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Automatic thermal switchAn 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.
Document ID
19830020085
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Cunningham, J. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Wing, L. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 4, 2013
Publication Date
June 21, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
83N28356
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,388,965|NASA-CASE-GSC-12553-1
Patent Application
US-PATENT-APPL-SN-106192
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