cooling apparatus of claim 1 , wherein the first member is configured such that the coolant from the liquid cooling system flows through the electronic device to be cooled and the circuit board.
3. The aircraft electronics cooling apparatus of claim 1 , wherein the first member further includes a heat sink coupled to the electronic device.
4. The aircraft electronics cooling apparatus of claim 3 , wherein the heat sink is surrounded along at least two sides with a plurality of electronic devices to be cooled.
5. The aircraft electronics cooling apparatus of claim 1 , wherein the coolant delivered by the liquid cooling system is permanently in the liquid state in the cooling conduit.
6. The aircraft electronics cooling apparatus of claim 1 , wherein the coolant delivered by the liquid cooling system vaporizes at least partially in the first member.
7. The aircraft electronics cooling apparatus of claim 1 , wherein the coolant delivered by the liquid cooling system is a dielectric liquid or an electrically non-conductive liquid.
8. A method for cooling an electronic device mounted on a first member in an aircraft having a liquid cooling system and a cooling conduit, the method comprising:
cooling a coolant in the liquid cooling system;
delivering cold coolant from the liquid cooling system via a feed line of the cooling conduit to the first member to cool the electronic device, the first member including a circuit board that the electronic device is mounted upon, such that the board is in the form of a heat exchanger that causes a flow of the coolant from the feed line to cool the electronic device; and
directing warm coolant from the first member via a return line of the cooling conduit back to the liquid cooling system.
9. The method of claim 8 , wherein delivering cold coolant from the liquid cooling system further comprises:
passing cold coolant through a heat sink coupled to the electronic device.
10. The method of claim 8 , wherein coolant passing through the cooling conduit is maintained in a liquid state.
11. The method of claim 8 , wherein coolant passing through the first member vaporizes at least partially in the first member.
12. The method of claim 8 , wherein delivering cold coolant from the liquid cooling system further comprises:
passing cold coolant through the electronic device to be cooled and the circuit board.