HYBRID SPINNER SUPPORT

A hybrid support ring for a splitter of an aircraft engine comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially a...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: BISHOP, MICHAEL, JASON, ROBY, BENJAMIN, JAMES
Format: Patent
Sprache:eng ; fre
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 BISHOP, MICHAEL, JASON
ROBY, BENJAMIN, JAMES
description A hybrid support ring for a splitter of an aircraft engine comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially and disposed in the lug, the belt being formed of a second material. L'invention concerne une bague de support hybride destinée à un séparateur de sortie d'un moteur d'aéronef qui comprend un élément de suspension et une courroie, l'élément de suspension défini par une bride et un montant s'étendant vers l'arrière et ayant un tenon, l'élément de suspension s'étendant également de façon circonférentielle, l'élément de suspension formé d'un premier matériau, la courroie s'étendant de façon circonférentielle et disposée dans le tenon, la courroie étant formée d'un second matériau.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2014123685A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2014123685A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2014123685A13</originalsourceid><addsrcrecordid>eNrjZBDziHQK8nRRCA7w9PNzDVIIDg0I8A8K4WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8eH-RgaGJoZGxmYWpo6GxsSpAgBHjCBL</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>HYBRID SPINNER SUPPORT</title><source>esp@cenet</source><creator>BISHOP, MICHAEL, JASON ; ROBY, BENJAMIN, JAMES</creator><creatorcontrib>BISHOP, MICHAEL, JASON ; ROBY, BENJAMIN, JAMES</creatorcontrib><description>A hybrid support ring for a splitter of an aircraft engine comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially and disposed in the lug, the belt being formed of a second material. L'invention concerne une bague de support hybride destinée à un séparateur de sortie d'un moteur d'aéronef qui comprend un élément de suspension et une courroie, l'élément de suspension défini par une bride et un montant s'étendant vers l'arrière et ayant un tenon, l'élément de suspension s'étendant également de façon circonférentielle, l'élément de suspension formé d'un premier matériau, la courroie s'étendant de façon circonférentielle et disposée dans le tenon, la courroie étant formée d'un second matériau.</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2014</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=20140814&amp;DB=EPODOC&amp;CC=WO&amp;NR=2014123685A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20140814&amp;DB=EPODOC&amp;CC=WO&amp;NR=2014123685A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BISHOP, MICHAEL, JASON</creatorcontrib><creatorcontrib>ROBY, BENJAMIN, JAMES</creatorcontrib><title>HYBRID SPINNER SUPPORT</title><description>A hybrid support ring for a splitter of an aircraft engine comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially and disposed in the lug, the belt being formed of a second material. L'invention concerne une bague de support hybride destinée à un séparateur de sortie d'un moteur d'aéronef qui comprend un élément de suspension et une courroie, l'élément de suspension défini par une bride et un montant s'étendant vers l'arrière et ayant un tenon, l'élément de suspension s'étendant également de façon circonférentielle, l'élément de suspension formé d'un premier matériau, la courroie s'étendant de façon circonférentielle et disposée dans le tenon, la courroie étant formée d'un second matériau.</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>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBDziHQK8nRRCA7w9PNzDVIIDg0I8A8K4WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8eH-RgaGJoZGxmYWpo6GxsSpAgBHjCBL</recordid><startdate>20140814</startdate><enddate>20140814</enddate><creator>BISHOP, MICHAEL, JASON</creator><creator>ROBY, BENJAMIN, JAMES</creator><scope>EVB</scope></search><sort><creationdate>20140814</creationdate><title>HYBRID SPINNER SUPPORT</title><author>BISHOP, MICHAEL, JASON ; ROBY, BENJAMIN, JAMES</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2014123685A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2014</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>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>BISHOP, MICHAEL, JASON</creatorcontrib><creatorcontrib>ROBY, BENJAMIN, JAMES</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BISHOP, MICHAEL, JASON</au><au>ROBY, BENJAMIN, JAMES</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>HYBRID SPINNER SUPPORT</title><date>2014-08-14</date><risdate>2014</risdate><abstract>A hybrid support ring for a splitter of an aircraft engine comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially and disposed in the lug, the belt being formed of a second material. L'invention concerne une bague de support hybride destinée à un séparateur de sortie d'un moteur d'aéronef qui comprend un élément de suspension et une courroie, l'élément de suspension défini par une bride et un montant s'étendant vers l'arrière et ayant un tenon, l'élément de suspension s'étendant également de façon circonférentielle, l'élément de suspension formé d'un premier matériau, la courroie s'étendant de façon circonférentielle et disposée dans le tenon, la courroie étant formée d'un second matériau.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre
recordid cdi_epo_espacenet_WO2014123685A1
source esp@cenet
subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
WEAPONS
title HYBRID SPINNER SUPPORT
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T00%3A06%3A20IST&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=BISHOP,%20MICHAEL,%20JASON&rft.date=2014-08-14&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2014123685A1%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