METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE
To provide a current return network assembly for an aircraft, the assembly being attached into a predetermined potential lightning strike zone.SOLUTION: The current return network assembly includes a central core 102, a left side support flange 104, and a right side support flange 106. The left side...
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| creator | GREGORY A FOLTZ ARTHUR C DAY PAUL S GREGG KIRK B KAJITA MARC J PIEHL |
| description | To provide a current return network assembly for an aircraft, the assembly being attached into a predetermined potential lightning strike zone.SOLUTION: The current return network assembly includes a central core 102, a left side support flange 104, and a right side support flange 106. The left side support flange 104 is angled inwardly from right to left, while the right side support flange 106 is angled inwardly from right to left. The central core 102 comprises a central honeycomb core section 108 which comprises hollow hexagonal interconnected structural unitary tubes. The honeycomb core section 108 is transversely positioned relative to laterally opposed sides 110 that form a load-bearing structure for the central core 102.SELECTED DRAWING: Figure 3A
【課題】所定の潜在的落雷ゾーン内に取り付けられる、航空機用の電流リターンネットワークアセンブリを提供する。【解決手段】電流リターンネットワークアセンブリは、中央コア部１０２と、左側支持フランジ１０４と、右側支持フランジ１０６を含む。左側支持フランジ１０４は右から左に内向きに角度が付けられており、同時に、右側支持フランジ１０６は右から左に内向きに角度が付けられている。中央コア１０２は、中空六角形状の相互連結された構造の一体管から構成される中央ハニカムコア部１０８を備える。ハニカムコア部１０８は、中央コア１０２に対して耐荷重構造をなして横方向に対向する側面１１０に対し、横断方向に位置する。【選択図】図３Ａ |
| format | Patent |
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【課題】所定の潜在的落雷ゾーン内に取り付けられる、航空機用の電流リターンネットワークアセンブリを提供する。【解決手段】電流リターンネットワークアセンブリは、中央コア部１０２と、左側支持フランジ１０４と、右側支持フランジ１０６を含む。左側支持フランジ１０４は右から左に内向きに角度が付けられており、同時に、右側支持フランジ１０６は右から左に内向きに角度が付けられている。中央コア１０２は、中空六角形状の相互連結された構造の一体管から構成される中央ハニカムコア部１０８を備える。ハニカムコア部１０８は、中央コア１０２に対して耐荷重構造をなして横方向に対向する側面１１０に対し、横断方向に位置する。【選択図】図３Ａ</description><language>eng ; jpn</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=20181213&DB=EPODOC&CC=JP&NR=2018197110A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181213&DB=EPODOC&CC=JP&NR=2018197110A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GREGORY A FOLTZ</creatorcontrib><creatorcontrib>ARTHUR C DAY</creatorcontrib><creatorcontrib>PAUL S GREGG</creatorcontrib><creatorcontrib>KIRK B KAJITA</creatorcontrib><creatorcontrib>MARC J PIEHL</creatorcontrib><title>METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE</title><description>To provide a current return network assembly for an aircraft, the assembly being attached into a predetermined potential lightning strike zone.SOLUTION: The current return network assembly includes a central core 102, a left side support flange 104, and a right side support flange 106. The left side support flange 104 is angled inwardly from right to left, while the right side support flange 106 is angled inwardly from right to left. The central core 102 comprises a central honeycomb core section 108 which comprises hollow hexagonal interconnected structural unitary tubes. The honeycomb core section 108 is transversely positioned relative to laterally opposed sides 110 that form a load-bearing structure for the central core 102.SELECTED DRAWING: Figure 3A
【課題】所定の潜在的落雷ゾーン内に取り付けられる、航空機用の電流リターンネットワークアセンブリを提供する。【解決手段】電流リターンネットワークアセンブリは、中央コア部１０２と、左側支持フランジ１０４と、右側支持フランジ１０６を含む。左側支持フランジ１０４は右から左に内向きに角度が付けられており、同時に、右側支持フランジ１０６は右から左に内向きに角度が付けられている。中央コア１０２は、中空六角形状の相互連結された構造の一体管から構成される中央ハニカムコア部１０８を備える。ハニカムコア部１０８は、中央コア１０２に対して耐荷重構造をなして横方向に対向する側面１１０に対し、横断方向に位置する。【選択図】図３Ａ</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>eNqNirEKwjAQQLs4iPoPh7vQ6KAdj_Rio3gJ14uOpUicRAv1_7GDH-DweMN78yJcSJtQA_JEjCioqQUXBKKEq689H8EmEWIFIU3CwKS3IGfwDOjFCjqFViXZqdKymD3655hXPy-KtSO1zSYP7y6PQ3_Pr_zpTnFbmoOp9saUuPtr-gLQ5C-l</recordid><startdate>20181213</startdate><enddate>20181213</enddate><creator>GREGORY A FOLTZ</creator><creator>ARTHUR C DAY</creator><creator>PAUL S GREGG</creator><creator>KIRK B KAJITA</creator><creator>MARC J PIEHL</creator><scope>EVB</scope></search><sort><creationdate>20181213</creationdate><title>METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE</title><author>GREGORY A FOLTZ ; ARTHUR C DAY ; PAUL S GREGG ; KIRK B KAJITA ; MARC J PIEHL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2018197110A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</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>GREGORY A FOLTZ</creatorcontrib><creatorcontrib>ARTHUR C DAY</creatorcontrib><creatorcontrib>PAUL S GREGG</creatorcontrib><creatorcontrib>KIRK B KAJITA</creatorcontrib><creatorcontrib>MARC J PIEHL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GREGORY A FOLTZ</au><au>ARTHUR C DAY</au><au>PAUL S GREGG</au><au>KIRK B KAJITA</au><au>MARC J PIEHL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE</title><date>2018-12-13</date><risdate>2018</risdate><abstract>To provide a current return network assembly for an aircraft, the assembly being attached into a predetermined potential lightning strike zone.SOLUTION: The current return network assembly includes a central core 102, a left side support flange 104, and a right side support flange 106. The left side support flange 104 is angled inwardly from right to left, while the right side support flange 106 is angled inwardly from right to left. The central core 102 comprises a central honeycomb core section 108 which comprises hollow hexagonal interconnected structural unitary tubes. The honeycomb core section 108 is transversely positioned relative to laterally opposed sides 110 that form a load-bearing structure for the central core 102.SELECTED DRAWING: Figure 3A
【課題】所定の潜在的落雷ゾーン内に取り付けられる、航空機用の電流リターンネットワークアセンブリを提供する。【解決手段】電流リターンネットワークアセンブリは、中央コア部１０２と、左側支持フランジ１０４と、右側支持フランジ１０６を含む。左側支持フランジ１０４は右から左に内向きに角度が付けられており、同時に、右側支持フランジ１０６は右から左に内向きに角度が付けられている。中央コア１０２は、中空六角形状の相互連結された構造の一体管から構成される中央ハニカムコア部１０８を備える。ハニカムコア部１０８は、中央コア１０２に対して耐荷重構造をなして横方向に対向する側面１１０に対し、横断方向に位置する。【選択図】図３Ａ</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 | METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE |
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