AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY
An automated apparatus for use in selectively installing temporary fasteners in an assembly is provided. The apparatus includes an end effector, a cutting mechanism coupled to the end effector and that forms an opening in the assembly when a potential opening location is substantially aligned with a...
Gespeichert in:
Hauptverfasser: | , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | FRENCH FRANKLIN BERNARD LONG DANIEL THOMAS COLE DAVID WILLIAM |
description | An automated apparatus for use in selectively installing temporary fasteners in an assembly is provided. The apparatus includes an end effector, a cutting mechanism coupled to the end effector and that forms an opening in the assembly when a potential opening location is substantially aligned with a cutting mechanism center point. The apparatus also includes at least one of a first sub-assembly and a second sub-assembly coupled to the end effector. The first sub-assembly includes a temporary fastener insertion mechanism that inserts a temporary fastener through the opening in the assembly when the opening is substantially aligned with an insertion mechanism center point different from the cutting mechanism center point. The second sub-assembly includes a temporary fastener removal mechanism that removes installed temporary fasteners from the assembly when the installed temporary fastener is substantially aligned with a removal mechanism center point different from the cutting mechanism center point. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2015298825A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2015298825A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2015298825A13</originalsourceid><addsrcrecordid>eNqNirsKwkAQANNYiPoPC9aCiQRiucaNHtyL2z0xVQhyVqKB-P8YwQ8QBoaBmWdXjOIMCh0BvceAEhkaFyAygbLApKkWdSHdTsmCWit7AiHjXcDQQoMsZCnw98YJZjIH3S6z2b1_jGn18yJbNyT1eZOGV5fGob-lZ3p3kYttXhb7qipKzHf_XR_qCjKZ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY</title><source>esp@cenet</source><creator>FRENCH FRANKLIN BERNARD ; LONG DANIEL THOMAS ; COLE DAVID WILLIAM</creator><creatorcontrib>FRENCH FRANKLIN BERNARD ; LONG DANIEL THOMAS ; COLE DAVID WILLIAM</creatorcontrib><description>An automated apparatus for use in selectively installing temporary fasteners in an assembly is provided. The apparatus includes an end effector, a cutting mechanism coupled to the end effector and that forms an opening in the assembly when a potential opening location is substantially aligned with a cutting mechanism center point. The apparatus also includes at least one of a first sub-assembly and a second sub-assembly coupled to the end effector. The first sub-assembly includes a temporary fastener insertion mechanism that inserts a temporary fastener through the opening in the assembly when the opening is substantially aligned with an insertion mechanism center point different from the cutting mechanism center point. The second sub-assembly includes a temporary fastener removal mechanism that removes installed temporary fasteners from the assembly when the installed temporary fastener is substantially aligned with a removal mechanism center point different from the cutting mechanism center point.</description><language>eng</language><subject>AIRCRAFT ; AVIATION ; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; MACHINE TOOLS ; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; 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=20151022&DB=EPODOC&CC=US&NR=2015298825A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20151022&DB=EPODOC&CC=US&NR=2015298825A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FRENCH FRANKLIN BERNARD</creatorcontrib><creatorcontrib>LONG DANIEL THOMAS</creatorcontrib><creatorcontrib>COLE DAVID WILLIAM</creatorcontrib><title>AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY</title><description>An automated apparatus for use in selectively installing temporary fasteners in an assembly is provided. The apparatus includes an end effector, a cutting mechanism coupled to the end effector and that forms an opening in the assembly when a potential opening location is substantially aligned with a cutting mechanism center point. The apparatus also includes at least one of a first sub-assembly and a second sub-assembly coupled to the end effector. The first sub-assembly includes a temporary fastener insertion mechanism that inserts a temporary fastener through the opening in the assembly when the opening is substantially aligned with an insertion mechanism center point different from the cutting mechanism center point. The second sub-assembly includes a temporary fastener removal mechanism that removes installed temporary fasteners from the assembly when the installed temporary fastener is substantially aligned with a removal mechanism center point different from the cutting mechanism center point.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING</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>MACHINE TOOLS</subject><subject>MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS</subject><subject>METAL-WORKING NOT OTHERWISE PROVIDED FOR</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNirsKwkAQANNYiPoPC9aCiQRiucaNHtyL2z0xVQhyVqKB-P8YwQ8QBoaBmWdXjOIMCh0BvceAEhkaFyAygbLApKkWdSHdTsmCWit7AiHjXcDQQoMsZCnw98YJZjIH3S6z2b1_jGn18yJbNyT1eZOGV5fGob-lZ3p3kYttXhb7qipKzHf_XR_qCjKZ</recordid><startdate>20151022</startdate><enddate>20151022</enddate><creator>FRENCH FRANKLIN BERNARD</creator><creator>LONG DANIEL THOMAS</creator><creator>COLE DAVID WILLIAM</creator><scope>EVB</scope></search><sort><creationdate>20151022</creationdate><title>AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY</title><author>FRENCH FRANKLIN BERNARD ; LONG DANIEL THOMAS ; COLE DAVID WILLIAM</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2015298825A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>MACHINE TOOLS</topic><topic>MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS</topic><topic>METAL-WORKING NOT OTHERWISE PROVIDED FOR</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>FRENCH FRANKLIN BERNARD</creatorcontrib><creatorcontrib>LONG DANIEL THOMAS</creatorcontrib><creatorcontrib>COLE DAVID WILLIAM</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FRENCH FRANKLIN BERNARD</au><au>LONG DANIEL THOMAS</au><au>COLE DAVID WILLIAM</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY</title><date>2015-10-22</date><risdate>2015</risdate><abstract>An automated apparatus for use in selectively installing temporary fasteners in an assembly is provided. The apparatus includes an end effector, a cutting mechanism coupled to the end effector and that forms an opening in the assembly when a potential opening location is substantially aligned with a cutting mechanism center point. The apparatus also includes at least one of a first sub-assembly and a second sub-assembly coupled to the end effector. The first sub-assembly includes a temporary fastener insertion mechanism that inserts a temporary fastener through the opening in the assembly when the opening is substantially aligned with an insertion mechanism center point different from the cutting mechanism center point. The second sub-assembly includes a temporary fastener removal mechanism that removes installed temporary fasteners from the assembly when the installed temporary fastener is substantially aligned with a removal mechanism center point different from the cutting mechanism center point.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_US2015298825A1 |
source | esp@cenet |
subjects | AIRCRAFT AVIATION COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOTDIRECTED TO A PARTICULAR RESULT COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g.ARRANGEMENTS FOR COPYING OR CONTROLLING GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MACHINE TOOLS MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OFPARTICULAR DETAILS OR COMPONENTS METAL-WORKING NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS TRANSPORTING |
title | AUTOMATED APPARATUS FOR USE IN SELECTIVELY INSTALLING TEMPORARY FASTENERS IN AN ASSEMBLY |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T18%3A46%3A32IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=FRENCH%20FRANKLIN%20BERNARD&rft.date=2015-10-22&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2015298825A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |