SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA
The fuel flow for a turboprop or turboshaft engine is provided by a plurality of parallel circuits each of which supplies a portion of the fuel to the engine with different valves controlling the flow through each of the separate circuits. In the turboprop engine there is imposed on the parallel flo...
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creator | HERBERT WILLIAM TUTHERLY CHARLES FREDERICK STEARNS |
description | The fuel flow for a turboprop or turboshaft engine is provided by a plurality of parallel circuits each of which supplies a portion of the fuel to the engine with different valves controlling the flow through each of the separate circuits. In the turboprop engine there is imposed on the parallel flow circuits a sensing device that determines the pressures in certain of the circuits and selects the appropriate pressure for signalling a pressure regulating valve whereby to vary the pressure drop through the fuel control. |
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In the turboprop engine there is imposed on the parallel flow circuits a sensing device that determines the pressures in certain of the circuits and selects the appropriate pressure for signalling a pressure regulating valve whereby to vary the pressure drop through the fuel control.</description><edition>4</edition><language>ita</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>1986</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=19860917&DB=EPODOC&CC=IT&NR=1138660B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19860917&DB=EPODOC&CC=IT&NR=1138660B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HERBERT WILLIAM TUTHERLY</creatorcontrib><creatorcontrib>CHARLES FREDERICK STEARNS</creatorcontrib><title>SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA</title><description>The fuel flow for a turboprop or turboshaft engine is provided by a plurality of parallel circuits each of which supplies a portion of the fuel to the engine with different valves controlling the flow through each of the separate circuits. In the turboprop engine there is imposed on the parallel flow circuits a sensing device that determines the pressures in certain of the circuits and selects the appropriate pressure for signalling a pressure regulating valve whereby to vary the pressure drop through the fuel control.</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>1986</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqFis0KwjAQBnvxIOozuC8gWArFa7JN8YP8SLK5WorEk2ihvj9W8O5pBmbW1TUhiXGKOhAjcobg673NKQW6mEgcvMRgLQhdDM4wKw9eLmOX5nROAg1rCJ5ckBBBiiRHDa-21eo-Puay-3FT7XsjfD6U6TWUeRpv5VneA6Sum1PbHnXz__gAQ20x-g</recordid><startdate>19860917</startdate><enddate>19860917</enddate><creator>HERBERT WILLIAM TUTHERLY</creator><creator>CHARLES FREDERICK STEARNS</creator><scope>EVB</scope></search><sort><creationdate>19860917</creationdate><title>SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA</title><author>HERBERT WILLIAM TUTHERLY ; CHARLES FREDERICK STEARNS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_IT1138660B3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ita</language><creationdate>1986</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>HERBERT WILLIAM TUTHERLY</creatorcontrib><creatorcontrib>CHARLES FREDERICK STEARNS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HERBERT WILLIAM TUTHERLY</au><au>CHARLES FREDERICK STEARNS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA</title><date>1986-09-17</date><risdate>1986</risdate><abstract>The fuel flow for a turboprop or turboshaft engine is provided by a plurality of parallel circuits each of which supplies a portion of the fuel to the engine with different valves controlling the flow through each of the separate circuits. In the turboprop engine there is imposed on the parallel flow circuits a sensing device that determines the pressures in certain of the circuits and selects the appropriate pressure for signalling a pressure regulating valve whereby to vary the pressure drop through the fuel control.</abstract><edition>4</edition><oa>free_for_read</oa></addata></record> |
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language | ita |
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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 | SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA |
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