PLANET GEAR HAVING FAILURE MODE OPTIMIZED FOR CONTINUED PLANETARY GEAR SYSTEM OPERATION
A method of optimizing a planetary gear system for continued operation after failure of a planet gear includes providing a planetary gear system and reducing a backup ratio of a planet gear of the planetary gear system by reducing a rim thickness of the planet gear. Un procédé doptimisation dun syst...
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| creator | WOODS, RON EHINGER, RYAN THOMAS |
| description | A method of optimizing a planetary gear system for continued operation after failure of a planet gear includes providing a planetary gear system and reducing a backup ratio of a planet gear of the planetary gear system by reducing a rim thickness of the planet gear.
Un procédé doptimisation dun système dengrenages planétaires pour un fonctionnement continu après défaillance dun engrenage planétaire comprend la fourniture dun système dengrenages planétaires et la réduction dun rapport de sauvegarde dun engrenage planétaire du système dengrenage planétaire par réduction dune épaisseur de jante de lengrenage planétaire. |
| format | Patent |
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Un procédé doptimisation dun système dengrenages planétaires pour un fonctionnement continu après défaillance dun engrenage planétaire comprend la fourniture dun système dengrenages planétaires et la réduction dun rapport de sauvegarde dun engrenage planétaire du système dengrenage planétaire par réduction dune épaisseur de jante de lengrenage planétaire.</description><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GEARING ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2021</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=20210518&DB=EPODOC&CC=CA&NR=3012147C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210518&DB=EPODOC&CC=CA&NR=3012147C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WOODS, RON</creatorcontrib><creatorcontrib>EHINGER, RYAN THOMAS</creatorcontrib><title>PLANET GEAR HAVING FAILURE MODE OPTIMIZED FOR CONTINUED PLANETARY GEAR SYSTEM OPERATION</title><description>A method of optimizing a planetary gear system for continued operation after failure of a planet gear includes providing a planetary gear system and reducing a backup ratio of a planet gear of the planetary gear system by reducing a rim thickness of the planet gear.
Un procédé doptimisation dun système dengrenages planétaires pour un fonctionnement continu après défaillance dun engrenage planétaire comprend la fourniture dun système dengrenages planétaires et la réduction dun rapport de sauvegarde dun engrenage planétaire du système dengrenage planétaire par réduction dune épaisseur de jante de lengrenage planétaire.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</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>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAgP8HH0cw1RcHd1DFLwcAzz9HNXcHP09AkNclXw9XdxVfAPCPH09YxydVFw8w9ScPb3C_H0CwXyIPocgyIhWoMjg0NcfYGqXYMcQzz9_XgYWNMSc4pTeaE0N4O8m2uIs4duakF-fGpxQWJyal5qSbyzo7GBoZGhibmzMWEVAAL5MB8</recordid><startdate>20210518</startdate><enddate>20210518</enddate><creator>WOODS, RON</creator><creator>EHINGER, RYAN THOMAS</creator><scope>EVB</scope></search><sort><creationdate>20210518</creationdate><title>PLANET GEAR HAVING FAILURE MODE OPTIMIZED FOR CONTINUED PLANETARY GEAR SYSTEM OPERATION</title><author>WOODS, RON ; EHINGER, RYAN THOMAS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA3012147C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2021</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</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>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>WOODS, RON</creatorcontrib><creatorcontrib>EHINGER, RYAN THOMAS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WOODS, RON</au><au>EHINGER, RYAN THOMAS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PLANET GEAR HAVING FAILURE MODE OPTIMIZED FOR CONTINUED PLANETARY GEAR SYSTEM OPERATION</title><date>2021-05-18</date><risdate>2021</risdate><abstract>A method of optimizing a planetary gear system for continued operation after failure of a planet gear includes providing a planetary gear system and reducing a backup ratio of a planet gear of the planetary gear system by reducing a rim thickness of the planet gear.
Un procédé doptimisation dun système dengrenages planétaires pour un fonctionnement continu après défaillance dun engrenage planétaire comprend la fourniture dun système dengrenages planétaires et la réduction dun rapport de sauvegarde dun engrenage planétaire du système dengrenage planétaire par réduction dune épaisseur de jante de lengrenage planétaire.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | PLANET GEAR HAVING FAILURE MODE OPTIMIZED FOR CONTINUED PLANETARY GEAR SYSTEM OPERATION |
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