Reinforced holes

A hole in an aircraft panel (e.g. wing cover access hole) is reinforced against fatigue by bonding a frustoconical reinforcement member 20 to the panel 10 using an adhesive 70. These are compressed together using an assembly comprising a compression member 40, a resilient rubber washer 50, a support...

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1. Verfasser:	Enzo Cosentino
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS 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
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creator	Enzo Cosentino
description	A hole in an aircraft panel (e.g. wing cover access hole) is reinforced against fatigue by bonding a frustoconical reinforcement member 20 to the panel 10 using an adhesive 70. These are compressed together using an assembly comprising a compression member 40, a resilient rubber washer 50, a support plate 30, and a clamping bolt 62. The compression member 40 has a frustoconical wall portion of complementary shape to the reinforcement member. The support plate 30 can have a heater for curing the adhesive used to bond the annular reinforcement member to the panel, and a protrusion (38, fig 2c) to help centre the reinforcement member 20 during assembly. The panel 10 and reinforcement member 20 can be metal (e.g. aluminium), composite, wood or plastic.
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These are compressed together using an assembly comprising a compression member 40, a resilient rubber washer 50, a support plate 30, and a clamping bolt 62. The compression member 40 has a frustoconical wall portion of complementary shape to the reinforcement member. The support plate 30 can have a heater for curing the adhesive used to bond the annular reinforcement member to the panel, and a protrusion (38, fig 2c) to help centre the reinforcement member 20 during assembly. The panel 10 and reinforcement member 20 can be metal (e.g. aluminium), composite, wood or plastic.</description><language>eng</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; 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=20220831&DB=EPODOC&CC=GB&NR=2604126A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220831&DB=EPODOC&CC=GB&NR=2604126A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Enzo Cosentino</creatorcontrib><title>Reinforced holes</title><description>A hole in an aircraft panel (e.g. wing cover access hole) is reinforced against fatigue by bonding a frustoconical reinforcement member 20 to the panel 10 using an adhesive 70. These are compressed together using an assembly comprising a compression member 40, a resilient rubber washer 50, a support plate 30, and a clamping bolt 62. The compression member 40 has a frustoconical wall portion of complementary shape to the reinforcement member. The support plate 30 can have a heater for curing the adhesive used to bond the annular reinforcement member to the panel, and a protrusion (38, fig 2c) to help centre the reinforcement member 20 during assembly. The panel 10 and reinforcement member 20 can be metal (e.g. aluminium), composite, wood or plastic.</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</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>eNrjZBAISs3MS8svSk5NUcjIz0kt5mFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8e5ORmYGJoZGZo7GhFUAAC8KHkk</recordid><startdate>20220831</startdate><enddate>20220831</enddate><creator>Enzo Cosentino</creator><scope>EVB</scope></search><sort><creationdate>20220831</creationdate><title>Reinforced holes</title><author>Enzo Cosentino</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2604126A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2022</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>Enzo Cosentino</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Enzo Cosentino</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Reinforced holes</title><date>2022-08-31</date><risdate>2022</risdate><abstract>A hole in an aircraft panel (e.g. wing cover access hole) is reinforced against fatigue by bonding a frustoconical reinforcement member 20 to the panel 10 using an adhesive 70. These are compressed together using an assembly comprising a compression member 40, a resilient rubber washer 50, a support plate 30, and a clamping bolt 62. The compression member 40 has a frustoconical wall portion of complementary shape to the reinforcement member. The support plate 30 can have a heater for curing the adhesive used to bond the annular reinforcement member to the panel, and a protrusion (38, fig 2c) to help centre the reinforcement member 20 during assembly. The panel 10 and reinforcement member 20 can be metal (e.g. aluminium), composite, wood or plastic.</abstract><oa>free_for_read</oa></addata></record>
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language	eng
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subjects	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS 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	Reinforced holes
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