Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework
A transverse framework for an avionics bay of an aircraft is delimited by a primary structure and a floor, the transverse framework having a mesh structure with square and/or rectangular mesh cells. According to one arrangement, an avionics bay of an aircraft includes two longitudinal rows of avioni...
Gespeichert in:
| Hauptverfasser: | , |
|---|---|
| Format: | Patent |
| 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 | Saint-Marc, Laurent Guering, Bernard |
| description | A transverse framework for an avionics bay of an aircraft is delimited by a primary structure and a floor, the transverse framework having a mesh structure with square and/or rectangular mesh cells. According to one arrangement, an avionics bay of an aircraft includes two longitudinal rows of avionics racks, parallel to the longitudinal direction and arranged on each side of a clear zone, and a transverse avionics rack supported by the transverse framework situated to the rear of the two longitudinal rows of avionics racks at the rear boundary of the avionics bay. This transverse framework makes it possible to optimize the space occupied by the avionics bay. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2019389596A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2019389596A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2019389596A13</originalsourceid><addsrcrecordid>eNqNjTEKwkAQRdNYiHqHAVsFY1BMuQaDFmKRWIc1O9HFZDbMxEhO4LUVESsLqwf_fXh975GyJmmRBSFmXeHd8RV21CAZNBA7BkWgWuvI5gJr3cGheE-Wc9ZFMwElgtWp7GDvzK3ElzRfC5GrarZi6QzpBSHR1sCv5NDrFboUHH048MbxJo22U6xdhlLrHAmb7JjMZ34YrMJFuFR-8N_rCYkJSzc</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework</title><source>esp@cenet</source><creator>Saint-Marc, Laurent ; Guering, Bernard</creator><creatorcontrib>Saint-Marc, Laurent ; Guering, Bernard</creatorcontrib><description>A transverse framework for an avionics bay of an aircraft is delimited by a primary structure and a floor, the transverse framework having a mesh structure with square and/or rectangular mesh cells. According to one arrangement, an avionics bay of an aircraft includes two longitudinal rows of avionics racks, parallel to the longitudinal direction and arranged on each side of a clear zone, and a transverse avionics rack supported by the transverse framework situated to the rear of the two longitudinal rows of avionics racks at the rear boundary of the avionics bay. This transverse framework makes it possible to optimize the space occupied by the avionics bay.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ; COSMONAUTICS ; ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS ; PARACHUTES ; PERFORMING OPERATIONS ; PRINTED CIRCUITS ; TRANSPORTING</subject><creationdate>2019</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=20191226&DB=EPODOC&CC=US&NR=2019389596A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191226&DB=EPODOC&CC=US&NR=2019389596A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Saint-Marc, Laurent</creatorcontrib><creatorcontrib>Guering, Bernard</creatorcontrib><title>Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework</title><description>A transverse framework for an avionics bay of an aircraft is delimited by a primary structure and a floor, the transverse framework having a mesh structure with square and/or rectangular mesh cells. According to one arrangement, an avionics bay of an aircraft includes two longitudinal rows of avionics racks, parallel to the longitudinal direction and arranged on each side of a clear zone, and a transverse avionics rack supported by the transverse framework situated to the rear of the two longitudinal rows of avionics racks at the rear boundary of the avionics bay. This transverse framework makes it possible to optimize the space occupied by the avionics bay.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</subject><subject>COSMONAUTICS</subject><subject>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HELICOPTERS</subject><subject>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>PRINTED CIRCUITS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjTEKwkAQRdNYiHqHAVsFY1BMuQaDFmKRWIc1O9HFZDbMxEhO4LUVESsLqwf_fXh975GyJmmRBSFmXeHd8RV21CAZNBA7BkWgWuvI5gJr3cGheE-Wc9ZFMwElgtWp7GDvzK3ElzRfC5GrarZi6QzpBSHR1sCv5NDrFboUHH048MbxJo22U6xdhlLrHAmb7JjMZ34YrMJFuFR-8N_rCYkJSzc</recordid><startdate>20191226</startdate><enddate>20191226</enddate><creator>Saint-Marc, Laurent</creator><creator>Guering, Bernard</creator><scope>EVB</scope></search><sort><creationdate>20191226</creationdate><title>Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework</title><author>Saint-Marc, Laurent ; Guering, Bernard</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2019389596A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS</topic><topic>COSMONAUTICS</topic><topic>ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR</topic><topic>ELECTRICITY</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HELICOPTERS</topic><topic>MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PRINTED CIRCUITS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Saint-Marc, Laurent</creatorcontrib><creatorcontrib>Guering, Bernard</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Saint-Marc, Laurent</au><au>Guering, Bernard</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework</title><date>2019-12-26</date><risdate>2019</risdate><abstract>A transverse framework for an avionics bay of an aircraft is delimited by a primary structure and a floor, the transverse framework having a mesh structure with square and/or rectangular mesh cells. According to one arrangement, an avionics bay of an aircraft includes two longitudinal rows of avionics racks, parallel to the longitudinal direction and arranged on each side of a clear zone, and a transverse avionics rack supported by the transverse framework situated to the rear of the two longitudinal rows of avionics racks at the rear boundary of the avionics bay. This transverse framework makes it possible to optimize the space occupied by the avionics bay.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_US2019389596A1 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS PARACHUTES PERFORMING OPERATIONS PRINTED CIRCUITS TRANSPORTING |
| title | Transverse Framework Intended For An Avionics Bay Of An Aircraft, Assembly Module And Aircraft Comprising The Said Transverse Framework |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T14%3A47%3A18IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Saint-Marc,%20Laurent&rft.date=2019-12-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2019389596A1%3C/epo_EVB%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 |