Connection system for long hollow bodies and method of connecting long hollow bodies
The connection system (1) has two connection elements (2,3) which are attached on ends of elongated hollow bodies. The ends face each other. The former connecting element has a projecting element (6) arranged in a radial direction. A locking unit (12) is arranged between the two connection elements,...
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| creator | HUBER, ALFRED MAYER, MANUEL HOEFLE ROLAND |
| description | The connection system (1) has two connection elements (2,3) which are attached on ends of elongated hollow bodies. The ends face each other. The former connecting element has a projecting element (6) arranged in a radial direction. A locking unit (12) is arranged between the two connection elements, which forms a detachable connection between the connection elements. The projecting element partially covers the outer periphery of the former connection element. A sealing (10) is attached on the latter connection element, whose sealing surfaces faces the former connection element. Independent claims are included for the following: (1) an aircraft with an air-conditioning system; and (2) a method for connecting two elongated hollow bodies, particularly for pipes or for flat channels in an aircraft.
Die Erfindung betrifft ein Verbindungssystem für längliche Hohlkörper (22), insbesondere für Rohre oder für Flachkanäle in einem Flugzeug, das ein erstes Verbindungselement (2) und ein zweites Verbindungselement (3) umfasst, die auf einander zugewandten Enden auf länglichen Hohlkörpern (22) anbringbar sind, wobei das erste Verbindungselement (2) wenigstens ein in einer radialen Richtung angeordnetes hervorstehendes Element (6) aufweist, das im Falle eines Zusammenschiebens in eine korrespondierende Ausnehmung (7) des zweiten Verbindungselements (3) einführbar ist, wobei zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) ein Verriegelungsmittel (12) angeordnet ist, das eine lösbare Verbindung zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) schafft. Des Weiteren betrifft die Erfindung ein Verfahren zur Verbindung zweier länglicher Hohlkörper, insbesondere für Rohre oder für Flachkanäle in einem Flugzeug. |
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Die Erfindung betrifft ein Verbindungssystem für längliche Hohlkörper (22), insbesondere für Rohre oder für Flachkanäle in einem Flugzeug, das ein erstes Verbindungselement (2) und ein zweites Verbindungselement (3) umfasst, die auf einander zugewandten Enden auf länglichen Hohlkörpern (22) anbringbar sind, wobei das erste Verbindungselement (2) wenigstens ein in einer radialen Richtung angeordnetes hervorstehendes Element (6) aufweist, das im Falle eines Zusammenschiebens in eine korrespondierende Ausnehmung (7) des zweiten Verbindungselements (3) einführbar ist, wobei zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) ein Verriegelungsmittel (12) angeordnet ist, das eine lösbare Verbindung zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) schafft. Des Weiteren betrifft die Erfindung ein Verfahren zur Verbindung zweier länglicher Hohlkörper, insbesondere für Rohre oder für Flachkanäle in einem Flugzeug.</description><language>eng ; fre ; ger</language><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING ; 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 ; HEATING ; JOINTS OR FITTINGS FOR PIPES ; LIGHTING ; MEANS FOR THERMAL INSULATION IN GENERAL ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; PIPES ; RANGES ; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; VENTILATING ; WEAPONS</subject><creationdate>2013</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=20130206&DB=EPODOC&CC=EP&NR=2554890A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20130206&DB=EPODOC&CC=EP&NR=2554890A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUBER, ALFRED</creatorcontrib><creatorcontrib>MAYER, MANUEL</creatorcontrib><creatorcontrib>HOEFLE ROLAND</creatorcontrib><title>Connection system for long hollow bodies and method of connecting long hollow bodies</title><description>The connection system (1) has two connection elements (2,3) which are attached on ends of elongated hollow bodies. The ends face each other. The former connecting element has a projecting element (6) arranged in a radial direction. A locking unit (12) is arranged between the two connection elements, which forms a detachable connection between the connection elements. The projecting element partially covers the outer periphery of the former connection element. A sealing (10) is attached on the latter connection element, whose sealing surfaces faces the former connection element. Independent claims are included for the following: (1) an aircraft with an air-conditioning system; and (2) a method for connecting two elongated hollow bodies, particularly for pipes or for flat channels in an aircraft.
Die Erfindung betrifft ein Verbindungssystem für längliche Hohlkörper (22), insbesondere für Rohre oder für Flachkanäle in einem Flugzeug, das ein erstes Verbindungselement (2) und ein zweites Verbindungselement (3) umfasst, die auf einander zugewandten Enden auf länglichen Hohlkörpern (22) anbringbar sind, wobei das erste Verbindungselement (2) wenigstens ein in einer radialen Richtung angeordnetes hervorstehendes Element (6) aufweist, das im Falle eines Zusammenschiebens in eine korrespondierende Ausnehmung (7) des zweiten Verbindungselements (3) einführbar ist, wobei zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) ein Verriegelungsmittel (12) angeordnet ist, das eine lösbare Verbindung zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) schafft. Des Weiteren betrifft die Erfindung ein Verfahren zur Verbindung zweier länglicher Hohlkörper, insbesondere für Rohre oder für Flachkanäle in einem Flugzeug.</description><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</subject><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>HEATING</subject><subject>JOINTS OR FITTINGS FOR PIPES</subject><subject>LIGHTING</subject><subject>MEANS FOR THERMAL INSULATION IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PIPES</subject><subject>RANGES</subject><subject>SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>VENTILATING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAhxzs_LS00uyczPUyiuLC5JzVVIyy9SyMnPS1fIyM_JyS9XSMpPyUwtVkjMS1HITS3JyE9RyE9TSIZqAyrDVMvDwJqWmFOcyguluRkU3FxDnD10Uwvy41OLCxKTU_NSS-JdA4xMTU0sLA0cjYyJUAIAOkA4ig</recordid><startdate>20130206</startdate><enddate>20130206</enddate><creator>HUBER, ALFRED</creator><creator>MAYER, MANUEL</creator><creator>HOEFLE ROLAND</creator><scope>EVB</scope></search><sort><creationdate>20130206</creationdate><title>Connection system for long hollow bodies and method of connecting long hollow bodies</title><author>HUBER, ALFRED ; MAYER, MANUEL ; HOEFLE ROLAND</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2554890A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2013</creationdate><topic>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</topic><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>HEATING</topic><topic>JOINTS OR FITTINGS FOR PIPES</topic><topic>LIGHTING</topic><topic>MEANS FOR THERMAL INSULATION IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PIPES</topic><topic>RANGES</topic><topic>SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>VENTILATING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>HUBER, ALFRED</creatorcontrib><creatorcontrib>MAYER, MANUEL</creatorcontrib><creatorcontrib>HOEFLE ROLAND</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUBER, ALFRED</au><au>MAYER, MANUEL</au><au>HOEFLE ROLAND</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Connection system for long hollow bodies and method of connecting long hollow bodies</title><date>2013-02-06</date><risdate>2013</risdate><abstract>The connection system (1) has two connection elements (2,3) which are attached on ends of elongated hollow bodies. The ends face each other. The former connecting element has a projecting element (6) arranged in a radial direction. A locking unit (12) is arranged between the two connection elements, which forms a detachable connection between the connection elements. The projecting element partially covers the outer periphery of the former connection element. A sealing (10) is attached on the latter connection element, whose sealing surfaces faces the former connection element. Independent claims are included for the following: (1) an aircraft with an air-conditioning system; and (2) a method for connecting two elongated hollow bodies, particularly for pipes or for flat channels in an aircraft.
Die Erfindung betrifft ein Verbindungssystem für längliche Hohlkörper (22), insbesondere für Rohre oder für Flachkanäle in einem Flugzeug, das ein erstes Verbindungselement (2) und ein zweites Verbindungselement (3) umfasst, die auf einander zugewandten Enden auf länglichen Hohlkörpern (22) anbringbar sind, wobei das erste Verbindungselement (2) wenigstens ein in einer radialen Richtung angeordnetes hervorstehendes Element (6) aufweist, das im Falle eines Zusammenschiebens in eine korrespondierende Ausnehmung (7) des zweiten Verbindungselements (3) einführbar ist, wobei zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) ein Verriegelungsmittel (12) angeordnet ist, das eine lösbare Verbindung zwischen dem ersten Verbindungselement (2) und dem zweiten Verbindungselement (3) schafft. Des Weiteren betrifft die Erfindung ein Verfahren zur Verbindung zweier länglicher Hohlkörper, insbesondere für Rohre oder für Flachkanäle in einem Flugzeug.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING 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 HEATING JOINTS OR FITTINGS FOR PIPES LIGHTING MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PIPES RANGES SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING THERMAL INSULATION IN GENERAL TRANSPORTING VENTILATING WEAPONS |
| title | Connection system for long hollow bodies and method of connecting long hollow bodies |
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