LOAD SPLIT MECHANISM FOR GEAR TRANSMISSION
A method and apparatus for a transmission system selectively positioning sets of planet gear support bearings (50, 55, 80, 90) to achieve an optimized load distribution among a set of drive planet pinions (22) and a set of idler planet pinions (70) disposed in engagement between two reaction gears (...
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| creator | FORBES, RYAN WILMER, MATTHEW AI, XIAOLAN ORKIN, CURT KRUSE, RANDY, P CHIAVAROLI, NEIL SMITH, BRADLEY |
| description | A method and apparatus for a transmission system selectively positioning sets of planet gear support bearings (50, 55, 80, 90) to achieve an optimized load distribution among a set of drive planet pinions (22) and a set of idler planet pinions (70) disposed in engagement between two reaction gears (30, 40) in the transmission system (A, A1), for splitting an applied load between at least two pathways between an input and an output.
L'invention concerne un procédé et un appareil pour système de transmission, caractérisés par le positionnement sélectif de jeux de roulements (50, 55, 80, 90) de guidage de satellites pour réaliser une répartition optimisée de la charge entre un ensemble de satellites menants (22) et un ensemble de satellites menés (70) disposés en engrènement entre deux engrenages (30, 40) de réaction du système (A, A1) de transmission, afin de partager une charge appliquée entre au moins deux parcours reliant une entrée à une sortie. |
| format | Patent |
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L'invention concerne un procédé et un appareil pour système de transmission, caractérisés par le positionnement sélectif de jeux de roulements (50, 55, 80, 90) de guidage de satellites pour réaliser une répartition optimisée de la charge entre un ensemble de satellites menants (22) et un ensemble de satellites menés (70) disposés en engrènement entre deux engrenages (30, 40) de réaction du système (A, A1) de transmission, afin de partager une charge appliquée entre au moins deux parcours reliant une entrée à une sortie.</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2011</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=20111020&DB=EPODOC&CC=WO&NR=2011130352A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20111020&DB=EPODOC&CC=WO&NR=2011130352A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FORBES, RYAN</creatorcontrib><creatorcontrib>WILMER, MATTHEW</creatorcontrib><creatorcontrib>AI, XIAOLAN</creatorcontrib><creatorcontrib>ORKIN, CURT</creatorcontrib><creatorcontrib>KRUSE, RANDY, P</creatorcontrib><creatorcontrib>CHIAVAROLI, NEIL</creatorcontrib><creatorcontrib>SMITH, BRADLEY</creatorcontrib><title>LOAD SPLIT MECHANISM FOR GEAR TRANSMISSION</title><description>A method and apparatus for a transmission system selectively positioning sets of planet gear support bearings (50, 55, 80, 90) to achieve an optimized load distribution among a set of drive planet pinions (22) and a set of idler planet pinions (70) disposed in engagement between two reaction gears (30, 40) in the transmission system (A, A1), for splitting an applied load between at least two pathways between an input and an output.
L'invention concerne un procédé et un appareil pour système de transmission, caractérisés par le positionnement sélectif de jeux de roulements (50, 55, 80, 90) de guidage de satellites pour réaliser une répartition optimisée de la charge entre un ensemble de satellites menants (22) et un ensemble de satellites menés (70) disposés en engrènement entre deux engrenages (30, 40) de réaction du système (A, A1) de transmission, afin de partager une charge appliquée entre au moins deux parcours reliant une entrée à une sortie.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</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>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNDy8Xd0UQgO8PEMUfB1dfZw9PMM9lVw8w9ScHd1DFIICXL0C_b1DA729PfjYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx4f5GBoaGhsYGxqZGjobGxKkCANw3JXY</recordid><startdate>20111020</startdate><enddate>20111020</enddate><creator>FORBES, RYAN</creator><creator>WILMER, MATTHEW</creator><creator>AI, XIAOLAN</creator><creator>ORKIN, CURT</creator><creator>KRUSE, RANDY, P</creator><creator>CHIAVAROLI, NEIL</creator><creator>SMITH, BRADLEY</creator><scope>EVB</scope></search><sort><creationdate>20111020</creationdate><title>LOAD SPLIT MECHANISM FOR GEAR TRANSMISSION</title><author>FORBES, RYAN ; WILMER, MATTHEW ; AI, XIAOLAN ; ORKIN, CURT ; KRUSE, RANDY, P ; CHIAVAROLI, NEIL ; SMITH, BRADLEY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2011130352A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2011</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</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>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>FORBES, RYAN</creatorcontrib><creatorcontrib>WILMER, MATTHEW</creatorcontrib><creatorcontrib>AI, XIAOLAN</creatorcontrib><creatorcontrib>ORKIN, CURT</creatorcontrib><creatorcontrib>KRUSE, RANDY, P</creatorcontrib><creatorcontrib>CHIAVAROLI, NEIL</creatorcontrib><creatorcontrib>SMITH, BRADLEY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FORBES, RYAN</au><au>WILMER, MATTHEW</au><au>AI, XIAOLAN</au><au>ORKIN, CURT</au><au>KRUSE, RANDY, P</au><au>CHIAVAROLI, NEIL</au><au>SMITH, BRADLEY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LOAD SPLIT MECHANISM FOR GEAR TRANSMISSION</title><date>2011-10-20</date><risdate>2011</risdate><abstract>A method and apparatus for a transmission system selectively positioning sets of planet gear support bearings (50, 55, 80, 90) to achieve an optimized load distribution among a set of drive planet pinions (22) and a set of idler planet pinions (70) disposed in engagement between two reaction gears (30, 40) in the transmission system (A, A1), for splitting an applied load between at least two pathways between an input and an output.
L'invention concerne un procédé et un appareil pour système de transmission, caractérisés par le positionnement sélectif de jeux de roulements (50, 55, 80, 90) de guidage de satellites pour réaliser une répartition optimisée de la charge entre un ensemble de satellites menants (22) et un ensemble de satellites menés (70) disposés en engrènement entre deux engrenages (30, 40) de réaction du système (A, A1) de transmission, afin de partager une charge appliquée entre au moins deux parcours reliant une entrée à une sortie.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | LOAD SPLIT MECHANISM FOR GEAR TRANSMISSION |
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