Assembly for a turbine engine
An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second z...
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creator | Benoit Andre Pierre Frossard Remi Philippe Guy Onfray Clement Miraton |
description | An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second zone 26b where the tubular component bulges 28 and does not make contact with the pivot, defining an annular space 30 there between. The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. The assembly is for a turbine engine, it may form part of a turbine engine compressor and may be used in a turbojet or turbo prop engine. |
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The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. The assembly is for a turbine engine, it may form part of a turbine engine compressor and may be used in a turbojet or turbo prop engine.</description><language>eng</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 ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; 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=20191127&DB=EPODOC&CC=GB&NR=2574107A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191127&DB=EPODOC&CC=GB&NR=2574107A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Benoit Andre Pierre Frossard</creatorcontrib><creatorcontrib>Remi Philippe Guy Onfray</creatorcontrib><creatorcontrib>Clement Miraton</creatorcontrib><title>Assembly for a turbine engine</title><description>An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second zone 26b where the tubular component bulges 28 and does not make contact with the pivot, defining an annular space 30 there between. The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. The assembly is for a turbine engine, it may form part of a turbine engine compressor and may be used in a turbojet or turbo prop engine.</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>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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB1LC5OzU3KqVRIyy9SSFQoKS1KysxLVUjNSwdSPAysaYk5xam8UJqbQd7NNcTZQze1ID8-tbggMTk1L7Uk3t3JyNTcxNDA3NGYsAoAJu0i-w</recordid><startdate>20191127</startdate><enddate>20191127</enddate><creator>Benoit Andre Pierre Frossard</creator><creator>Remi Philippe Guy Onfray</creator><creator>Clement Miraton</creator><scope>EVB</scope></search><sort><creationdate>20191127</creationdate><title>Assembly for a turbine engine</title><author>Benoit Andre Pierre Frossard ; Remi Philippe Guy Onfray ; Clement Miraton</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2574107A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</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>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>Benoit Andre Pierre Frossard</creatorcontrib><creatorcontrib>Remi Philippe Guy Onfray</creatorcontrib><creatorcontrib>Clement Miraton</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Benoit Andre Pierre Frossard</au><au>Remi Philippe Guy Onfray</au><au>Clement Miraton</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Assembly for a turbine engine</title><date>2019-11-27</date><risdate>2019</risdate><abstract>An assembly 50 includes an annular row of stator blades including vanes 6 extending radially which are variable in pitch, with a tubular component mounted around a radially extending pivot 14, the tubular component 26 having at least a first zone 26a, 26c fitted tightly to the pivot, with a second zone 26b where the tubular component bulges 28 and does not make contact with the pivot, defining an annular space 30 there between. The bulge of the tubular component may be convex. There may be two tightly fitted zones, which may be at either end of the tubular component. The assembly is for a turbine engine, it may form part of a turbine engine compressor and may be used in a turbojet or turbo prop engine.</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 NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS |
title | Assembly for a turbine engine |
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