METHOD AND SYSTEM FOR CARRYING A WING PANEL OF AN AIRCRAFT
A method (800) and a system for carrying a wing panel of an aircraft are provided, the method comprising:- aligning (802) a strongback (540) over a wing panel (550);- forming (804) a vacuum attachment between an upper surface (574) of the wing panel and adjustable-length pogos (545) extending beneat...
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creator | Jones, Darrell D Swanstrom, Frederick M Smith, Daniel R Wright, Monte D |
description | A method (800) and a system for carrying a wing panel of an aircraft are provided, the method comprising:- aligning (802) a strongback (540) over a wing panel (550);- forming (804) a vacuum attachment between an upper surface (574) of the wing panel and adjustable-length pogos (545) extending beneath the strongback; and- adjusting (806) the length of at least one of the pogos to impart forces onto the wing panel and enforce a predetermined contour (544) to the wing panel; and- further comprising advancing the wing panel (550) in a process direction (541) while the contour (544) is enforced.The system comprises:- a strongback (540) configured to extend over a transverse section of a wing panel (550);- adjustable-length pogos (545) that extend beneath the strongback; and- vacuum couplers (548) at the pogos that are configured to form a vacuum attachment to an upper surface (574) of the wing panel;wherein the strongback (540) is configured to, during advancing in a process direction, enforce a contour (544) onto the wing panel by holding each pogo (545) at a desired length. |
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and- adjusting (806) the length of at least one of the pogos to impart forces onto the wing panel and enforce a predetermined contour (544) to the wing panel; and- further comprising advancing the wing panel (550) in a process direction (541) while the contour (544) is enforced.The system comprises:- a strongback (540) configured to extend over a transverse section of a wing panel (550);- adjustable-length pogos (545) that extend beneath the strongback; and- vacuum couplers (548) at the pogos that are configured to form a vacuum attachment to an upper surface (574) of the wing panel;wherein the strongback (540) is configured to, during advancing in a process direction, enforce a contour (544) onto the wing panel by holding each pogo (545) at a desired length.</description><language>eng ; fre ; ger</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2022</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=20220525&DB=EPODOC&CC=EP&NR=4000899A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220525&DB=EPODOC&CC=EP&NR=4000899A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Jones, Darrell D</creatorcontrib><creatorcontrib>Swanstrom, Frederick M</creatorcontrib><creatorcontrib>Smith, Daniel R</creatorcontrib><creatorcontrib>Wright, Monte D</creatorcontrib><title>METHOD AND SYSTEM FOR CARRYING A WING PANEL OF AN AIRCRAFT</title><description>A method (800) and a system for carrying a wing panel of an aircraft are provided, the method comprising:- aligning (802) a strongback (540) over a wing panel (550);- forming (804) a vacuum attachment between an upper surface (574) of the wing panel and adjustable-length pogos (545) extending beneath the strongback; and- adjusting (806) the length of at least one of the pogos to impart forces onto the wing panel and enforce a predetermined contour (544) to the wing panel; and- further comprising advancing the wing panel (550) in a process direction (541) while the contour (544) is enforced.The system comprises:- a strongback (540) configured to extend over a transverse section of a wing panel (550);- adjustable-length pogos (545) that extend beneath the strongback; and- vacuum couplers (548) at the pogos that are configured to form a vacuum attachment to an upper surface (574) of the wing panel;wherein the strongback (540) is configured to, during advancing in a process direction, enforce a contour (544) onto the wing panel by holding each pogo (545) at a desired length.</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</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>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDydQ3x8HdRcPRzUQiODA5x9VVw8w9ScHYMCor09HNXcFQIB1EBjn6uPgr-bkB1Co6eQc5Bjm4hPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXAxMDAwMLS0tHQmAglACuiKBo</recordid><startdate>20220525</startdate><enddate>20220525</enddate><creator>Jones, Darrell D</creator><creator>Swanstrom, Frederick M</creator><creator>Smith, Daniel R</creator><creator>Wright, Monte D</creator><scope>EVB</scope></search><sort><creationdate>20220525</creationdate><title>METHOD AND SYSTEM FOR CARRYING A WING PANEL OF AN AIRCRAFT</title><author>Jones, Darrell D ; 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and- adjusting (806) the length of at least one of the pogos to impart forces onto the wing panel and enforce a predetermined contour (544) to the wing panel; and- further comprising advancing the wing panel (550) in a process direction (541) while the contour (544) is enforced.The system comprises:- a strongback (540) configured to extend over a transverse section of a wing panel (550);- adjustable-length pogos (545) that extend beneath the strongback; and- vacuum couplers (548) at the pogos that are configured to form a vacuum attachment to an upper surface (574) of the wing panel;wherein the strongback (540) is configured to, during advancing in a process direction, enforce a contour (544) onto the wing panel by holding each pogo (545) at a desired length.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
title | METHOD AND SYSTEM FOR CARRYING A WING PANEL OF AN AIRCRAFT |
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