CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT
A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fu...
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creator | EPSTEIN, MICHAEL, JAY BALADI, MEHDI, MILANI BUCHHOLZ, TODD, JAMES KAMATH, DEEPAK, MANOHAR |
description | A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine. |
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fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2015</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151104&DB=EPODOC&CC=EP&NR=2938850A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151104&DB=EPODOC&CC=EP&NR=2938850A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>EPSTEIN, MICHAEL, JAY</creatorcontrib><creatorcontrib>BALADI, MEHDI, MILANI</creatorcontrib><creatorcontrib>BUCHHOLZ, TODD, JAMES</creatorcontrib><creatorcontrib>KAMATH, DEEPAK, MANOHAR</creatorcontrib><title>CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT</title><description>A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHB2Dor0d3f183RWcAt19VEIjgwOcfVVcPRzUfB1DfHwd1Fw8w9ScHH18QxzDfL0c4eo8vQDqlBw9AxyDnJ0C-FhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAUaWxhYWpgaOhsZEKAEAuB4qzg</recordid><startdate>20151104</startdate><enddate>20151104</enddate><creator>EPSTEIN, MICHAEL, JAY</creator><creator>BALADI, MEHDI, MILANI</creator><creator>BUCHHOLZ, TODD, JAMES</creator><creator>KAMATH, DEEPAK, MANOHAR</creator><scope>EVB</scope></search><sort><creationdate>20151104</creationdate><title>CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT</title><author>EPSTEIN, MICHAEL, JAY ; BALADI, MEHDI, MILANI ; BUCHHOLZ, TODD, JAMES ; KAMATH, DEEPAK, MANOHAR</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2938850A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>EPSTEIN, MICHAEL, JAY</creatorcontrib><creatorcontrib>BALADI, MEHDI, MILANI</creatorcontrib><creatorcontrib>BUCHHOLZ, TODD, JAMES</creatorcontrib><creatorcontrib>KAMATH, DEEPAK, MANOHAR</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>EPSTEIN, MICHAEL, JAY</au><au>BALADI, MEHDI, MILANI</au><au>BUCHHOLZ, TODD, JAMES</au><au>KAMATH, DEEPAK, MANOHAR</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT</title><date>2015-11-04</date><risdate>2015</risdate><abstract>A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT |
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