TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM
The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surf...
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| creator | ANDREANI, Luc LORENZ, Florian BLANC, Sébastien |
| description | The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surface (27) of the trailing edge movable (20). A first spacer element (26) is disposed on the upper surface (27) of the trailing edge movable (20) and extends at least over a first portion of the upper surface (27) of the trailing edge movable (20). The first spacer element (26) is configured to maintain a spacing between a first end (33) of the flexible panel element (30) and the upper surface (27) of the trailing edge movable (20) when the trailing edge movable (20) is in the extended position (60). |
| format | Patent |
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The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surface (27) of the trailing edge movable (20). A first spacer element (26) is disposed on the upper surface (27) of the trailing edge movable (20) and extends at least over a first portion of the upper surface (27) of the trailing edge movable (20). 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The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surface (27) of the trailing edge movable (20). A first spacer element (26) is disposed on the upper surface (27) of the trailing edge movable (20) and extends at least over a first portion of the upper surface (27) of the trailing edge movable (20). The first spacer element (26) is configured to maintain a spacing between a first end (33) of the flexible panel element (30) and the upper surface (27) of the trailing edge movable (20) when the trailing edge movable (20) is in the extended position (60).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2025</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZMgPCXL09PH0c1dwdXF3VQiODA5x9VVw8w9ScPRTcPQMcg5ydAsBsl0UfF1DPPxdwFL-Aa5BjiEgTY4KqPp9_cMcnXxcFfzdMKQgRvMwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXABMTCxMjc0tHQ2MilAAAwd42ZA</recordid><startdate>20250101</startdate><enddate>20250101</enddate><creator>ANDREANI, Luc</creator><creator>LORENZ, Florian</creator><creator>BLANC, Sébastien</creator><scope>EVB</scope></search><sort><creationdate>20250101</creationdate><title>TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM</title><author>ANDREANI, Luc ; LORENZ, Florian ; BLANC, Sébastien</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4484279A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2025</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ANDREANI, Luc</creatorcontrib><creatorcontrib>LORENZ, Florian</creatorcontrib><creatorcontrib>BLANC, Sébastien</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ANDREANI, Luc</au><au>LORENZ, Florian</au><au>BLANC, Sébastien</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM</title><date>2025-01-01</date><risdate>2025</risdate><abstract>The invention relates to a trailing edge system (10). The system (10) comprises a wing structure (12) to which a trailing edge movable (20) is movably coupled. A flexible panel element (30) at least partially seals a gap (21) between an upper surface (16) of the wing structure (12) and an upper surface (27) of the trailing edge movable (20). A first spacer element (26) is disposed on the upper surface (27) of the trailing edge movable (20) and extends at least over a first portion of the upper surface (27) of the trailing edge movable (20). The first spacer element (26) is configured to maintain a spacing between a first end (33) of the flexible panel element (30) and the upper surface (27) of the trailing edge movable (20) when the trailing edge movable (20) is in the extended position (60).</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 PERFORMING OPERATIONS TRANSPORTING |
| title | TRAILING EDGE SYSTEM FOR AN AIRCRAFT AND METHOD FOR OPERATING A TRAILING EDGE MOVABLE OF A TRAILING EDGE SYSTEM |
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