Device and method for fitting two connections at the end of two conduits, in particular in an aircraft
Device for fitting two connectors at the end of two conduits, particularly in an aircraft, with a view to subsequent mutual connection of the connectors by a connecting pipe, including a body; a first support including temporary connector retainers that define an associated connector axis; an opposi...
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| creator | Fraysse Damien Thomas Benoït Gagnaire Thierry |
| description | Device for fitting two connectors at the end of two conduits, particularly in an aircraft, with a view to subsequent mutual connection of the connectors by a connecting pipe, including a body; a first support including temporary connector retainers that define an associated connector axis; an opposite second support including temporary connector retainers that define an associated connector axis; structure for moving the first support in translation relative to the body parallel to the associated connector axis, between a retracted position and a deployed position. A method of establishing fluidic communication between two conduits in an aircraft, including fitting two connectors at the end of the two conduits by such a device. |
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A method of establishing fluidic communication between two conduits in an aircraft, including fitting two connectors at the end of the two conduits by such a device.</description><language>eng</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 ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HAND TOOLS ; HEATING ; JOINTS OR FITTINGS FOR PIPES ; LIGHTING ; MANIPULATORS ; MEANS FOR THERMAL INSULATION IN GENERAL ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; PIPES ; PORTABLE POWER-DRIVEN TOOLS ; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING ; THERMAL INSULATION IN GENERAL ; TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING ; TRANSPORTING ; WEAPONS</subject><creationdate>2017</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=20171017&DB=EPODOC&CC=US&NR=9791070B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20171017&DB=EPODOC&CC=US&NR=9791070B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Fraysse Damien</creatorcontrib><creatorcontrib>Thomas Benoït</creatorcontrib><creatorcontrib>Gagnaire Thierry</creatorcontrib><title>Device and method for fitting two connections at the end of two conduits, in particular in an aircraft</title><description>Device for fitting two connectors at the end of two conduits, particularly in an aircraft, with a view to subsequent mutual connection of the connectors by a connecting pipe, including a body; a first support including temporary connector retainers that define an associated connector axis; an opposite second support including temporary connector retainers that define an associated connector axis; structure for moving the first support in translation relative to the body parallel to the associated connector axis, between a retracted position and a deployed position. A method of establishing fluidic communication between two conduits in an aircraft, including fitting two connectors at the end of the two conduits by such a device.</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>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HAND TOOLS</subject><subject>HEATING</subject><subject>JOINTS OR FITTINGS FOR PIPES</subject><subject>LIGHTING</subject><subject>MANIPULATORS</subject><subject>MEANS FOR THERMAL INSULATION IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PIPES</subject><subject>PORTABLE POWER-DRIVEN TOOLS</subject><subject>SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNirsKwkAQRbexEPUf5gMUohYhrS_s1ToMu7NmIM4suxP9fSNoLxy4HO6ZunigJ3sClAAPsk4DRM0Q2YzlDvZS8CpC3lilABpYR0BjrfH3hoGtLIEFEmZjP_SYP4YjnH3GaHM3idgXWnx35uB0vO7PK0raUknoScja26Wpm3VVV7vN9o_kDYZGPo8</recordid><startdate>20171017</startdate><enddate>20171017</enddate><creator>Fraysse Damien</creator><creator>Thomas Benoït</creator><creator>Gagnaire Thierry</creator><scope>EVB</scope></search><sort><creationdate>20171017</creationdate><title>Device and method for fitting two connections at the end of two conduits, in particular in an aircraft</title><author>Fraysse Damien ; Thomas Benoït ; Gagnaire Thierry</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US9791070B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2017</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>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HAND TOOLS</topic><topic>HEATING</topic><topic>JOINTS OR FITTINGS FOR PIPES</topic><topic>LIGHTING</topic><topic>MANIPULATORS</topic><topic>MEANS FOR THERMAL INSULATION IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PIPES</topic><topic>PORTABLE POWER-DRIVEN TOOLS</topic><topic>SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Fraysse Damien</creatorcontrib><creatorcontrib>Thomas Benoït</creatorcontrib><creatorcontrib>Gagnaire Thierry</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Fraysse Damien</au><au>Thomas Benoït</au><au>Gagnaire Thierry</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Device and method for fitting two connections at the end of two conduits, in particular in an aircraft</title><date>2017-10-17</date><risdate>2017</risdate><abstract>Device for fitting two connectors at the end of two conduits, particularly in an aircraft, with a view to subsequent mutual connection of the connectors by a connecting pipe, including a body; a first support including temporary connector retainers that define an associated connector axis; an opposite second support including temporary connector retainers that define an associated connector axis; structure for moving the first support in translation relative to the body parallel to the associated connector axis, between a retracted position and a deployed position. A method of establishing fluidic communication between two conduits in an aircraft, including fitting two connectors at the end of the two conduits by such a device.</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 GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HAND TOOLS HEATING JOINTS OR FITTINGS FOR PIPES LIGHTING MANIPULATORS MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PIPES PORTABLE POWER-DRIVEN TOOLS SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING THERMAL INSULATION IN GENERAL TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FORFASTENING, CONNECTING, DISENGAGING OR HOLDING TRANSPORTING WEAPONS |
| title | Device and method for fitting two connections at the end of two conduits, in particular in an aircraft |
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