RETENTION SYSTEM FOR GAS CYLINDER OF EVACUATION SYSTEM
A retention unit for securing a charged gas cylinder (102) to a body of an aircraft includes a container (104) having an opening and configured to cover the charged gas cylinder (102). The retention unit also includes a plurality of flaps (106A, 106B) coupled to the container (104) and configured to...
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creator | Schmidt, Ryan Hartman, Drew Larner, William T Flores, Jesus I Baglini Jr., James |
description | A retention unit for securing a charged gas cylinder (102) to a body of an aircraft includes a container (104) having an opening and configured to cover the charged gas cylinder (102). The retention unit also includes a plurality of flaps (106A, 106B) coupled to the container (104) and configured to be attached to the body of the aircraft using a contact adhesive (116). The retention unit also includes a drawstring (112) disposed around the opening of the container (104) and configured to provide a closure of the container (104) around a neck (114) of the charged gas cylinder (102) inside the container (104). |
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The retention unit also includes a plurality of flaps (106A, 106B) coupled to the container (104) and configured to be attached to the body of the aircraft using a contact adhesive (116). The retention unit also includes a drawstring (112) disposed around the opening of the container (104) and configured to provide a closure of the container (104) around a neck (114) of the charged gas cylinder (102) inside the container (104).</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2018</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=20181212&DB=EPODOC&CC=EP&NR=3235733B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181212&DB=EPODOC&CC=EP&NR=3235733B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schmidt, Ryan</creatorcontrib><creatorcontrib>Hartman, Drew</creatorcontrib><creatorcontrib>Larner, William T</creatorcontrib><creatorcontrib>Flores, Jesus I</creatorcontrib><creatorcontrib>Baglini Jr., James</creatorcontrib><title>RETENTION SYSTEM FOR GAS CYLINDER OF EVACUATION SYSTEM</title><description>A retention unit for securing a charged gas cylinder (102) to a body of an aircraft includes a container (104) having an opening and configured to cover the charged gas cylinder (102). The retention unit also includes a plurality of flaps (106A, 106B) coupled to the container (104) and configured to be attached to the body of the aircraft using a contact adhesive (116). The retention unit also includes a drawstring (112) disposed around the opening of the container (104) and configured to provide a closure of the container (104) around a neck (114) of the charged gas cylinder (102) inside the container (104).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDALcg1x9Qvx9PdTCI4MDnH1VXDzD1JwdwxWcI708fRzcQ1S8HdTcA1zdA51RFLFw8CalphTnMoLpbkZFNxcQ5w9dFML8uNTiwsSk1PzUkviXQOMjYxNzY2NnQyNiVACAOD6J70</recordid><startdate>20181212</startdate><enddate>20181212</enddate><creator>Schmidt, Ryan</creator><creator>Hartman, Drew</creator><creator>Larner, William T</creator><creator>Flores, Jesus I</creator><creator>Baglini Jr., James</creator><scope>EVB</scope></search><sort><creationdate>20181212</creationdate><title>RETENTION SYSTEM FOR GAS CYLINDER OF EVACUATION SYSTEM</title><author>Schmidt, Ryan ; Hartman, Drew ; Larner, William T ; Flores, Jesus I ; Baglini Jr., James</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3235733B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Schmidt, Ryan</creatorcontrib><creatorcontrib>Hartman, Drew</creatorcontrib><creatorcontrib>Larner, William T</creatorcontrib><creatorcontrib>Flores, Jesus I</creatorcontrib><creatorcontrib>Baglini Jr., James</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schmidt, Ryan</au><au>Hartman, Drew</au><au>Larner, William T</au><au>Flores, Jesus I</au><au>Baglini Jr., James</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>RETENTION SYSTEM FOR GAS CYLINDER OF EVACUATION SYSTEM</title><date>2018-12-12</date><risdate>2018</risdate><abstract>A retention unit for securing a charged gas cylinder (102) to a body of an aircraft includes a container (104) having an opening and configured to cover the charged gas cylinder (102). The retention unit also includes a plurality of flaps (106A, 106B) coupled to the container (104) and configured to be attached to the body of the aircraft using a contact adhesive (116). The retention unit also includes a drawstring (112) disposed around the opening of the container (104) and configured to provide a closure of the container (104) around a neck (114) of the charged gas cylinder (102) inside the container (104).</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | RETENTION SYSTEM FOR GAS CYLINDER OF EVACUATION SYSTEM |
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