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Fuel combustorA fuel combustor comprises a chamber with air and fuel inlets and a combination gas outlet. The fuel is supplied to a vaporization zone and fuel and air are mixed in a pair of mixing chambers, each exemplified by a swirl can. The resultant mixture is directed into a combustion zone within the combustor. Heat pipes are arranged with one end portion substantially in the combustion zone and the other end in the vaporization zone of its appropriate mixing chamber. Some of the heat of combustion is thus carried back upstream into the swirl cans, to vaporize the fuel as it enters the vaporization zone in the swirl can, thereby improving vaporization and fuel mixing.
Document ID
19780002281
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Marek, C. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 4, 1977
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
Patent Number: US-PATENT-4,052,144
Patent Number: NASA-CASE-LEW-12137-1
Patent Application Number: US-PATENT-APPL-SN-672210
Accession Number
78N10224
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,052,144|NASA-CASE-LEW-12137-1
Patent Application
US-PATENT-APPL-SN-672210
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