The Lightning Spark Barrier
Lightning protection of modern aerospace vehicles must prohibit sparking in critical fuel vapor areas. In the past, it has been particularly difficult to keep mechanical fasteners from sparking during a lightning event. Attempts to seal off the fasteners from the critical fuel vapor area by manual a...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Report |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | Amason, M P Hofmeister, M C |
description | Lightning protection of modern aerospace vehicles must prohibit sparking in critical fuel vapor areas. In the past, it has been particularly difficult to keep mechanical fasteners from sparking during a lightning event. Attempts to seal off the fasteners from the critical fuel vapor area by manual application of sealant material have proven to be ineffective due to gaps and voids produced by the application process. A technique was developed by Douglas Aircraft Company to control the application of dielectric sealant material to isolate the mechanical fastener sparking from the critical fuel vapor area. The technique consists of a specially designed dielectric cap that fits over the fastener, providing uniform and controlled application of dielectric filler material. An adequate thickness of filler material provides a barrier that prevents the sparks from entering the critical fuel vapor area. The Lightning Spark Barrier is applicable to a wide variety of installations, including those with composite materials. A patent has been applied for. (Author)
This article is from 'International Aerospace and Ground Conference on Lightning and Static Electricity (8th): 'Lightning Technology Roundup,' held at Fort Worth, Texas on 21-23 June 1983,' ADA135100, p96-1 thru 96-3. |
format | Report |
fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADP002240</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADP002240</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADP0022403</originalsourceid><addsrcrecordid>eNrjZJAOyUhV8MlMzyjJy8xLVwguSCzKVnBKLCrKTC3iYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4uAQYGRkYmBsYEpAHuKSAZ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>The Lightning Spark Barrier</title><source>DTIC Technical Reports</source><creator>Amason, M P ; Hofmeister, M C</creator><creatorcontrib>Amason, M P ; Hofmeister, M C ; DOUGLAS AIRCRAFT CO LONG BEACH CA</creatorcontrib><description>Lightning protection of modern aerospace vehicles must prohibit sparking in critical fuel vapor areas. In the past, it has been particularly difficult to keep mechanical fasteners from sparking during a lightning event. Attempts to seal off the fasteners from the critical fuel vapor area by manual application of sealant material have proven to be ineffective due to gaps and voids produced by the application process. A technique was developed by Douglas Aircraft Company to control the application of dielectric sealant material to isolate the mechanical fastener sparking from the critical fuel vapor area. The technique consists of a specially designed dielectric cap that fits over the fastener, providing uniform and controlled application of dielectric filler material. An adequate thickness of filler material provides a barrier that prevents the sparks from entering the critical fuel vapor area. The Lightning Spark Barrier is applicable to a wide variety of installations, including those with composite materials. A patent has been applied for. (Author)
This article is from 'International Aerospace and Ground Conference on Lightning and Static Electricity (8th): 'Lightning Technology Roundup,' held at Fort Worth, Texas on 21-23 June 1983,' ADA135100, p96-1 thru 96-3.</description><language>eng</language><subject>AIRCRAFT EQUIPMENT ; AVIATION FUELS ; BARRIERS ; CAPS(COVERINGS) ; COMPONENT REPORTS ; DIELECTRICS ; FASTENINGS ; HAZARDS ; LIGHTNING ; Meteorology ; PROTECTIVE COVERINGS ; SPARKS ; SYMPOSIA ; VAPORS</subject><creationdate>1983</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADP002240$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Amason, M P</creatorcontrib><creatorcontrib>Hofmeister, M C</creatorcontrib><creatorcontrib>DOUGLAS AIRCRAFT CO LONG BEACH CA</creatorcontrib><title>The Lightning Spark Barrier</title><description>Lightning protection of modern aerospace vehicles must prohibit sparking in critical fuel vapor areas. In the past, it has been particularly difficult to keep mechanical fasteners from sparking during a lightning event. Attempts to seal off the fasteners from the critical fuel vapor area by manual application of sealant material have proven to be ineffective due to gaps and voids produced by the application process. A technique was developed by Douglas Aircraft Company to control the application of dielectric sealant material to isolate the mechanical fastener sparking from the critical fuel vapor area. The technique consists of a specially designed dielectric cap that fits over the fastener, providing uniform and controlled application of dielectric filler material. An adequate thickness of filler material provides a barrier that prevents the sparks from entering the critical fuel vapor area. The Lightning Spark Barrier is applicable to a wide variety of installations, including those with composite materials. A patent has been applied for. (Author)
This article is from 'International Aerospace and Ground Conference on Lightning and Static Electricity (8th): 'Lightning Technology Roundup,' held at Fort Worth, Texas on 21-23 June 1983,' ADA135100, p96-1 thru 96-3.</description><subject>AIRCRAFT EQUIPMENT</subject><subject>AVIATION FUELS</subject><subject>BARRIERS</subject><subject>CAPS(COVERINGS)</subject><subject>COMPONENT REPORTS</subject><subject>DIELECTRICS</subject><subject>FASTENINGS</subject><subject>HAZARDS</subject><subject>LIGHTNING</subject><subject>Meteorology</subject><subject>PROTECTIVE COVERINGS</subject><subject>SPARKS</subject><subject>SYMPOSIA</subject><subject>VAPORS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1983</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZJAOyUhV8MlMzyjJy8xLVwguSCzKVnBKLCrKTC3iYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4uAQYGRkYmBsYEpAHuKSAZ</recordid><startdate>198301</startdate><enddate>198301</enddate><creator>Amason, M P</creator><creator>Hofmeister, M C</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198301</creationdate><title>The Lightning Spark Barrier</title><author>Amason, M P ; Hofmeister, M C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADP0022403</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1983</creationdate><topic>AIRCRAFT EQUIPMENT</topic><topic>AVIATION FUELS</topic><topic>BARRIERS</topic><topic>CAPS(COVERINGS)</topic><topic>COMPONENT REPORTS</topic><topic>DIELECTRICS</topic><topic>FASTENINGS</topic><topic>HAZARDS</topic><topic>LIGHTNING</topic><topic>Meteorology</topic><topic>PROTECTIVE COVERINGS</topic><topic>SPARKS</topic><topic>SYMPOSIA</topic><topic>VAPORS</topic><toplevel>online_resources</toplevel><creatorcontrib>Amason, M P</creatorcontrib><creatorcontrib>Hofmeister, M C</creatorcontrib><creatorcontrib>DOUGLAS AIRCRAFT CO LONG BEACH CA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Amason, M P</au><au>Hofmeister, M C</au><aucorp>DOUGLAS AIRCRAFT CO LONG BEACH CA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>The Lightning Spark Barrier</btitle><date>1983-01</date><risdate>1983</risdate><abstract>Lightning protection of modern aerospace vehicles must prohibit sparking in critical fuel vapor areas. In the past, it has been particularly difficult to keep mechanical fasteners from sparking during a lightning event. Attempts to seal off the fasteners from the critical fuel vapor area by manual application of sealant material have proven to be ineffective due to gaps and voids produced by the application process. A technique was developed by Douglas Aircraft Company to control the application of dielectric sealant material to isolate the mechanical fastener sparking from the critical fuel vapor area. The technique consists of a specially designed dielectric cap that fits over the fastener, providing uniform and controlled application of dielectric filler material. An adequate thickness of filler material provides a barrier that prevents the sparks from entering the critical fuel vapor area. The Lightning Spark Barrier is applicable to a wide variety of installations, including those with composite materials. A patent has been applied for. (Author)
This article is from 'International Aerospace and Ground Conference on Lightning and Static Electricity (8th): 'Lightning Technology Roundup,' held at Fort Worth, Texas on 21-23 June 1983,' ADA135100, p96-1 thru 96-3.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_dtic_stinet_ADP002240 |
source | DTIC Technical Reports |
subjects | AIRCRAFT EQUIPMENT AVIATION FUELS BARRIERS CAPS(COVERINGS) COMPONENT REPORTS DIELECTRICS FASTENINGS HAZARDS LIGHTNING Meteorology PROTECTIVE COVERINGS SPARKS SYMPOSIA VAPORS |
title | The Lightning Spark Barrier |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-01T23%3A24%3A14IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=The%20Lightning%20Spark%20Barrier&rft.au=Amason,%20M%20P&rft.aucorp=DOUGLAS%20AIRCRAFT%20CO%20LONG%20BEACH%20CA&rft.date=1983-01&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EADP002240%3C/dtic_1RU%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |