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Stacked-Disk CombustorMaterials chosen for strength rather than thermal conductivity. Stacked washerlike disks accommodate built-in coolant passages while providing combustion zone of ideal shape. Fuel flows through coolant passages where preheated before entering combustion zone through passages in disks. Eight coolant passages in cross section, although number in particular application determined by required rate of flow of fuel and pressure drop. Combustion chamber operates for greater efficiency at pressures and temperatures higher than those of conventional tube-wall combustion chamber.
Document ID
19880000501
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Ingle, Walter B.
(Rockwell International Corp.)
Date Acquired
August 13, 2013
Publication Date
October 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 9
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-29333
ISSN: 0145-319X
Report Number: MFS-29333
Accession Number
88B10501
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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