Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
7050599 | Applied Thermal Engineering | 2013 | 6 Pages |
Abstract
⺠A passive cooling system has been developed for avionics application. ⺠The system consists of loop thermosyphons and a passenger seat as a heat sink. ⺠Successful system tests have been run at heat loads to 100 W and angle tilts to 20°.
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Fluid Flow and Transfer Processes
Authors
C. Sarno, C. Tantolin, R. Hodot, Yu. Maydanik, S. Vershinin,