DE2141371
A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shif...
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| creator | TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC WALKER, COLIN G., LAVAL DARLINGTON, RALPH F., LACHINE LEADBEATER, EDWARD J., MONTREAL |
| description | A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shift during shutdown of the failed channel. |
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This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shift during shutdown of the failed channel.</description><edition>3</edition><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; COSMONAUTICS ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; HELICOPTERS ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES ; TRANSPORTING</subject><creationdate>1980</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=19801030&DB=EPODOC&CC=DE&NR=2141371C3$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19801030&DB=EPODOC&CC=DE&NR=2141371C3$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC</creatorcontrib><creatorcontrib>WALKER, COLIN G., LAVAL</creatorcontrib><creatorcontrib>DARLINGTON, RALPH F., LACHINE</creatorcontrib><creatorcontrib>LEADBEATER, EDWARD J., MONTREAL</creatorcontrib><title>DE2141371</title><description>A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shift during shutdown of the failed channel.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>HELICOPTERS</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1980</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOB0cTUyNDE0NjfkYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxcPXOxsZEKAEAyF8aWg</recordid><startdate>19801030</startdate><enddate>19801030</enddate><creator>TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC</creator><creator>WALKER, COLIN G., LAVAL</creator><creator>DARLINGTON, RALPH F., LACHINE</creator><creator>LEADBEATER, EDWARD J., MONTREAL</creator><scope>EVB</scope></search><sort><creationdate>19801030</creationdate><title>DE2141371</title><author>TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC ; WALKER, COLIN G., LAVAL ; DARLINGTON, RALPH F., LACHINE ; LEADBEATER, EDWARD J., MONTREAL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE2141371C33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1980</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>HELICOPTERS</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC</creatorcontrib><creatorcontrib>WALKER, COLIN G., LAVAL</creatorcontrib><creatorcontrib>DARLINGTON, RALPH F., LACHINE</creatorcontrib><creatorcontrib>LEADBEATER, EDWARD J., MONTREAL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC</au><au>WALKER, COLIN G., LAVAL</au><au>DARLINGTON, RALPH F., LACHINE</au><au>LEADBEATER, EDWARD J., MONTREAL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DE2141371</title><date>1980-10-30</date><risdate>1980</risdate><abstract>A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shift during shutdown of the failed channel.</abstract><edition>3</edition><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING |
| title | DE2141371 |
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