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Investigation of Capillary Limit in a Loop Heat PipeThis paper presets an experimental study on the capillary limit of a loop heat pipe (LHP) at low powers. The slow thermal response of the loop at low powers made it possible to observe interactions among various components after the capillary limit was exceeded. The capillary limit at low powers was achieved by imposing additional pressure drops on the vapor line through the use of a metering valve. A differential pressure transducer was also used to measure the pressure drop across the evaporator and the compensation chamber (CC). Test results show that when the capillary limit is exceeded, vapor will penetrate the primary wick, resulting in a partial dry-out of the evaporator and a rapid increase of the CC temperature. Because the evaporator can tolerate vapor bubbles, the LHP will continue to function and may reach a new steady state at the higher temperature. Thus, the LHP will exhibit a graceful degradation in performance rather than a complete failure. Moreover, the loop can recover from a partial dry-out by reducing the heat load without a re-start.
Document ID
20020014292
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ottenstein, Laura
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Rogers, Paul
(Army Tank-Automotive Research and Development Command Warren, MI United States)
Cheung, Kwok
(Naval Research Lab. Washington, DC United States)
Obenschain, Arthur F.
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 12th International Heat Transfer Conference
Location: Grenoble
Country: France
Start Date: August 18, 2002
End Date: August 23, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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