LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT
The present disclosure relates to the lubrication of a planet-carrier for a mechanical reduction gear of a turbine engine, for example of an aircraft. The planet-carrier includes a cage defining an internal housing configured to receive a central sun gear with an axis of rotation X, and an annular r...
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| creator | Di Giovanni, Jean-Charles Michel Pierre Robinet, Guillaume Jean Pierre Charrier, Mathieu Jean Lefebvre, Simon Loïc Clément Simon, Adrien Louis |
| description | The present disclosure relates to the lubrication of a planet-carrier for a mechanical reduction gear of a turbine engine, for example of an aircraft. The planet-carrier includes a cage defining an internal housing configured to receive a central sun gear with an axis of rotation X, and an annular row of planet gears arranged around the sun gear. The cage includes two annular walls that are radial with respect to the axis X, and connected to one another at their outer periphery by a cylindrical wall. At least one of the radial walls has orifices for mounting the planet gears, and the cylindrical wall has through-holes for the passage of the gearings of the planet gears so that they may engage with a gearing of the ring gear, which is configured to extend around the planet gears and the cage. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2020263784A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2020263784A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2020263784A13</originalsourceid><addsrcrecordid>eNqNy8EKwjAQBNBcPIj6DwteLagV9bqNm3YhpmVNzqVIPIlW6v9j0H6AzGFgeDNVLxsKYY2eawe1AYTGoiOfaRRhEjC1pPFMukKXnAWhU9BfXhLK7-ODFOwIyJWpVsAOGhTPOtiROEAWLWj8XE1u3X2Ii7FnamnI6yqL_bONQ99d4yO-23DZrlP2-eG4w03-n_oAXAM4Aw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT</title><source>esp@cenet</source><creator>Di Giovanni, Jean-Charles Michel Pierre ; Robinet, Guillaume Jean Pierre ; Charrier, Mathieu Jean ; Lefebvre, Simon Loïc Clément ; Simon, Adrien Louis</creator><creatorcontrib>Di Giovanni, Jean-Charles Michel Pierre ; Robinet, Guillaume Jean Pierre ; Charrier, Mathieu Jean ; Lefebvre, Simon Loïc Clément ; Simon, Adrien Louis</creatorcontrib><description>The present disclosure relates to the lubrication of a planet-carrier for a mechanical reduction gear of a turbine engine, for example of an aircraft. The planet-carrier includes a cage defining an internal housing configured to receive a central sun gear with an axis of rotation X, and an annular row of planet gears arranged around the sun gear. The cage includes two annular walls that are radial with respect to the axis X, and connected to one another at their outer periphery by a cylindrical wall. At least one of the radial walls has orifices for mounting the planet gears, and the cylindrical wall has through-holes for the passage of the gearings of the planet gears so that they may engage with a gearing of the ring gear, which is configured to extend around the planet gears and the cage.</description><language>eng</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GAS-TURBINE PLANTS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; 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 ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2020</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=20200820&DB=EPODOC&CC=US&NR=2020263784A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200820&DB=EPODOC&CC=US&NR=2020263784A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Di Giovanni, Jean-Charles Michel Pierre</creatorcontrib><creatorcontrib>Robinet, Guillaume Jean Pierre</creatorcontrib><creatorcontrib>Charrier, Mathieu Jean</creatorcontrib><creatorcontrib>Lefebvre, Simon Loïc Clément</creatorcontrib><creatorcontrib>Simon, Adrien Louis</creatorcontrib><title>LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT</title><description>The present disclosure relates to the lubrication of a planet-carrier for a mechanical reduction gear of a turbine engine, for example of an aircraft. The planet-carrier includes a cage defining an internal housing configured to receive a central sun gear with an axis of rotation X, and an annular row of planet gears arranged around the sun gear. The cage includes two annular walls that are radial with respect to the axis X, and connected to one another at their outer periphery by a cylindrical wall. At least one of the radial walls has orifices for mounting the planet gears, and the cylindrical wall has through-holes for the passage of the gearings of the planet gears so that they may engage with a gearing of the ring gear, which is configured to extend around the planet gears and the cage.</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>ENGINEERING ELEMENTS AND UNITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GEARING</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>STEAM ENGINES</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNy8EKwjAQBNBcPIj6DwteLagV9bqNm3YhpmVNzqVIPIlW6v9j0H6AzGFgeDNVLxsKYY2eawe1AYTGoiOfaRRhEjC1pPFMukKXnAWhU9BfXhLK7-ODFOwIyJWpVsAOGhTPOtiROEAWLWj8XE1u3X2Ii7FnamnI6yqL_bONQ99d4yO-23DZrlP2-eG4w03-n_oAXAM4Aw</recordid><startdate>20200820</startdate><enddate>20200820</enddate><creator>Di Giovanni, Jean-Charles Michel Pierre</creator><creator>Robinet, Guillaume Jean Pierre</creator><creator>Charrier, Mathieu Jean</creator><creator>Lefebvre, Simon Loïc Clément</creator><creator>Simon, Adrien Louis</creator><scope>EVB</scope></search><sort><creationdate>20200820</creationdate><title>LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT</title><author>Di Giovanni, Jean-Charles Michel Pierre ; Robinet, Guillaume Jean Pierre ; Charrier, Mathieu Jean ; Lefebvre, Simon Loïc Clément ; Simon, Adrien Louis</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2020263784A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2020</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>ENGINEERING ELEMENTS AND UNITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GEARING</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Di Giovanni, Jean-Charles Michel Pierre</creatorcontrib><creatorcontrib>Robinet, Guillaume Jean Pierre</creatorcontrib><creatorcontrib>Charrier, Mathieu Jean</creatorcontrib><creatorcontrib>Lefebvre, Simon Loïc Clément</creatorcontrib><creatorcontrib>Simon, Adrien Louis</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Di Giovanni, Jean-Charles Michel Pierre</au><au>Robinet, Guillaume Jean Pierre</au><au>Charrier, Mathieu Jean</au><au>Lefebvre, Simon Loïc Clément</au><au>Simon, Adrien Louis</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT</title><date>2020-08-20</date><risdate>2020</risdate><abstract>The present disclosure relates to the lubrication of a planet-carrier for a mechanical reduction gear of a turbine engine, for example of an aircraft. The planet-carrier includes a cage defining an internal housing configured to receive a central sun gear with an axis of rotation X, and an annular row of planet gears arranged around the sun gear. The cage includes two annular walls that are radial with respect to the axis X, and connected to one another at their outer periphery by a cylindrical wall. At least one of the radial walls has orifices for mounting the planet gears, and the cylindrical wall has through-holes for the passage of the gearings of the planet gears so that they may engage with a gearing of the ring gear, which is configured to extend around the planet gears and the cage.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GAS-TURBINE PLANTS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS 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 STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS |
| title | LUBRICATION OF A PLANET-CARRIER FOR A MECHANICAL REDUCTION GEAR OF A TURBINE ENGINE, IN PARTICULAR OF AN AIRCRAFT |
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