REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE
A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring g...
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creator | Mouton, Clémentine Charlotte Marie Lao, Jérémy Phorla Patsouris, Emmanuel Pierre Dimitri Nguyen Van, Thomas Julien Belmonte, Olivier |
description | A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring gear and the planetary shaft; and a planet carrier including members for supporting bearings of the planet gears, having axes of rotation B, which are evenly distributed around the axis A, as well as a part holding each supporting member substantially by the middle thereof along the axis B thereof, wherein said supporting members are made as a single part having means for supplying lubricating oil to said bearings. A method for assembling said reduction gear is also provided. |
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A method for assembling said reduction gear is also provided.</description><language>eng</language><subject>BLASTING ; ENGINEERING ELEMENTS AND UNITS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2018</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=20180614&DB=EPODOC&CC=US&NR=2018163850A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180614&DB=EPODOC&CC=US&NR=2018163850A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Mouton, Clémentine Charlotte Marie</creatorcontrib><creatorcontrib>Lao, Jérémy Phorla</creatorcontrib><creatorcontrib>Patsouris, Emmanuel Pierre Dimitri</creatorcontrib><creatorcontrib>Nguyen Van, Thomas Julien</creatorcontrib><creatorcontrib>Belmonte, Olivier</creatorcontrib><title>REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE</title><description>A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring gear and the planetary shaft; and a planet carrier including members for supporting bearings of the planet gears, having axes of rotation B, which are evenly distributed around the axis A, as well as a part holding each supporting member substantially by the middle thereof along the axis B thereof, wherein said supporting members are made as a single part having means for supplying lubricating oil to said bearings. A method for assembling said reduction gear is also provided.</description><subject>BLASTING</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GEARING</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAKcnUJdQ7x9PdTcHd1DFLwcAzz9HNXcPRTcA3wdI509vF0hkiEBDl6-im4-QcpOCqEhAY5efq5Krj6uQMpHgbWtMSc4lReKM3NoOzmGuLsoZtakB-fWlyQmJyal1oSHxpsZGBoYWhmbGFq4GhoTJwqAHBkK6I</recordid><startdate>20180614</startdate><enddate>20180614</enddate><creator>Mouton, Clémentine Charlotte Marie</creator><creator>Lao, Jérémy Phorla</creator><creator>Patsouris, Emmanuel Pierre Dimitri</creator><creator>Nguyen Van, Thomas Julien</creator><creator>Belmonte, Olivier</creator><scope>EVB</scope></search><sort><creationdate>20180614</creationdate><title>REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE</title><author>Mouton, Clémentine Charlotte Marie ; Lao, Jérémy Phorla ; Patsouris, Emmanuel Pierre Dimitri ; Nguyen Van, Thomas Julien ; Belmonte, Olivier</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2018163850A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</creationdate><topic>BLASTING</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GEARING</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Mouton, Clémentine Charlotte Marie</creatorcontrib><creatorcontrib>Lao, Jérémy Phorla</creatorcontrib><creatorcontrib>Patsouris, Emmanuel Pierre Dimitri</creatorcontrib><creatorcontrib>Nguyen Van, Thomas Julien</creatorcontrib><creatorcontrib>Belmonte, Olivier</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Mouton, Clémentine Charlotte Marie</au><au>Lao, Jérémy Phorla</au><au>Patsouris, Emmanuel Pierre Dimitri</au><au>Nguyen Van, Thomas Julien</au><au>Belmonte, Olivier</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE</title><date>2018-06-14</date><risdate>2018</risdate><abstract>A reduction gear having an epicyclic gear train for a turbine engine, in particular of an aircraft, comprising: a planetary shaft having an axis of rotation A; a ring gear having an axis A extending around said planetary shaft; planet gears distributed around said axis A, which mesh with said ring gear and the planetary shaft; and a planet carrier including members for supporting bearings of the planet gears, having axes of rotation B, which are evenly distributed around the axis A, as well as a part holding each supporting member substantially by the middle thereof along the axis B thereof, wherein said supporting members are made as a single part having means for supplying lubricating oil to said bearings. A method for assembling said reduction gear is also provided.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING ENGINEERING ELEMENTS AND UNITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING THERMAL INSULATION IN GENERAL WEAPONS |
title | REDUCTION GEAR HAVING AN EPICYCLIC GEAR TRAIN FOR A TURBINE ENGINE |
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