TURBINE AIRFOIL WITH PASSIVE MORPHING STRUCTURE

A turbine engine airfoil apparatus, including an airfoil defined by a plurality of airfoil sections arrayed along a stacking axis that extends between a root and a tip, wherein at least two of the airfoil sections spaced apart from each other have differing airfoil section thermal expansion properti...

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Hauptverfasser:	KRAY, NICHOLAS JOSEPH, JOSHI, NARENDRA DIGAMBER, MARSLAND, PAUL GERARD, KALITA, SAMAR JYOTI, SPENCE, WAYNE ALLEN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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creator	KRAY, NICHOLAS JOSEPH JOSHI, NARENDRA DIGAMBER MARSLAND, PAUL GERARD KALITA, SAMAR JYOTI SPENCE, WAYNE ALLEN
description	A turbine engine airfoil apparatus, including an airfoil defined by a plurality of airfoil sections arrayed along a stacking axis that extends between a root and a tip, wherein at least two of the airfoil sections spaced apart from each other have differing airfoil section thermal expansion properties. La présente invention concerne un appareil daubage de moteur à turbine, y compris un profil de voilure défini par une pluralité de sections de profil placées sur un axe de montage qui sétend entre une racine et une pointe dans laquelle au moins deux des sections de profil espacées les unes des autres ont différentes propriétés de dilatation thermique de la section de profil.
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La présente invention concerne un appareil daubage de moteur à turbine, y compris un profil de voilure défini par une pluralité de sections de profil placées sur un axe de montage qui sétend entre une racine et une pointe dans laquelle au moins deux des sections de profil espacées les unes des autres ont différentes propriétés de dilatation thermique de la section de profil.</description><language>eng ; fre</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2019</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=20191210&DB=EPODOC&CC=CA&NR=2948252C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191210&DB=EPODOC&CC=CA&NR=2948252C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRAY, NICHOLAS JOSEPH</creatorcontrib><creatorcontrib>JOSHI, NARENDRA DIGAMBER</creatorcontrib><creatorcontrib>MARSLAND, PAUL GERARD</creatorcontrib><creatorcontrib>KALITA, SAMAR JYOTI</creatorcontrib><creatorcontrib>SPENCE, WAYNE ALLEN</creatorcontrib><title>TURBINE AIRFOIL WITH PASSIVE MORPHING STRUCTURE</title><description>A turbine engine airfoil apparatus, including an airfoil defined by a plurality of airfoil sections arrayed along a stacking axis that extends between a root and a tip, wherein at least two of the airfoil sections spaced apart from each other have differing airfoil section thermal expansion properties. La présente invention concerne un appareil daubage de moteur à turbine, y compris un profil de voilure défini par une pluralité de sections de profil placées sur un axe de montage qui sétend entre une racine et une pointe dans laquelle au moins deux des sections de profil espacées les unes des autres ont différentes propriétés de dilatation thermique de la section de profil.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAPCQ1y8vRzVXD0DHLz9_RRCPcM8VAIcAwO9gxzVfD1Dwrw8PRzVwgOCQp1Bip15WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c6ORpYmFkamRs7GhFUAAJsjJYc</recordid><startdate>20191210</startdate><enddate>20191210</enddate><creator>KRAY, NICHOLAS JOSEPH</creator><creator>JOSHI, NARENDRA DIGAMBER</creator><creator>MARSLAND, PAUL GERARD</creator><creator>KALITA, SAMAR JYOTI</creator><creator>SPENCE, WAYNE ALLEN</creator><scope>EVB</scope></search><sort><creationdate>20191210</creationdate><title>TURBINE AIRFOIL WITH PASSIVE MORPHING STRUCTURE</title><author>KRAY, NICHOLAS JOSEPH ; JOSHI, NARENDRA DIGAMBER ; MARSLAND, PAUL GERARD ; KALITA, SAMAR JYOTI ; SPENCE, WAYNE ALLEN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2948252C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2019</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRAY, NICHOLAS JOSEPH</creatorcontrib><creatorcontrib>JOSHI, NARENDRA DIGAMBER</creatorcontrib><creatorcontrib>MARSLAND, PAUL GERARD</creatorcontrib><creatorcontrib>KALITA, SAMAR JYOTI</creatorcontrib><creatorcontrib>SPENCE, WAYNE ALLEN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRAY, NICHOLAS JOSEPH</au><au>JOSHI, NARENDRA DIGAMBER</au><au>MARSLAND, PAUL GERARD</au><au>KALITA, SAMAR JYOTI</au><au>SPENCE, WAYNE ALLEN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE AIRFOIL WITH PASSIVE MORPHING STRUCTURE</title><date>2019-12-10</date><risdate>2019</risdate><abstract>A turbine engine airfoil apparatus, including an airfoil defined by a plurality of airfoil sections arrayed along a stacking axis that extends between a root and a tip, wherein at least two of the airfoil sections spaced apart from each other have differing airfoil section thermal expansion properties. La présente invention concerne un appareil daubage de moteur à turbine, y compris un profil de voilure défini par une pluralité de sections de profil placées sur un axe de montage qui sétend entre une racine et une pointe dans laquelle au moins deux des sections de profil espacées les unes des autres ont différentes propriétés de dilatation thermique de la section de profil.</abstract><oa>free_for_read</oa></addata></record>
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subjects	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
title	TURBINE AIRFOIL WITH PASSIVE MORPHING STRUCTURE
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