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High gradient directional solidification furnaceA high gradient directional solidification furnace is disclosed which includes eight thermal zones throughout the length of the furnace. In the hot end of the furnace, furnace elements provide desired temperatures. These elements include Nichrome wire received in a grooved tube which is encapsulated y an outer alumina core. A booster heater is provided in the hot end of the furnace which includes toroidal tungsten/rhenium wire which has a capacity to put heat quickly into the furnace. An adiabatic zone is provided by an insulation barrier to separate the hot end of the furnace from the cold end. The old end of the furnace is defined by additional heating elements. A heat transfer plate provides a means by which heat may be extracted from the furnace and conducted away through liquid cooled jackets. By varying the input of heat via the booster heater and output of heat via the heat transfer plate, a desired thermal gradient profile may be provided.
Document ID
19860011279
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Aldrich, B. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Whitt, W. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Subject Category
Instrumentation And Photography
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-571614
Patent Number: US-PATENT-4,544,025
Patent Number: NASA-CASE-MFS-25963-1
Accession Number
86N20750
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,544,025|NASA-CASE-MFS-25963-1
Patent Application
US-PATENT-APPL-SN-571614
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