LEADING EDGE STRUCTURE
The invention provides a leading edge structure for providing an aerodynamic surface of an aircraft, the leading edge structure comprising a skin structure, the skin structure providing an outer aerodynamic surface and an inner surface, both surfaces extending in a chordwise and spanwise direction o...
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creator | HANSEN HEINZ WILLIAMS LLIFON RAFLA MARCUS PAYNE CHRISTOPHER MCCORMICK ROBERT SALISBURY ROSS THEOBALD HUGH EVANS TIMOTHY |
description | The invention provides a leading edge structure for providing an aerodynamic surface of an aircraft, the leading edge structure comprising a skin structure, the skin structure providing an outer aerodynamic surface and an inner surface, both surfaces extending in a chordwise and spanwise direction of the structure, and a plurality of structural members, each structural member being connected to the inner surface of the skin structure and extending in the chordwise direction along the inner surface, wherein the structural members are integrally formed with the inner surface of the skin structure. The invention also provides an aircraft wing, aircraft tailplane, wing box structure, wing or wing structure and an aircraft including the leading edge structure. |
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The invention also provides an aircraft wing, aircraft tailplane, wing box structure, wing or wing structure and an aircraft including the leading edge structure.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2015</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=20150219&DB=EPODOC&CC=US&NR=2015048207A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150219&DB=EPODOC&CC=US&NR=2015048207A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HANSEN HEINZ</creatorcontrib><creatorcontrib>WILLIAMS LLIFON</creatorcontrib><creatorcontrib>RAFLA MARCUS</creatorcontrib><creatorcontrib>PAYNE CHRISTOPHER</creatorcontrib><creatorcontrib>MCCORMICK ROBERT</creatorcontrib><creatorcontrib>SALISBURY ROSS</creatorcontrib><creatorcontrib>THEOBALD HUGH</creatorcontrib><creatorcontrib>EVANS TIMOTHY</creatorcontrib><title>LEADING EDGE STRUCTURE</title><description>The invention provides a leading edge structure for providing an aerodynamic surface of an aircraft, the leading edge structure comprising a skin structure, the skin structure providing an outer aerodynamic surface and an inner surface, both surfaces extending in a chordwise and spanwise direction of the structure, and a plurality of structural members, each structural member being connected to the inner surface of the skin structure and extending in the chordwise direction along the inner surface, wherein the structural members are integrally formed with the inner surface of the skin structure. The invention also provides an aircraft wing, aircraft tailplane, wing box structure, wing or wing structure and an aircraft including the leading edge structure.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBDzcXV08fRzV3B1cXdVCA4JCnUOCQ1y5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgaGpgYmFkYG5o6GxsSpAgArRSAF</recordid><startdate>20150219</startdate><enddate>20150219</enddate><creator>HANSEN HEINZ</creator><creator>WILLIAMS LLIFON</creator><creator>RAFLA MARCUS</creator><creator>PAYNE CHRISTOPHER</creator><creator>MCCORMICK ROBERT</creator><creator>SALISBURY ROSS</creator><creator>THEOBALD HUGH</creator><creator>EVANS TIMOTHY</creator><scope>EVB</scope></search><sort><creationdate>20150219</creationdate><title>LEADING EDGE STRUCTURE</title><author>HANSEN HEINZ ; WILLIAMS LLIFON ; RAFLA MARCUS ; PAYNE CHRISTOPHER ; MCCORMICK ROBERT ; SALISBURY ROSS ; THEOBALD HUGH ; EVANS TIMOTHY</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2015048207A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</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>HANSEN HEINZ</creatorcontrib><creatorcontrib>WILLIAMS LLIFON</creatorcontrib><creatorcontrib>RAFLA MARCUS</creatorcontrib><creatorcontrib>PAYNE CHRISTOPHER</creatorcontrib><creatorcontrib>MCCORMICK ROBERT</creatorcontrib><creatorcontrib>SALISBURY ROSS</creatorcontrib><creatorcontrib>THEOBALD HUGH</creatorcontrib><creatorcontrib>EVANS TIMOTHY</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HANSEN HEINZ</au><au>WILLIAMS LLIFON</au><au>RAFLA MARCUS</au><au>PAYNE CHRISTOPHER</au><au>MCCORMICK ROBERT</au><au>SALISBURY ROSS</au><au>THEOBALD HUGH</au><au>EVANS TIMOTHY</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LEADING EDGE STRUCTURE</title><date>2015-02-19</date><risdate>2015</risdate><abstract>The invention provides a leading edge structure for providing an aerodynamic surface of an aircraft, the leading edge structure comprising a skin structure, the skin structure providing an outer aerodynamic surface and an inner surface, both surfaces extending in a chordwise and spanwise direction of the structure, and a plurality of structural members, each structural member being connected to the inner surface of the skin structure and extending in the chordwise direction along the inner surface, wherein the structural members are integrally formed with the inner surface of the skin structure. The invention also provides an aircraft wing, aircraft tailplane, wing box structure, wing or wing structure and an aircraft including the leading edge structure.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | LEADING EDGE STRUCTURE |
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