Arrangement for fixing anemometric probe on opening of structural panel of aircraft, has support element comprising set of holes, flange comprising dimensions and form to surround tap opening, where flange is attached to panel
The arrangement has a stop wall (1) received partly in an opening by having its external surface levelled with an external surface of a structural panel i.e. fuselage (2). The stop wall comprises a pressure tap opening (4), and a set of openings for receiving fastenings (5) for assembly of the stop...
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| creator | THOMAS MARIE ANNE ARROUY PASCAL LEBRETON RICHARD |
| description | The arrangement has a stop wall (1) received partly in an opening by having its external surface levelled with an external surface of a structural panel i.e. fuselage (2). The stop wall comprises a pressure tap opening (4), and a set of openings for receiving fastenings (5) for assembly of the stop wall on a support element (6). The element comprises a set of holes for passage of a rod of another set of fastenings (13) for assembly of the element with a structural flange (14). The flange comprises dimensions and a form to surround the tap opening. The flange is attached to the panel. An independent claim is also included for a fuselage.
L'invention concerne un agencement pour la fixation d'un dispositif de mesure (10) sur une ouverture d'un panneau structural (2) d'aéronef présentant une surface extérieure. Selon l'invention, cet agencement comprend: - une paroi d'obturation (1) destinée à être reçue dans ladite ouverture en ayant sa surface externe affleurant avec ladite surface extérieure, cette paroi d'obturation (1) comportant au moins un premier orifice (4) de prise de pression, - ladite paroi d'obturation (1) comportant également des seconds orifices destinés à recevoir des premiers organes de fixation (5) pour l'assemblage de ladite paroi (1) sur un élément de support (6), lesdits organes de fixation (5) ayant une extrémité destinée à être affleurant avec la surface extérieure dudit panneau structural (2), - ledit élément de support (6) comportant des trous pour le passage de la tige de seconds organes de fixation (13) en vue de son assemblage avec une collerette structurale (14), - ladite collerette structurale (14) ayant des dimensions et une forme permettant d'entourer ladite ouverture, ladite collerette (14) étant destinée à être solidarisée audit panneau structural (2). |
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L'invention concerne un agencement pour la fixation d'un dispositif de mesure (10) sur une ouverture d'un panneau structural (2) d'aéronef présentant une surface extérieure. Selon l'invention, cet agencement comprend: - une paroi d'obturation (1) destinée à être reçue dans ladite ouverture en ayant sa surface externe affleurant avec ladite surface extérieure, cette paroi d'obturation (1) comportant au moins un premier orifice (4) de prise de pression, - ladite paroi d'obturation (1) comportant également des seconds orifices destinés à recevoir des premiers organes de fixation (5) pour l'assemblage de ladite paroi (1) sur un élément de support (6), lesdits organes de fixation (5) ayant une extrémité destinée à être affleurant avec la surface extérieure dudit panneau structural (2), - ledit élément de support (6) comportant des trous pour le passage de la tige de seconds organes de fixation (13) en vue de son assemblage avec une collerette structurale (14), - ladite collerette structurale (14) ayant des dimensions et une forme permettant d'entourer ladite ouverture, ladite collerette (14) étant destinée à être solidarisée audit panneau structural (2).</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20131108&DB=EPODOC&CC=FR&NR=2990191A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20131108&DB=EPODOC&CC=FR&NR=2990191A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>THOMAS MARIE ANNE</creatorcontrib><creatorcontrib>ARROUY PASCAL</creatorcontrib><creatorcontrib>LEBRETON RICHARD</creatorcontrib><title>Arrangement for fixing anemometric probe on opening of structural panel of aircraft, has support element comprising set of holes, flange comprising dimensions and form to surround tap opening, where flange is attached to panel</title><description>The arrangement has a stop wall (1) received partly in an opening by having its external surface levelled with an external surface of a structural panel i.e. fuselage (2). The stop wall comprises a pressure tap opening (4), and a set of openings for receiving fastenings (5) for assembly of the stop wall on a support element (6). The element comprises a set of holes for passage of a rod of another set of fastenings (13) for assembly of the element with a structural flange (14). The flange comprises dimensions and a form to surround the tap opening. The flange is attached to the panel. An independent claim is also included for a fuselage.
L'invention concerne un agencement pour la fixation d'un dispositif de mesure (10) sur une ouverture d'un panneau structural (2) d'aéronef présentant une surface extérieure. Selon l'invention, cet agencement comprend: - une paroi d'obturation (1) destinée à être reçue dans ladite ouverture en ayant sa surface externe affleurant avec ladite surface extérieure, cette paroi d'obturation (1) comportant au moins un premier orifice (4) de prise de pression, - ladite paroi d'obturation (1) comportant également des seconds orifices destinés à recevoir des premiers organes de fixation (5) pour l'assemblage de ladite paroi (1) sur un élément de support (6), lesdits organes de fixation (5) ayant une extrémité destinée à être affleurant avec la surface extérieure dudit panneau structural (2), - ledit élément de support (6) comportant des trous pour le passage de la tige de seconds organes de fixation (13) en vue de son assemblage avec une collerette structurale (14), - ladite collerette structurale (14) ayant des dimensions et une forme permettant d'entourer ladite ouverture, ladite collerette (14) étant destinée à être solidarisée audit panneau structural (2).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjkFKBEEMRXvjQkbvkAO0YOuql4M4uBb3Q6xOTRdUVUKSZjyvJ7FKHXDpKvDz3-ddD597VawnKlQdIivE9JHqCbBS4UKuKYAovxNwBRaq_ckRzHULvilmkNbNPcOkQTH6CCsa2CbC6kD5ZzxwEU3WeSPv_ZUz2Qgxd4G__yU1whJXax5L1yrg3BZVeWuBo1xcRjivpHQZSY1wx7DS0olvtZvhKmI2uv29uwEOz29PL3ckfCQTDFTJj4fXh3m-n-ZpPz3-o_IFQI5t4g</recordid><startdate>20131108</startdate><enddate>20131108</enddate><creator>THOMAS MARIE ANNE</creator><creator>ARROUY PASCAL</creator><creator>LEBRETON RICHARD</creator><scope>EVB</scope></search><sort><creationdate>20131108</creationdate><title>Arrangement for fixing anemometric probe on opening of structural panel of aircraft, has support element comprising set of holes, flange comprising dimensions and form to surround tap opening, where flange is attached to panel</title><author>THOMAS MARIE ANNE ; ARROUY PASCAL ; LEBRETON RICHARD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2990191A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2013</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>THOMAS MARIE ANNE</creatorcontrib><creatorcontrib>ARROUY PASCAL</creatorcontrib><creatorcontrib>LEBRETON RICHARD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>THOMAS MARIE ANNE</au><au>ARROUY PASCAL</au><au>LEBRETON RICHARD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Arrangement for fixing anemometric probe on opening of structural panel of aircraft, has support element comprising set of holes, flange comprising dimensions and form to surround tap opening, where flange is attached to panel</title><date>2013-11-08</date><risdate>2013</risdate><abstract>The arrangement has a stop wall (1) received partly in an opening by having its external surface levelled with an external surface of a structural panel i.e. fuselage (2). The stop wall comprises a pressure tap opening (4), and a set of openings for receiving fastenings (5) for assembly of the stop wall on a support element (6). The element comprises a set of holes for passage of a rod of another set of fastenings (13) for assembly of the element with a structural flange (14). The flange comprises dimensions and a form to surround the tap opening. The flange is attached to the panel. An independent claim is also included for a fuselage.
L'invention concerne un agencement pour la fixation d'un dispositif de mesure (10) sur une ouverture d'un panneau structural (2) d'aéronef présentant une surface extérieure. Selon l'invention, cet agencement comprend: - une paroi d'obturation (1) destinée à être reçue dans ladite ouverture en ayant sa surface externe affleurant avec ladite surface extérieure, cette paroi d'obturation (1) comportant au moins un premier orifice (4) de prise de pression, - ladite paroi d'obturation (1) comportant également des seconds orifices destinés à recevoir des premiers organes de fixation (5) pour l'assemblage de ladite paroi (1) sur un élément de support (6), lesdits organes de fixation (5) ayant une extrémité destinée à être affleurant avec la surface extérieure dudit panneau structural (2), - ledit élément de support (6) comportant des trous pour le passage de la tige de seconds organes de fixation (13) en vue de son assemblage avec une collerette structurale (14), - ladite collerette structurale (14) ayant des dimensions et une forme permettant d'entourer ladite ouverture, ladite collerette (14) étant destinée à être solidarisée audit panneau structural (2).</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 COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Arrangement for fixing anemometric probe on opening of structural panel of aircraft, has support element comprising set of holes, flange comprising dimensions and form to surround tap opening, where flange is attached to panel |
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