GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY
The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also...
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| creator | TONDU, Thomas |
| description | The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also comprises: - a retaining element (120), a first portion (121) of which is fixedly inserted into at least the adhesive interlayer and a second portion (122) of which extends the first portion outside of the glazing; - a plurality of cleats (130) arranged in respective cavities (140) formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies. |
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The glazed assembly also comprises: - a retaining element (120), a first portion (121) of which is fixedly inserted into at least the adhesive interlayer and a second portion (122) of which extends the first portion outside of the glazing; - a plurality of cleats (130) arranged in respective cavities (140) formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; PERFORMING OPERATIONS ; REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES ; TRANSPORTING ; VEHICLES IN GENERAL ; WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES</subject><creationdate>2024</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=20241218&DB=EPODOC&CC=EP&NR=4476134A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241218&DB=EPODOC&CC=EP&NR=4476134A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TONDU, Thomas</creatorcontrib><title>GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY</title><description>The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also comprises: - a retaining element (120), a first portion (121) of which is fixedly inserted into at least the adhesive interlayer and a second portion (122) of which extends the first portion outside of the glazing; - a plurality of cleats (130) arranged in respective cavities (140) formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>PERFORMING OPERATIONS</subject><subject>REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES</subject><subject>TRANSPORTING</subject><subject>VEHICLES IN GENERAL</subject><subject>WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZKh393GMcnVRcAwOdvV18olUcPMPUnD0U3D0DHIOcnQL0VHwdQ3x8HcBi_s6-oW6OTqHhAZ5-rkrBIc6eyg4KqAb4OjnAtet4OzvGxDkGYxbOQ8Da1piTnEqL5TmZlBwcw1x9tBNLciPTy0uSExOzUstiXcNMDExNzM0NnE0NCZCCQBmjjr5</recordid><startdate>20241218</startdate><enddate>20241218</enddate><creator>TONDU, Thomas</creator><scope>EVB</scope></search><sort><creationdate>20241218</creationdate><title>GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY</title><author>TONDU, Thomas</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4476134A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>PERFORMING OPERATIONS</topic><topic>REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES</topic><topic>TRANSPORTING</topic><topic>VEHICLES IN GENERAL</topic><topic>WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES</topic><toplevel>online_resources</toplevel><creatorcontrib>TONDU, Thomas</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TONDU, Thomas</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY</title><date>2024-12-18</date><risdate>2024</risdate><abstract>The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by means of an adhesive interlayer (115). The glazed assembly also comprises: - a retaining element (120), a first portion (121) of which is fixedly inserted into at least the adhesive interlayer and a second portion (122) of which extends the first portion outside of the glazing; - a plurality of cleats (130) arranged in respective cavities (140) formed in the glazing in such a way that the cleats extend through the first portion and into each of the structural plies.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES TRANSPORTING VEHICLES IN GENERAL WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES |
| title | GLAZED ASSEMBLY FOR AN AIRCRAFT, METHOD FOR MANUFACTURING SUCH A GLAZED ASSEMBLY AND AIRCRAFT COMPRISING SUCH A GLAZED ASSEMBLY |
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