Automatic thermal switch
Abstract
An automatic thermal switch to control heat flow includes two thermally conductive plates and a thermally conductive switch saddle pivotally mounted to the first plate. A flexible heat carrier is connected between the switch saddle and the second plate. A phase-change power unit, including a piston coupled to the switch saddle, is in thermal contact with the first thermally conductive plate. A biasing element biases the switch saddle in a predetermined position with respect to the first plate. When the phase-change power unit is actuated by an increase in heat transmitted through the first place, the piston extends and causes the switch saddle to pivot, thereby varying the thermal conduction between the two plates through the switch saddle and flexible heat carrier. The biasing element, switch saddle, and piston can be arranged to provide either a normally closed or normally opened thermally conductive path between the two plates.
- Publication:
-
National Aeronautics and Space Administration Report
- Pub Date:
- June 1983
- Bibcode:
- 1983nasa.reptR....C
- Keywords:
-
- Automatic Control;
- Electric Switches;
- Heat Transfer;
- Spacecraft Environments;
- Temperature Control;
- Thermal Conductivity;
- Armatures;
- Disconnect Devices;
- Electromechanical Devices;
- Heat Pipes;
- Patents;
- Pistons;
- Fluid Mechanics and Heat Transfer