ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT
L'invention concerne un ensemble de liaison (100) entre deux structures (130, 150) d'un aéronef, l'ensemble de liaison (100) comprenant un élément central présentant un trou de passage, préférentiellement un alésage, agencé pour opérer une liaison avec l'une des deux structures (...
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| creator | MATHEIS, Xavier GOUPIL, Frédéric |
| description | L'invention concerne un ensemble de liaison (100) entre deux structures (130, 150) d'un aéronef, l'ensemble de liaison (100) comprenant un élément central présentant un trou de passage, préférentiellement un alésage, agencé pour opérer une liaison avec l'une des deux structures (150) grâce à un élément de fixation (160, 161) comportant une tige (160') insérée dans le trou de passage, l'ensemble de liaison (100) comprenant en outre une pluralité d'éléments amortisseurs faits d'un matériau déformable, chacun des éléments amortisseurs étant solidaire dudit élément central d'une part, et configuré pour prendre appui sur une surface de l'autre structure (130) parmi les deux structures (130, 150), d'autre part. L'invention concerne également une partie d'aéronef (400) comprenant un tel ensemble de liaison (100).
A connecting assembly for connecting two structures of an aircraft, the connecting assembly including a central element featuring a through-hole, preferably a bore, configured to make a connection with one of the two structures by virtue of a fastener element including a shank inserted into the through-hole. The connecting assembly further includes a plurality of shock-absorbing elements made from a deformable material. Each of the shock-absorbing elements are, on the one hand, secured to the central element and, on the other hand, configured to bear against a surface of the other of the two structures. An aircraft part includes such a connecting assembly. |
| format | Patent |
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A connecting assembly for connecting two structures of an aircraft, the connecting assembly including a central element featuring a through-hole, preferably a bore, configured to make a connection with one of the two structures by virtue of a fastener element including a shank inserted into the through-hole. The connecting assembly further includes a plurality of shock-absorbing elements made from a deformable material. Each of the shock-absorbing elements are, on the one hand, secured to the central element and, on the other hand, configured to bear against a surface of the other of the two structures. An aircraft part includes such a connecting assembly.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BEARINGS ; BLASTING ; COSMONAUTICS ; DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ; ELEMENTS OR CRANKSHAFT MECHANISMS ; ENGINEERING ELEMENTS AND UNITS ; FLEXIBLE SHAFTS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; ROTARY BODIES OTHER THAN GEARING ELEMENTS ; SHAFTS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</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=20221005&DB=EPODOC&CC=EP&NR=4067226A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221005&DB=EPODOC&CC=EP&NR=4067226A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MATHEIS, Xavier</creatorcontrib><creatorcontrib>GOUPIL, Frédéric</creatorcontrib><title>ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT</title><description>L'invention concerne un ensemble de liaison (100) entre deux structures (130, 150) d'un aéronef, l'ensemble de liaison (100) comprenant un élément central présentant un trou de passage, préférentiellement un alésage, agencé pour opérer une liaison avec l'une des deux structures (150) grâce à un élément de fixation (160, 161) comportant une tige (160') insérée dans le trou de passage, l'ensemble de liaison (100) comprenant en outre une pluralité d'éléments amortisseurs faits d'un matériau déformable, chacun des éléments amortisseurs étant solidaire dudit élément central d'une part, et configuré pour prendre appui sur une surface de l'autre structure (130) parmi les deux structures (130, 150), d'autre part. L'invention concerne également une partie d'aéronef (400) comprenant un tel ensemble de liaison (100).
A connecting assembly for connecting two structures of an aircraft, the connecting assembly including a central element featuring a through-hole, preferably a bore, configured to make a connection with one of the two structures by virtue of a fastener element including a shank inserted into the through-hole. The connecting assembly further includes a plurality of shock-absorbing elements made from a deformable material. Each of the shock-absorbing elements are, on the one hand, secured to the central element and, on the other hand, configured to bear against a surface of the other of the two structures. An aircraft part includes such a connecting assembly.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BEARINGS</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING</subject><subject>ELEMENTS OR CRANKSHAFT MECHANISMS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FLEXIBLE SHAFTS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>ROTARY BODIES OTHER THAN GEARING ELEMENTS</subject><subject>SHAFTS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjTELwjAUhLs4iPof3g-ooFXaOY0vNmCT8PJCcSpF4iRaqKM_3iLFwcnpuLuPu3nyEt5jXZ7OoCyBtMagZG0NlMgNogFuLHimIDkQerAKhAGhSZJQnIITxD_huFI70l6bI_ggq083vaSjOXzJZTK7drchriZdJKCQZbWO_aONQ99d4j0-W3T7TV5kWS62uz-QN-pPOks</recordid><startdate>20221005</startdate><enddate>20221005</enddate><creator>MATHEIS, Xavier</creator><creator>GOUPIL, Frédéric</creator><scope>EVB</scope></search><sort><creationdate>20221005</creationdate><title>ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT</title><author>MATHEIS, Xavier ; GOUPIL, Frédéric</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4067226A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BEARINGS</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING</topic><topic>ELEMENTS OR CRANKSHAFT MECHANISMS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FLEXIBLE SHAFTS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>ROTARY BODIES OTHER THAN GEARING ELEMENTS</topic><topic>SHAFTS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MATHEIS, Xavier</creatorcontrib><creatorcontrib>GOUPIL, Frédéric</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MATHEIS, Xavier</au><au>GOUPIL, Frédéric</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT</title><date>2022-10-05</date><risdate>2022</risdate><abstract>L'invention concerne un ensemble de liaison (100) entre deux structures (130, 150) d'un aéronef, l'ensemble de liaison (100) comprenant un élément central présentant un trou de passage, préférentiellement un alésage, agencé pour opérer une liaison avec l'une des deux structures (150) grâce à un élément de fixation (160, 161) comportant une tige (160') insérée dans le trou de passage, l'ensemble de liaison (100) comprenant en outre une pluralité d'éléments amortisseurs faits d'un matériau déformable, chacun des éléments amortisseurs étant solidaire dudit élément central d'une part, et configuré pour prendre appui sur une surface de l'autre structure (130) parmi les deux structures (130, 150), d'autre part. L'invention concerne également une partie d'aéronef (400) comprenant un tel ensemble de liaison (100).
A connecting assembly for connecting two structures of an aircraft, the connecting assembly including a central element featuring a through-hole, preferably a bore, configured to make a connection with one of the two structures by virtue of a fastener element including a shank inserted into the through-hole. The connecting assembly further includes a plurality of shock-absorbing elements made from a deformable material. Each of the shock-absorbing elements are, on the one hand, secured to the central element and, on the other hand, configured to bear against a surface of the other of the two structures. An aircraft part includes such a connecting assembly.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT AVIATION BEARINGS BLASTING COSMONAUTICS DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ELEMENTS OR CRANKSHAFT MECHANISMS ENGINEERING ELEMENTS AND UNITS FLEXIBLE SHAFTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS ROTARY BODIES OTHER THAN GEARING ELEMENTS SHAFTS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | ASSEMBLY FOR CONNECTION BETWEEN TWO STRUCTURES OF AN AIRCRAFT, PART OF AN AIRCRAFT COMPRISING SUCH AN ASSEMBLY, AND AIRCRAFT |
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