AIRCRAFT THROTTLE CONTROL DEVICE INCLUDING A CAM COUPLING
An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot...
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| creator | CARTRY THIERRY MERLET ETIENNE PAUTARD SEBASTIEN ENGLER DAVID ELABELLAOUI HAFID BESOLD JEAN-ERIC |
| description | An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position. |
| format | Patent |
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Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.</description><language>eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2014</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=20140306&DB=EPODOC&CC=US&NR=2014061389A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140306&DB=EPODOC&CC=US&NR=2014061389A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CARTRY THIERRY</creatorcontrib><creatorcontrib>MERLET ETIENNE</creatorcontrib><creatorcontrib>PAUTARD SEBASTIEN</creatorcontrib><creatorcontrib>ENGLER DAVID</creatorcontrib><creatorcontrib>ELABELLAOUI HAFID</creatorcontrib><creatorcontrib>BESOLD JEAN-ERIC</creatorcontrib><title>AIRCRAFT THROTTLE CONTROL DEVICE INCLUDING A CAM COUPLING</title><description>An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB09AxyDnJ0C1EI8QjyDwnxcVVw9vcLCfL3UXBxDfN0dlXw9HP2CXXx9HNXcFRwdvQFSocG-AC5PAysaYk5xam8UJqbQdnNNcTZQze1ID8-tbggMTk1L7UkPjTYyMDQxMDM0NjC0tHQmDhVACpnKZs</recordid><startdate>20140306</startdate><enddate>20140306</enddate><creator>CARTRY THIERRY</creator><creator>MERLET ETIENNE</creator><creator>PAUTARD SEBASTIEN</creator><creator>ENGLER DAVID</creator><creator>ELABELLAOUI HAFID</creator><creator>BESOLD JEAN-ERIC</creator><scope>EVB</scope></search><sort><creationdate>20140306</creationdate><title>AIRCRAFT THROTTLE CONTROL DEVICE INCLUDING A CAM COUPLING</title><author>CARTRY THIERRY ; MERLET ETIENNE ; PAUTARD SEBASTIEN ; ENGLER DAVID ; ELABELLAOUI HAFID ; BESOLD JEAN-ERIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2014061389A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CARTRY THIERRY</creatorcontrib><creatorcontrib>MERLET ETIENNE</creatorcontrib><creatorcontrib>PAUTARD SEBASTIEN</creatorcontrib><creatorcontrib>ENGLER DAVID</creatorcontrib><creatorcontrib>ELABELLAOUI HAFID</creatorcontrib><creatorcontrib>BESOLD JEAN-ERIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CARTRY THIERRY</au><au>MERLET ETIENNE</au><au>PAUTARD SEBASTIEN</au><au>ENGLER DAVID</au><au>ELABELLAOUI HAFID</au><au>BESOLD JEAN-ERIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT THROTTLE CONTROL DEVICE INCLUDING A CAM COUPLING</title><date>2014-03-06</date><risdate>2014</risdate><abstract>An aeroengine control device including a mount and having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel. Each lever is movable between a rest position and a maximum actuation position. The secondary lever is mounted to pivot on the main lever. Cam paths are mounted on the code wheel and on the mount in such a manner that the main lever can move the code wheel when the main lever is moved while the secondary lever is in the rest position. The secondary lever can move the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is clearly away from its rest position.</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 COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | AIRCRAFT THROTTLE CONTROL DEVICE INCLUDING A CAM COUPLING |
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