ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT
Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed pos...
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| creator | SMITH, Howard Ian HANSON, Thomas BUDNITSKY, Dmitry |
| description | Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member. |
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An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</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=20240711&DB=EPODOC&CC=US&NR=2024228016A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76292</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240711&DB=EPODOC&CC=US&NR=2024228016A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SMITH, Howard Ian</creatorcontrib><creatorcontrib>HANSON, Thomas</creatorcontrib><creatorcontrib>BUDNITSKY, Dmitry</creatorcontrib><title>ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT</title><description>Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPBwDA529XXy8XQNVnD0c1HwdQ3x8HcJVnDzD1JwcQ3w8Y_09HNXcFQICXL09AExXV3cXRXcfBwDFPzdgDoUHD2DnIMc3UJ4GFjTEnOKU3mhNDeDsptriLOHbmpBfnxqcUFicmpeakl8aLCRgZGJkZGFgaGZo6ExcaoAcIEtHQ</recordid><startdate>20240711</startdate><enddate>20240711</enddate><creator>SMITH, Howard Ian</creator><creator>HANSON, Thomas</creator><creator>BUDNITSKY, Dmitry</creator><scope>EVB</scope></search><sort><creationdate>20240711</creationdate><title>ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT</title><author>SMITH, Howard Ian ; HANSON, Thomas ; BUDNITSKY, Dmitry</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2024228016A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2024</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>SMITH, Howard Ian</creatorcontrib><creatorcontrib>HANSON, Thomas</creatorcontrib><creatorcontrib>BUDNITSKY, Dmitry</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SMITH, Howard Ian</au><au>HANSON, Thomas</au><au>BUDNITSKY, Dmitry</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT</title><date>2024-07-11</date><risdate>2024</risdate><abstract>Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT |
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