System for powering and controlling electrical equipment of an aircraft motor or of its environment
The system has a power supply modules set (50) whose number of power supply modules (52) is greater than a minimum number needed to activate an electrical equipment (62) of an electrical equipments group (60) to provide an emergency module (52s). A selector circuit (70) is inserted between outputs o...
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creator | BERENGER, SERGE |
description | The system has a power supply modules set (50) whose number of power supply modules (52) is greater than a minimum number needed to activate an electrical equipment (62) of an electrical equipments group (60) to provide an emergency module (52s). A selector circuit (70) is inserted between outputs of the modules and the group. A central control unit of a control device controls the modules and the circuit to activate each equipment by connecting the unit to one of the modules. The unit puts the emergency module into service in the event of a failure detected in one of the other modules. |
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A selector circuit (70) is inserted between outputs of the modules and the group. A central control unit of a control device controls the modules and the circuit to activate each equipment by connecting the unit to one of the modules. The unit puts the emergency module into service in the event of a failure detected in one of the other modules.</description><language>eng ; pol</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>2009</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=20091231&DB=EPODOC&CC=PL&NR=1852347T3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20091231&DB=EPODOC&CC=PL&NR=1852347T3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BERENGER, SERGE</creatorcontrib><title>System for powering and controlling electrical equipment of an aircraft motor or of its environment</title><description>The system has a power supply modules set (50) whose number of power supply modules (52) is greater than a minimum number needed to activate an electrical equipment (62) of an electrical equipments group (60) to provide an emergency module (52s). A selector circuit (70) is inserted between outputs of the modules and the group. A central control unit of a control device controls the modules and the circuit to activate each equipment by connecting the unit to one of the modules. The unit puts the emergency module into service in the event of a failure detected in one of the other modules.</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>2009</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzDEKQjEQBNDfWIh6h_UAFhpFe1EsLATTf0LcSCDZjZtV8fb-gAcQBoaBx4w7f_1UxQyBBQq_USLdwdENPJMKp9Q2JvQq0bsE-HjGkpEUOAwOXBQvLihk1uGiJUDUCkivKEyNTrtRcKni7NeTbn482P1pgYV7rMV5JNT-cl7uNiuz3lprzD_mC-sfP3E</recordid><startdate>20091231</startdate><enddate>20091231</enddate><creator>BERENGER, SERGE</creator><scope>EVB</scope></search><sort><creationdate>20091231</creationdate><title>System for powering and controlling electrical equipment of an aircraft motor or of its environment</title><author>BERENGER, SERGE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_PL1852347TT33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; pol</language><creationdate>2009</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>BERENGER, SERGE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BERENGER, SERGE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>System for powering and controlling electrical equipment of an aircraft motor or of its environment</title><date>2009-12-31</date><risdate>2009</risdate><abstract>The system has a power supply modules set (50) whose number of power supply modules (52) is greater than a minimum number needed to activate an electrical equipment (62) of an electrical equipments group (60) to provide an emergency module (52s). A selector circuit (70) is inserted between outputs of the modules and the group. A central control unit of a control device controls the modules and the circuit to activate each equipment by connecting the unit to one of the modules. The unit puts the emergency module into service in the event of a failure detected in one of the other modules.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; pol |
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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 | System for powering and controlling electrical equipment of an aircraft motor or of its environment |
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