Load bearing window
A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are fo...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| 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 | SALMON JAMES J.,MCKEE SCOT |
| description | A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors (22) to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin (14) of the aircraft. The connector fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN1968851A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN1968851A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN1968851A3</originalsourceid><addsrcrecordid>eNrjZBD2yU9MUUhKTSzKzEtXKM_MS8kv52FgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c5-hpZmFhamho7GhFUAAJW6H3I</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Load bearing window</title><source>esp@cenet</source><creator>SALMON JAMES J.,MCKEE SCOT</creator><creatorcontrib>SALMON JAMES J.,MCKEE SCOT</creatorcontrib><description>A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors (22) to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin (14) of the aircraft. The connector fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.</description><language>eng</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; VEHICLES IN GENERAL ; WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2007</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=20070523&DB=EPODOC&CC=CN&NR=1968851A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20070523&DB=EPODOC&CC=CN&NR=1968851A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SALMON JAMES J.,MCKEE SCOT</creatorcontrib><title>Load bearing window</title><description>A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors (22) to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin (14) of the aircraft. The connector fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.</description><subject>AEROPLANES</subject><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>VEHICLES IN GENERAL</subject><subject>WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2007</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBD2yU9MUUhKTSzKzEtXKM_MS8kv52FgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c5-hpZmFhamho7GhFUAAJW6H3I</recordid><startdate>20070523</startdate><enddate>20070523</enddate><creator>SALMON JAMES J.,MCKEE SCOT</creator><scope>EVB</scope></search><sort><creationdate>20070523</creationdate><title>Load bearing window</title><author>SALMON JAMES J.,MCKEE SCOT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN1968851A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2007</creationdate><topic>AEROPLANES</topic><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>VEHICLES IN GENERAL</topic><topic>WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>SALMON JAMES J.,MCKEE SCOT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SALMON JAMES J.,MCKEE SCOT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Load bearing window</title><date>2007-05-23</date><risdate>2007</risdate><abstract>A substantially strong, lightweight load bearing window for use in a mobile platform, for example, an aircraft. The window includes a rim portion (18) having a carbon reinforced resin structure and a transparent portion (20) having a fiberglass reinforced resin structure. A plurality of holes are formed in the rim portion for enabling a plurality of connectors (22) to be inserted therethrough. The rim portion has a smaller cross sectional area (i.e., thickness) than the transparent portion such that the rim portion is adapted to fit behind a skin (14) of the aircraft. The connector fix the window to the skin of the aircraft. The window effectively forms a strong, structurally integral portion of the skin.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_CN1968851A |
| source | esp@cenet |
| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FORVEHICLES SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING VEHICLES IN GENERAL WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILARDEVICES FOR VEHICLES WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | Load bearing window |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-11T09%3A28%3A21IST&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=SALMON%20JAMES%20J.,MCKEE%20SCOT&rft.date=2007-05-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN1968851A%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 |