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Heat exchangerA heat exchanger, as exemplified by a rocket combustion chamber, is constructed by stacking thin metal rings having microsized openings therein at selective locations to form cooling passages defined by an inner wall, an outer wall and fins. Suitable manifolds are provided at each end of the rocket chamber. In addition to the cooling channel openings, coolant feed openings may be formed in each of rings. The coolant feed openings may be nested or positioned within generally U-shaped cooling channel openings. Compression on the stacked rings may be maintained by welds or the like or by bolts extending through the stacked rings.
Document ID
19790005117
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Sokolowski, D. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 22, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
Patent Number: NASA-CASE-LEW-12252-1
Patent Number: US-PATENT-4,107,919
Patent Application Number: US-PATENT-APPL-SN-559847
Accession Number
79N13288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12252-1|US-PATENT-4,107,919
Patent Application
US-PATENT-APPL-SN-559847
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