ROTORCRAFT FUEL SYSTEM HAVING ENHANCED CRASH RESISTANCE
A rotorcraft (10) includes a fuselage (16) having a fuel tank receiving assembly (24) with a fuel tank (28) positioned therein. The fuel tank (28) including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank (28) forming a res...
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| creator | PERYEA, Martin EMRICH, Joshua SMITH, Michael Reaugh HAMELWRIGHT Jr., Douglas BRAND, Albert G CARR, Timothy PLAGIANOS, Nicholas J |
| description | A rotorcraft (10) includes a fuselage (16) having a fuel tank receiving assembly (24) with a fuel tank (28) positioned therein. The fuel tank (28) including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank (28) forming a restraint assembly (130; 172; 182; 202). The network of straps includes at least one perimeter strap (132, 134, 136, 138, 140) extending at least partially about at least two fuel bags and at least one surrounding strap (142, 144, 146) extending at least partially about the at least two fuel bags. The at least one perimeter strap (132, 134, 136, 138, 140) has at least two intersections (156, 158) with the at least one surrounding strap (142, 144, 146). |
| format | Patent |
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The fuel tank (28) including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank (28) forming a restraint assembly (130; 172; 182; 202). The network of straps includes at least one perimeter strap (132, 134, 136, 138, 140) extending at least partially about at least two fuel bags and at least one surrounding strap (142, 144, 146) extending at least partially about the at least two fuel bags. The at least one perimeter strap (132, 134, 136, 138, 140) has at least two intersections (156, 158) with the at least one surrounding strap (142, 144, 146).</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>2017</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=20171108&DB=EPODOC&CC=EP&NR=3241756A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20171108&DB=EPODOC&CC=EP&NR=3241756A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PERYEA, Martin</creatorcontrib><creatorcontrib>EMRICH, Joshua</creatorcontrib><creatorcontrib>SMITH, Michael Reaugh</creatorcontrib><creatorcontrib>HAMELWRIGHT Jr., Douglas</creatorcontrib><creatorcontrib>BRAND, Albert G</creatorcontrib><creatorcontrib>CARR, Timothy</creatorcontrib><creatorcontrib>PLAGIANOS, Nicholas J</creatorcontrib><title>ROTORCRAFT FUEL SYSTEM HAVING ENHANCED CRASH RESISTANCE</title><description>A rotorcraft (10) includes a fuselage (16) having a fuel tank receiving assembly (24) with a fuel tank (28) positioned therein. The fuel tank (28) including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank (28) forming a restraint assembly (130; 172; 182; 202). The network of straps includes at least one perimeter strap (132, 134, 136, 138, 140) extending at least partially about at least two fuel bags and at least one surrounding strap (142, 144, 146) extending at least partially about the at least two fuel bags. The at least one perimeter strap (132, 134, 136, 138, 140) has at least two intersections (156, 158) with the at least one surrounding strap (142, 144, 146).</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>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAP8g_xD3IOcnQLUXALdfVRCI4MDnH1VfBwDPP0c1dw9fNw9HN2dVEAqgj2UAhyDfYMDgGJ8DCwpiXmFKfyQmluBgU31xBnD93Ugvz41OKCxOTUvNSSeNcAYyMTQ3NTM0dDYyKUAAD_7Sfq</recordid><startdate>20171108</startdate><enddate>20171108</enddate><creator>PERYEA, Martin</creator><creator>EMRICH, Joshua</creator><creator>SMITH, Michael Reaugh</creator><creator>HAMELWRIGHT Jr., Douglas</creator><creator>BRAND, Albert G</creator><creator>CARR, Timothy</creator><creator>PLAGIANOS, Nicholas J</creator><scope>EVB</scope></search><sort><creationdate>20171108</creationdate><title>ROTORCRAFT FUEL SYSTEM HAVING ENHANCED CRASH RESISTANCE</title><author>PERYEA, Martin ; EMRICH, Joshua ; SMITH, Michael Reaugh ; HAMELWRIGHT Jr., Douglas ; BRAND, Albert G ; CARR, Timothy ; PLAGIANOS, Nicholas J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3241756A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2017</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>PERYEA, Martin</creatorcontrib><creatorcontrib>EMRICH, Joshua</creatorcontrib><creatorcontrib>SMITH, Michael Reaugh</creatorcontrib><creatorcontrib>HAMELWRIGHT Jr., Douglas</creatorcontrib><creatorcontrib>BRAND, Albert G</creatorcontrib><creatorcontrib>CARR, Timothy</creatorcontrib><creatorcontrib>PLAGIANOS, Nicholas J</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PERYEA, Martin</au><au>EMRICH, Joshua</au><au>SMITH, Michael Reaugh</au><au>HAMELWRIGHT Jr., Douglas</au><au>BRAND, Albert G</au><au>CARR, Timothy</au><au>PLAGIANOS, Nicholas J</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ROTORCRAFT FUEL SYSTEM HAVING ENHANCED CRASH RESISTANCE</title><date>2017-11-08</date><risdate>2017</risdate><abstract>A rotorcraft (10) includes a fuselage (16) having a fuel tank receiving assembly (24) with a fuel tank (28) positioned therein. The fuel tank (28) including a plurality of interconnected fuel bags operable to contain liquid fuel. A network of straps is disposed about the fuel tank (28) forming a restraint assembly (130; 172; 182; 202). The network of straps includes at least one perimeter strap (132, 134, 136, 138, 140) extending at least partially about at least two fuel bags and at least one surrounding strap (142, 144, 146) extending at least partially about the at least two fuel bags. The at least one perimeter strap (132, 134, 136, 138, 140) has at least two intersections (156, 158) with the at least one surrounding strap (142, 144, 146).</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 | ROTORCRAFT FUEL SYSTEM HAVING ENHANCED CRASH RESISTANCE |
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