AIRCRAFT WINDOWS AND ASSOCIATED METHODS FOR INSTALLATION
Aircraft windows and associated methods for installation. The windows c an be installed in a passenger cabin of an aircraft and can include a frame tha t supports a pane assembly having a viewing area of at least 180 square inches . The viewing area can have a triangular shape, with the sides of the...
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creator | GIUNTOLI, DOMENIC S CONDON, JOSEPH P RITTS, MICHAEL A WARREN, RYON CHRISTOPHER BLADT, RALPH FRAKER, RICHARD QUAN, WILLIAM MIKULENCAK, PAUL |
description | Aircraft windows and associated methods for installation. The windows c an be installed in a passenger cabin of an aircraft and can include a frame tha t supports a pane assembly having a viewing area of at least 180 square inches . The viewing area can have a triangular shape, with the sides of the wind ow aligned with none of the major axis of the aircraft. Alternatively, the wind ow can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel. |
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The windows c an be installed in a passenger cabin of an aircraft and can include a frame tha t supports a pane assembly having a viewing area of at least 180 square inches . The viewing area can have a triangular shape, with the sides of the wind ow aligned with none of the major axis of the aircraft. Alternatively, the wind ow can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2003</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLBw9AxyDnJ0C1EI9_Rz8Q8PVnD0c1FwDA72d_Z0DHF1UfB1DfHwdwlWcPMPUvD0Cw5x9PFxDPH09-NhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfHOjkYmhibmBgaOhsZEKAEAHPgoAA</recordid><startdate>20031225</startdate><enddate>20031225</enddate><creator>GIUNTOLI, DOMENIC S</creator><creator>CONDON, JOSEPH P</creator><creator>RITTS, MICHAEL A</creator><creator>WARREN, RYON CHRISTOPHER</creator><creator>BLADT, RALPH</creator><creator>FRAKER, RICHARD</creator><creator>QUAN, WILLIAM</creator><creator>MIKULENCAK, PAUL</creator><scope>EVB</scope></search><sort><creationdate>20031225</creationdate><title>AIRCRAFT WINDOWS AND ASSOCIATED METHODS FOR INSTALLATION</title><author>GIUNTOLI, DOMENIC S ; CONDON, JOSEPH P ; RITTS, MICHAEL A ; WARREN, RYON CHRISTOPHER ; BLADT, RALPH ; FRAKER, RICHARD ; QUAN, WILLIAM ; MIKULENCAK, PAUL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2414700A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2003</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>GIUNTOLI, DOMENIC S</creatorcontrib><creatorcontrib>CONDON, JOSEPH P</creatorcontrib><creatorcontrib>RITTS, MICHAEL A</creatorcontrib><creatorcontrib>WARREN, RYON CHRISTOPHER</creatorcontrib><creatorcontrib>BLADT, RALPH</creatorcontrib><creatorcontrib>FRAKER, RICHARD</creatorcontrib><creatorcontrib>QUAN, WILLIAM</creatorcontrib><creatorcontrib>MIKULENCAK, PAUL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GIUNTOLI, DOMENIC S</au><au>CONDON, JOSEPH P</au><au>RITTS, MICHAEL A</au><au>WARREN, RYON CHRISTOPHER</au><au>BLADT, RALPH</au><au>FRAKER, RICHARD</au><au>QUAN, WILLIAM</au><au>MIKULENCAK, PAUL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT WINDOWS AND ASSOCIATED METHODS FOR INSTALLATION</title><date>2003-12-25</date><risdate>2003</risdate><abstract>Aircraft windows and associated methods for installation. The windows c an be installed in a passenger cabin of an aircraft and can include a frame tha t supports a pane assembly having a viewing area of at least 180 square inches . The viewing area can have a triangular shape, with the sides of the wind ow aligned with none of the major axis of the aircraft. Alternatively, the wind ow can have a longitudinally extended rectangular shape, a diamond shape or an elliptical shape. The window frame can have a divider portion that separates two window apertures, each of which carries a separate pane assembly. Adjacent windows can be closed out with a common bezel.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | AIRCRAFT WINDOWS AND ASSOCIATED METHODS FOR INSTALLATION |
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