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...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: HERBERT WILLIAM TUTHERLY, CHARLES FREDERICK STEARNS
Format: Patent
Sprache:ita
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page
container_title
container_volume
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.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_IT1138660B</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>IT1138660B</sourcerecordid><originalsourceid>FETCH-epo_espacenet_IT1138660B3</originalsourceid><addsrcrecordid>eNqFis0KwjAQBnvxIOozuC8gWArFa7JN8YP8SLK5WorEk2ihvj9W8O5pBmbW1TUhiXGKOhAjcobg673NKQW6mEgcvMRgLQhdDM4wKw9eLmOX5nROAg1rCJ5ckBBBiiRHDa-21eo-Puay-3FT7XsjfD6U6TWUeRpv5VneA6Sum1PbHnXz__gAQ20x-g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SISTEMA DI CIRCUITI DI FLUSSO PER CONTROLLI IDROMECCANICI DEL COMBUSTIBILE IN MOTORI A TURBINA</title><source>esp@cenet</source><creator>HERBERT WILLIAM TUTHERLY ; CHARLES FREDERICK STEARNS</creator><creatorcontrib>HERBERT WILLIAM TUTHERLY ; CHARLES FREDERICK STEARNS</creatorcontrib><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><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&amp;date=19860917&amp;DB=EPODOC&amp;CC=IT&amp;NR=1138660B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19860917&amp;DB=EPODOC&amp;CC=IT&amp;NR=1138660B$$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>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language ita
recordid cdi_epo_espacenet_IT1138660B
source esp@cenet
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
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T04%3A08%3A59IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=HERBERT%20WILLIAM%20TUTHERLY&rft.date=1986-09-17&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EIT1138660B%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true