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Monogroove heat pipe design: Insulated liquid channel with bridging wickA screen mesh artery supported concentrically within the evaporator section of a heat pipe liquid channel retains liquid in the channel. Continued and uniform liquid feed to the heat pipe evaporation section (20) during periods of excessive heat transfer is assured. The overall design provides high evaporation and condensation film coefficients for the working fluid by means of the circumferential grooves in the walls of the vapor channel, while not interfering with the overall heat transport capability of the axial groove. The design has particular utility in zero-g environments.
Document ID
19850020868
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Alario, J. P.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Brown, R. F.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Kosson, R. L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 12, 2013
Publication Date
May 7, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
Patent Number: US-PATENT-4,515,207
Patent Application Number: US-PATENT-APPL-SN-615505
Patent Number: NASA-CASE-MSC-20497-1
Accession Number
85N29180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,515,207|NASA-CASE-MSC-20497-1
Patent Application
US-PATENT-APPL-SN-615505
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