CONTINUOUSLY VARIABLE TRANSMISSION FOR RAM AIR TURBINES
Power generation systems for aircraft are described. The power generation systems include at least one aircraft component and a ram air turbine assembly (200) configured to provide power to the at least one aircraft component. The ram air turbine assembly includes a turbine (204), a power generator...
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creator | LARSON, Michael E KONICEK, Timothy Scott |
description | Power generation systems for aircraft are described. The power generation systems include at least one aircraft component and a ram air turbine assembly (200) configured to provide power to the at least one aircraft component. The ram air turbine assembly includes a turbine (204), a power generator (212) operably connected to the turbine, and a continuously variable transmission (300) arranged between the turbine and the power generator, the continuously variable transmission configured to receive an input rotational speed from the turbine and output a constant output rotation speed to enable power generation at the power generator. |
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The power generation systems include at least one aircraft component and a ram air turbine assembly (200) configured to provide power to the at least one aircraft component. The ram air turbine assembly includes a turbine (204), a power generator (212) operably connected to the turbine, and a continuously variable transmission (300) arranged between the turbine and the power generator, the continuously variable transmission configured to receive an input rotational speed from the turbine and output a constant output rotation speed to enable power generation at the power generator.</description><language>eng ; fre ; ger</language><subject>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 ; 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=20210929&DB=EPODOC&CC=EP&NR=3705753B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210929&DB=EPODOC&CC=EP&NR=3705753B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LARSON, Michael E</creatorcontrib><creatorcontrib>KONICEK, Timothy Scott</creatorcontrib><title>CONTINUOUSLY VARIABLE TRANSMISSION FOR RAM AIR TURBINES</title><description>Power generation systems for aircraft are described. 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The ram air turbine assembly includes a turbine (204), a power generator (212) operably connected to the turbine, and a continuously variable transmission (300) arranged between the turbine and the power generator, the continuously variable transmission configured to receive an input rotational speed from the turbine and output a constant output rotation speed to enable power generation at the power generator.</description><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>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>eNrjZDB39vcL8fQL9Q8N9olUCHMM8nR08nFVCAly9Av29QwO9vT3U3DzD1IIcvRVcPQMUggJDXLy9HMN5mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxuYGpuamxk6GxkQoAQAmvSg_</recordid><startdate>20210929</startdate><enddate>20210929</enddate><creator>LARSON, Michael E</creator><creator>KONICEK, Timothy Scott</creator><scope>EVB</scope></search><sort><creationdate>20210929</creationdate><title>CONTINUOUSLY VARIABLE TRANSMISSION FOR RAM AIR TURBINES</title><author>LARSON, Michael E ; KONICEK, Timothy Scott</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3705753B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><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>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>LARSON, Michael E</creatorcontrib><creatorcontrib>KONICEK, Timothy Scott</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LARSON, Michael E</au><au>KONICEK, Timothy Scott</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>CONTINUOUSLY VARIABLE TRANSMISSION FOR RAM AIR TURBINES</title><date>2021-09-29</date><risdate>2021</risdate><abstract>Power generation systems for aircraft are described. The power generation systems include at least one aircraft component and a ram air turbine assembly (200) configured to provide power to the at least one aircraft component. The ram air turbine assembly includes a turbine (204), a power generator (212) operably connected to the turbine, and a continuously variable transmission (300) arranged between the turbine and the power generator, the continuously variable transmission configured to receive an input rotational speed from the turbine and output a constant output rotation speed to enable power generation at the power generator.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | 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 LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
title | CONTINUOUSLY VARIABLE TRANSMISSION FOR RAM AIR TURBINES |
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