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Heat pipes to reduce engine exhaust emissionsA fuel combustor is presented that consists of an elongated casing with an air inlet conduit portion at one end, and having an opposite exit end. An elongated heat pipe is mounted longitudinally in the casing and is offset from and extends alongside the combustion space. The heat pipe is in heat transmitting relationship with the air intake conduit for heating incoming air. A guide conduit structure is provided for conveying the heated air from the intake conduit into the combustion space. A fuel discharge nozzle is provided to inject fuel into the combustion space. A fuel conduit from a fuel supply source has a portion engaged in heat transfer relationship of the heat pipe for preheating the fuel. The downstream end of the heat pipe is in heat transfer relationship with the casing and is located adjacent to the downstream end of the combustion space. The offset position of the heat pipe relative to the combustion space minimizes the quenching effect of the heat pipe on the gaseous products of combustion, as well as reducing coking of the fuel on the heat pipe, thereby improving the efficiency of the combustor.
Document ID
19840014890
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Schultz, D. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
February 7, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: NASA-CASE-LEW-12590-1
Patent Application Number: US-PATENT-APPL-SN-229693
Patent Number: US-PATENT-4,429,537
Accession Number
84N22958
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12590-1|US-PATENT-4,429,537
Patent Application
US-PATENT-APPL-SN-229693
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