Heat transfer of a remote heat source using a loop heat pipe
View Patent ↗Heat transfer systems and methods 30 for use on a spacecraft that use a loop heat pipe to transfer heat from a remotely located heat source to a thermal radiator or other heat dissipating apparatus. The loop heat pipe is a two phase heat transfer device that has an evaporator coupled to the heat source and a condenser coupled to the thermal radiator or other heat dissipating apparatus. The loop heat pipe comprises thin walled tubing to connect the evaporator and condenser. The thin walled tubing allows the loop heat pipe to be flexible. This flexibility offers significant advantages in terms of routing and accommodating design
1. A heat transfer system comprising:
a spacecraft comprising a heat dissipating system;
a remotely-located heat source disposed on the spacecraft at a location that is remote from the heat dissipating system and which is not located on a heat pipe panel; and
a loop heat pipe thermally coupled between the remotely-located heat source and the heat dissipating system for coupling heat generated by the heat source to the heat dissipating system.
2. The heat transfer system recited in claim 1 wherein the loop heat pipe comprises flexible thin walled tubing coupled between an evaporator that is thermally coupled to the remotely-located heat source and a condenser that is thermally coupled to the heat dissipating system.
3. The spacecraft recited in claim 2 wherein the loop heat pipe comprises flexible thin walled tubing coupled between an evaporator that is thermally coupled to the remotely-located heat source and a condenser that is thermally coupled to heat dissipating system.
4. A spacecraft comprising:
a heat dissipating system for radiating heat into space;
a remotely-located heat source disposed at a location that is remote from the heat dissipating system and which is not located on a heat pipe panel; and
a loop heat pipe thermally coupled between the remotely-located heat source and the heat dissipating system for coupling heat generated by the remotely-located heat source to the heat dissipating system.
5. A heat dissipation method for use on a spacecraft comprising the steps of:
disposing a remotely-located heat source on a spacecraft at a location that is remote from a heat dissipating system and which is not located on a heat pipe panel;
thermally coupling a loop heat pipe between the remotely-located heat source and the heat dissipating system; and
coupling heat generated by the remotely-located heat source to the heat dissipating system by way of the loop heat pipe.
6. The method recited in claim 5 wherein the loop heat pipe comprises flexible thin walled tubing coupled between an evaporator that is thermally coupled to the remotely-located heat source and a condenser that is thermally coupled to heat dissipating system.