An auxiliary power unit with integrated fire detection system
The present invention refers to an Auxiliary Power Unit (APU) for an aircraft with reduced weight, but which at the same time meets all fire-related airworthiness standards. The auxiliary power unit (5) of the invention, comprises a metallic housing (21) having mounts (2) for attaching the housing (...
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creator | FERNANDEZ LOPEZ PIO CASADO MONTERO CARLOS ZAMARRO MARTIN MARIA CRUZ |
description | The present invention refers to an Auxiliary Power Unit (APU) for an aircraft with reduced weight, but which at the same time meets all fire-related airworthiness standards. The auxiliary power unit (5) of the invention, comprises a metallic housing (21) having mounts (2) for attaching the housing (21) to an external structure, wherein the auxiliary power unit (5) further comprises at least one temperature sensor (3) suitable for detecting temperature under fire conditions, wherein said temperature sensor (3) is coupled with said mounts (2) for sensing temperature at the housing (21). |
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The auxiliary power unit (5) of the invention, comprises a metallic housing (21) having mounts (2) for attaching the housing (21) to an external structure, wherein the auxiliary power unit (5) further comprises at least one temperature sensor (3) suitable for detecting temperature under fire conditions, wherein said temperature sensor (3) is coupled with said mounts (2) for sensing temperature at the housing (21).</description><language>eng</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>2015</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=20150701&DB=EPODOC&CC=CN&NR=104743127A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150701&DB=EPODOC&CC=CN&NR=104743127A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FERNANDEZ LOPEZ PIO</creatorcontrib><creatorcontrib>CASADO MONTERO CARLOS</creatorcontrib><creatorcontrib>ZAMARRO MARTIN MARIA CRUZ</creatorcontrib><title>An auxiliary power unit with integrated fire detection system</title><description>The present invention refers to an Auxiliary Power Unit (APU) for an aircraft with reduced weight, but which at the same time meets all fire-related airworthiness standards. The auxiliary power unit (5) of the invention, comprises a metallic housing (21) having mounts (2) for attaching the housing (21) to an external structure, wherein the auxiliary power unit (5) further comprises at least one temperature sensor (3) suitable for detecting temperature under fire conditions, wherein said temperature sensor (3) is coupled with said mounts (2) for sensing temperature at the housing (21).</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB1zFNILK3IzMlMLKpUKMgvTy1SKM3LLFEozyzJUMjMK0lNL0osSU1RSMssSlVISS1JTS7JzM9TKK4sLknN5WFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8c5-hgYm5ibGhkbmjsbEqAEAQZowfw</recordid><startdate>20150701</startdate><enddate>20150701</enddate><creator>FERNANDEZ LOPEZ PIO</creator><creator>CASADO MONTERO CARLOS</creator><creator>ZAMARRO MARTIN MARIA CRUZ</creator><scope>EVB</scope></search><sort><creationdate>20150701</creationdate><title>An auxiliary power unit with integrated fire detection system</title><author>FERNANDEZ LOPEZ PIO ; CASADO MONTERO CARLOS ; ZAMARRO MARTIN MARIA CRUZ</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN104743127A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</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>FERNANDEZ LOPEZ PIO</creatorcontrib><creatorcontrib>CASADO MONTERO CARLOS</creatorcontrib><creatorcontrib>ZAMARRO MARTIN MARIA CRUZ</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FERNANDEZ LOPEZ PIO</au><au>CASADO MONTERO CARLOS</au><au>ZAMARRO MARTIN MARIA CRUZ</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>An auxiliary power unit with integrated fire detection system</title><date>2015-07-01</date><risdate>2015</risdate><abstract>The present invention refers to an Auxiliary Power Unit (APU) for an aircraft with reduced weight, but which at the same time meets all fire-related airworthiness standards. The auxiliary power unit (5) of the invention, comprises a metallic housing (21) having mounts (2) for attaching the housing (21) to an external structure, wherein the auxiliary power unit (5) further comprises at least one temperature sensor (3) suitable for detecting temperature under fire conditions, wherein said temperature sensor (3) is coupled with said mounts (2) for sensing temperature at the housing (21).</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 | An auxiliary power unit with integrated fire detection system |
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