AIRPLANE FIRE DETECTION SYSTEM
A fire detection system includes a heat detector controller and a multiplicity of heat detectors. The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Eac...
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| creator | NOE, Darrin M CLOS, William Robert |
| description | A fire detection system includes a heat detector controller and a multiplicity of heat detectors. The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Each of the multiplicity of heat detectors are configured to measure temperature and to transmit temperature measurements to the heat detector controller. The heat detector controller is configured to determine that a fire has breached the cargo compartment liner based on the temperature measurements. |
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The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Each of the multiplicity of heat detectors are configured to measure temperature and to transmit temperature measurements to the heat detector controller. The heat detector controller is configured to determine that a fire has breached the cargo compartment liner based on the temperature measurements.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ALARM SYSTEMS ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; ORDER TELEGRAPHS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; SIGNALLING ; SIGNALLING OR CALLING SYSTEMS ; 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=20181107&DB=EPODOC&CC=EP&NR=3399509A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,782,887,25571,76555</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181107&DB=EPODOC&CC=EP&NR=3399509A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NOE, Darrin M</creatorcontrib><creatorcontrib>CLOS, William Robert</creatorcontrib><title>AIRPLANE FIRE DETECTION SYSTEM</title><description>A fire detection system includes a heat detector controller and a multiplicity of heat detectors. The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Each of the multiplicity of heat detectors are configured to measure temperature and to transmit temperature measurements to the heat detector controller. The heat detector controller is configured to determine that a fire has breached the cargo compartment liner based on the temperature measurements.</description><subject>AIRCRAFT</subject><subject>ALARM SYSTEMS</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>ORDER TELEGRAPHS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>SIGNALLING</subject><subject>SIGNALLING OR CALLING SYSTEMS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBz9AwK8HH0c1Vw8wxyVXBxDXF1DvH091MIjgwOcfXlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGxpaWpgaWjobGRCgBAHX1IQ8</recordid><startdate>20181107</startdate><enddate>20181107</enddate><creator>NOE, Darrin M</creator><creator>CLOS, William Robert</creator><scope>EVB</scope></search><sort><creationdate>20181107</creationdate><title>AIRPLANE FIRE DETECTION SYSTEM</title><author>NOE, Darrin M ; CLOS, William Robert</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3399509A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</creationdate><topic>AIRCRAFT</topic><topic>ALARM SYSTEMS</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>ORDER TELEGRAPHS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>SIGNALLING</topic><topic>SIGNALLING OR CALLING SYSTEMS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>NOE, Darrin M</creatorcontrib><creatorcontrib>CLOS, William Robert</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NOE, Darrin M</au><au>CLOS, William Robert</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRPLANE FIRE DETECTION SYSTEM</title><date>2018-11-07</date><risdate>2018</risdate><abstract>A fire detection system includes a heat detector controller and a multiplicity of heat detectors. The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Each of the multiplicity of heat detectors are configured to measure temperature and to transmit temperature measurements to the heat detector controller. The heat detector controller is configured to determine that a fire has breached the cargo compartment liner based on the temperature measurements.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIRCRAFT ALARM SYSTEMS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS ORDER TELEGRAPHS PARACHUTES PERFORMING OPERATIONS PHYSICS SIGNALLING SIGNALLING OR CALLING SYSTEMS TRANSPORTING |
| title | AIRPLANE FIRE DETECTION SYSTEM |
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