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Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation
•An innovative fuel-cooled combustor is set-up.•The sensible and chemical heat sink absorbed by the decomposing fuel are determined.•The cooling system heat exchange efficiency is investigated.•Fuel coking activity is analyzed and quantified.•A coking monitoring method suitable for on-board applicat...
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Published in: | Fuel (Guildford) 2019-03, Vol.239, p.1091-1101 |
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creator | Taddeo, L. Gascoin, N. Chetehouna, K. Ingenito, A. Stella, F. Bouchez, M. Le Naour, B. |
description | •An innovative fuel-cooled combustor is set-up.•The sensible and chemical heat sink absorbed by the decomposing fuel are determined.•The cooling system heat exchange efficiency is investigated.•Fuel coking activity is analyzed and quantified.•A coking monitoring method suitable for on-board application is validated.
Scramjets engines are suitable to propel high-speed hypersonic vehicles. As flight velocities increase, vehicle thermal protection becomes very critical. In this sense, regenerative cooling is a well-known cooling technique, particularly effective when an endothermic hydrocarbon is used as fuel. The development of regeneratively cooled engines faces several challenges, the most important being the difficulty of defining an engine regulation strategy because of the dual function of the fuel (both propellant and coolant). In this context, a regeneratively cooled combustor allowing the experimental study of a fuel-cooled engine has been designed. Experiments are run using ethylene as fuel and air as oxidizer. Two command parameters, i.e. fuel mass flow rate and equivalence ratio (1.0–1.5), are investigated. It has been observed that fuel mass flow rate increases by 16–20% result in heat flux density (from the combustion gases to the combustor wall) increases between 20 and 28%, depending on equivalence ratio and pressure. The dependence of the cooling system heat exchange efficiency on the two operating parameters has been demonstrated. Ethylene coking activity has been investigated. For applied interest, a monitoring method for carbon deposits formation has been developed and validated. |
doi_str_mv | 10.1016/j.fuel.2018.11.096 |
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Scramjets engines are suitable to propel high-speed hypersonic vehicles. As flight velocities increase, vehicle thermal protection becomes very critical. In this sense, regenerative cooling is a well-known cooling technique, particularly effective when an endothermic hydrocarbon is used as fuel. The development of regeneratively cooled engines faces several challenges, the most important being the difficulty of defining an engine regulation strategy because of the dual function of the fuel (both propellant and coolant). In this context, a regeneratively cooled combustor allowing the experimental study of a fuel-cooled engine has been designed. Experiments are run using ethylene as fuel and air as oxidizer. Two command parameters, i.e. fuel mass flow rate and equivalence ratio (1.0–1.5), are investigated. It has been observed that fuel mass flow rate increases by 16–20% result in heat flux density (from the combustion gases to the combustor wall) increases between 20 and 28%, depending on equivalence ratio and pressure. The dependence of the cooling system heat exchange efficiency on the two operating parameters has been demonstrated. Ethylene coking activity has been investigated. For applied interest, a monitoring method for carbon deposits formation has been developed and validated.</description><identifier>ISSN: 0016-2361</identifier><identifier>EISSN: 1873-7153</identifier><identifier>DOI: 10.1016/j.fuel.2018.11.096</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>Coking ; Combustion ; Combustion chambers ; Combustion-pyrolysis coupling ; Cooling ; Cooling systems ; Engines ; Equivalence ratio ; Ethylene ; Flow rates ; Flux density ; Fuels ; Gases ; Heat exchange ; Heat flux ; Heat transfer ; Hydrocarbon pyrolysis ; Hydrocarbons coking activity ; Hypersonic vehicles ; Mass flow rate ; Parameters ; Pressure dependence ; Pyrolysis ; Regenerative cooling ; Supersonic combustion ramjet engines ; Thermal protection</subject><ispartof>Fuel (Guildford), 2019-03, Vol.239, p.1091-1101</ispartof><rights>2018</rights><rights>Copyright Elsevier BV Mar 1, 2019</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c365t-6d018c868893f2924af31e9a48d9841eaa3016ff126862e9f0b9e5e8bce2e4a43</citedby><cites>FETCH-LOGICAL-c365t-6d018c868893f2924af31e9a48d9841eaa3016ff126862e9f0b9e5e8bce2e4a43</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Taddeo, L.</creatorcontrib><creatorcontrib>Gascoin, N.</creatorcontrib><creatorcontrib>Chetehouna, K.</creatorcontrib><creatorcontrib>Ingenito, A.</creatorcontrib><creatorcontrib>Stella, F.</creatorcontrib><creatorcontrib>Bouchez, M.</creatorcontrib><creatorcontrib>Le Naour, B.</creatorcontrib><title>Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation</title><title>Fuel (Guildford)</title><description>•An innovative fuel-cooled combustor is set-up.•The sensible and chemical heat sink absorbed by the decomposing fuel are determined.•The cooling system heat exchange efficiency is investigated.•Fuel coking activity is analyzed and quantified.•A coking monitoring method suitable for on-board application is validated.
Scramjets engines are suitable to propel high-speed hypersonic vehicles. As flight velocities increase, vehicle thermal protection becomes very critical. In this sense, regenerative cooling is a well-known cooling technique, particularly effective when an endothermic hydrocarbon is used as fuel. The development of regeneratively cooled engines faces several challenges, the most important being the difficulty of defining an engine regulation strategy because of the dual function of the fuel (both propellant and coolant). In this context, a regeneratively cooled combustor allowing the experimental study of a fuel-cooled engine has been designed. Experiments are run using ethylene as fuel and air as oxidizer. Two command parameters, i.e. fuel mass flow rate and equivalence ratio (1.0–1.5), are investigated. It has been observed that fuel mass flow rate increases by 16–20% result in heat flux density (from the combustion gases to the combustor wall) increases between 20 and 28%, depending on equivalence ratio and pressure. The dependence of the cooling system heat exchange efficiency on the two operating parameters has been demonstrated. Ethylene coking activity has been investigated. For applied interest, a monitoring method for carbon deposits formation has been developed and validated.</description><subject>Coking</subject><subject>Combustion</subject><subject>Combustion chambers</subject><subject>Combustion-pyrolysis coupling</subject><subject>Cooling</subject><subject>Cooling systems</subject><subject>Engines</subject><subject>Equivalence ratio</subject><subject>Ethylene</subject><subject>Flow rates</subject><subject>Flux density</subject><subject>Fuels</subject><subject>Gases</subject><subject>Heat exchange</subject><subject>Heat flux</subject><subject>Heat transfer</subject><subject>Hydrocarbon pyrolysis</subject><subject>Hydrocarbons coking activity</subject><subject>Hypersonic vehicles</subject><subject>Mass flow rate</subject><subject>Parameters</subject><subject>Pressure dependence</subject><subject>Pyrolysis</subject><subject>Regenerative cooling</subject><subject>Supersonic combustion ramjet engines</subject><subject>Thermal protection</subject><issn>0016-2361</issn><issn>1873-7153</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNp9kEtv2zAQhImgAeI6-QM5EehZCpd6mCp6KYw8ChjIJTkTNLUM6MikSlJGlV8fCs65pz3szOzOR8gtsBIYtHeH0kw4lJyBKAFK1rUXZAViUxUbaKpvZMWyquBVC1fke4wHxthGNPWKfNz_GzHYI7qkBhrT1M_UGzrOwQ9ztLHQ_rifYrLeUe2ncbDujVpHFQ34hg6DSvaEw5yXfsCefsl9-EmfUCWagnLRYKDKLct3pMaHo1ryrsmlUUPEm6-5Jq8P9y_bp2L3_Phn-3tX6KptUtH2uZQWrRBdZXjHa2UqwE7Vou9EDahUlbsZA7wVLcfOsH2HDYq9Ro61qqs1-XHOHYP_O2FM8uCn4PJJyUHwetM1sKj4WaWDjzGgkWPGosIsgcmFsTzIhbFcGEsAmRln06-zCfP_J4tBRm3RaextQJ1k7-3_7J-a24gW</recordid><startdate>20190301</startdate><enddate>20190301</enddate><creator>Taddeo, L.</creator><creator>Gascoin, N.</creator><creator>Chetehouna, K.</creator><creator>Ingenito, A.</creator><creator>Stella, F.</creator><creator>Bouchez, M.</creator><creator>Le Naour, B.</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7QO</scope><scope>7QQ</scope><scope>7SC</scope><scope>7SE</scope><scope>7SP</scope><scope>7SR</scope><scope>7T7</scope><scope>7TA</scope><scope>7TB</scope><scope>7U5</scope><scope>8BQ</scope><scope>8FD</scope><scope>C1K</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope><scope>H8G</scope><scope>JG9</scope><scope>JQ2</scope><scope>KR7</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>P64</scope></search><sort><creationdate>20190301</creationdate><title>Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation</title><author>Taddeo, L. ; Gascoin, N. ; Chetehouna, K. ; Ingenito, A. ; Stella, F. ; Bouchez, M. ; Le Naour, B.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c365t-6d018c868893f2924af31e9a48d9841eaa3016ff126862e9f0b9e5e8bce2e4a43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Coking</topic><topic>Combustion</topic><topic>Combustion chambers</topic><topic>Combustion-pyrolysis coupling</topic><topic>Cooling</topic><topic>Cooling systems</topic><topic>Engines</topic><topic>Equivalence ratio</topic><topic>Ethylene</topic><topic>Flow rates</topic><topic>Flux density</topic><topic>Fuels</topic><topic>Gases</topic><topic>Heat exchange</topic><topic>Heat flux</topic><topic>Heat transfer</topic><topic>Hydrocarbon pyrolysis</topic><topic>Hydrocarbons coking activity</topic><topic>Hypersonic vehicles</topic><topic>Mass flow rate</topic><topic>Parameters</topic><topic>Pressure dependence</topic><topic>Pyrolysis</topic><topic>Regenerative cooling</topic><topic>Supersonic combustion ramjet engines</topic><topic>Thermal protection</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Taddeo, L.</creatorcontrib><creatorcontrib>Gascoin, N.</creatorcontrib><creatorcontrib>Chetehouna, K.</creatorcontrib><creatorcontrib>Ingenito, A.</creatorcontrib><creatorcontrib>Stella, F.</creatorcontrib><creatorcontrib>Bouchez, M.</creatorcontrib><creatorcontrib>Le Naour, B.</creatorcontrib><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Biotechnology Research Abstracts</collection><collection>Ceramic Abstracts</collection><collection>Computer and Information Systems Abstracts</collection><collection>Corrosion Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Industrial and Applied Microbiology Abstracts (Microbiology A)</collection><collection>Materials Business File</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Copper Technical Reference Library</collection><collection>Materials Research Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><collection>Biotechnology and BioEngineering Abstracts</collection><jtitle>Fuel (Guildford)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Taddeo, L.</au><au>Gascoin, N.</au><au>Chetehouna, K.</au><au>Ingenito, A.</au><au>Stella, F.</au><au>Bouchez, M.</au><au>Le Naour, B.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation</atitle><jtitle>Fuel (Guildford)</jtitle><date>2019-03-01</date><risdate>2019</risdate><volume>239</volume><spage>1091</spage><epage>1101</epage><pages>1091-1101</pages><issn>0016-2361</issn><eissn>1873-7153</eissn><abstract>•An innovative fuel-cooled combustor is set-up.•The sensible and chemical heat sink absorbed by the decomposing fuel are determined.•The cooling system heat exchange efficiency is investigated.•Fuel coking activity is analyzed and quantified.•A coking monitoring method suitable for on-board application is validated.
Scramjets engines are suitable to propel high-speed hypersonic vehicles. As flight velocities increase, vehicle thermal protection becomes very critical. In this sense, regenerative cooling is a well-known cooling technique, particularly effective when an endothermic hydrocarbon is used as fuel. The development of regeneratively cooled engines faces several challenges, the most important being the difficulty of defining an engine regulation strategy because of the dual function of the fuel (both propellant and coolant). In this context, a regeneratively cooled combustor allowing the experimental study of a fuel-cooled engine has been designed. Experiments are run using ethylene as fuel and air as oxidizer. Two command parameters, i.e. fuel mass flow rate and equivalence ratio (1.0–1.5), are investigated. It has been observed that fuel mass flow rate increases by 16–20% result in heat flux density (from the combustion gases to the combustor wall) increases between 20 and 28%, depending on equivalence ratio and pressure. The dependence of the cooling system heat exchange efficiency on the two operating parameters has been demonstrated. Ethylene coking activity has been investigated. For applied interest, a monitoring method for carbon deposits formation has been developed and validated.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.fuel.2018.11.096</doi><tpages>11</tpages></addata></record> |
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subjects | Coking Combustion Combustion chambers Combustion-pyrolysis coupling Cooling Cooling systems Engines Equivalence ratio Ethylene Flow rates Flux density Fuels Gases Heat exchange Heat flux Heat transfer Hydrocarbon pyrolysis Hydrocarbons coking activity Hypersonic vehicles Mass flow rate Parameters Pressure dependence Pyrolysis Regenerative cooling Supersonic combustion ramjet engines Thermal protection |
title | Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation |
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