METHOD AND APPARATUS FOR COVERING A FASTENER SYSTEM

체결요소 시스템을 덮는 방법 및 장치에 관한 것이다. 하나의 예시적인 실시 예에서, 장치는 커버(100)를 포함한다. 커버(100)는 체결요소 시스템(102)이 장착되는 대상물(103)의 표면(101)에서 체결요소 시스템(102) 위에 배치되게 구성되어 있다. 커버(100)는, 커버(100)가 커버(100) 바깥 주변 환경(114)에, 체결요소 시스템(102) 주위에서 일러나는, 전기적 방전의 효과를 감소시키도록 구성되게 선택된 다수의 복합재료로 구성되어 있다. A method and apparatus for covering a f...

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Hauptverfasser: ILSOP YOON STEVEN, PATE KEVIN DARRELL, EICHINGER JEFFREY D
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creator ILSOP YOON STEVEN
PATE KEVIN DARRELL
EICHINGER JEFFREY D
description 체결요소 시스템을 덮는 방법 및 장치에 관한 것이다. 하나의 예시적인 실시 예에서, 장치는 커버(100)를 포함한다. 커버(100)는 체결요소 시스템(102)이 장착되는 대상물(103)의 표면(101)에서 체결요소 시스템(102) 위에 배치되게 구성되어 있다. 커버(100)는, 커버(100)가 커버(100) 바깥 주변 환경(114)에, 체결요소 시스템(102) 주위에서 일러나는, 전기적 방전의 효과를 감소시키도록 구성되게 선택된 다수의 복합재료로 구성되어 있다. A method and apparatus for covering a fastener system. In one illustrative embodiment, an apparatus comprises a cover. The cover is configured to be placed over a fastener system at a surface of an object in which the fastener system is installed. The cover is comprised of a number of composite materials selected such that the cover is configured to reduce an effect of an electrical discharge, which occurs around the fastener system, on an environment outside the cover.
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A method and apparatus for covering a fastener system. In one illustrative embodiment, an apparatus comprises a cover. The cover is configured to be placed over a fastener system at a surface of an object in which the fastener system is installed. The cover is comprised of a number of composite materials selected such that the cover is configured to reduce an effect of an electrical discharge, which occurs around the fastener system, on an environment outside the cover.</description><language>eng ; kor</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</subject><creationdate>2020</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&amp;date=20200903&amp;DB=EPODOC&amp;CC=KR&amp;NR=20200104420A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20200903&amp;DB=EPODOC&amp;CC=KR&amp;NR=20200104420A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ILSOP YOON STEVEN</creatorcontrib><creatorcontrib>PATE KEVIN DARRELL</creatorcontrib><creatorcontrib>EICHINGER JEFFREY D</creatorcontrib><title>METHOD AND APPARATUS FOR COVERING A FASTENER SYSTEM</title><description>체결요소 시스템을 덮는 방법 및 장치에 관한 것이다. 하나의 예시적인 실시 예에서, 장치는 커버(100)를 포함한다. 커버(100)는 체결요소 시스템(102)이 장착되는 대상물(103)의 표면(101)에서 체결요소 시스템(102) 위에 배치되게 구성되어 있다. 커버(100)는, 커버(100)가 커버(100) 바깥 주변 환경(114)에, 체결요소 시스템(102) 주위에서 일러나는, 전기적 방전의 효과를 감소시키도록 구성되게 선택된 다수의 복합재료로 구성되어 있다. A method and apparatus for covering a fastener system. In one illustrative embodiment, an apparatus comprises a cover. The cover is configured to be placed over a fastener system at a surface of an object in which the fastener system is installed. 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A method and apparatus for covering a fastener system. In one illustrative embodiment, an apparatus comprises a cover. The cover is configured to be placed over a fastener system at a surface of an object in which the fastener system is installed. The cover is comprised of a number of composite materials selected such that the cover is configured to reduce an effect of an electrical discharge, which occurs around the fastener system, on an environment outside the cover.</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
BLASTING
COSMONAUTICS
DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS ORMACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS,CLIPS, WEDGES, JOINTS OR JOINTING
ENGINEERING ELEMENTS AND UNITS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
THERMAL INSULATION IN GENERAL
TRANSPORTING
WEAPONS
title METHOD AND APPARATUS FOR COVERING A FASTENER SYSTEM
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