发明名称 LOAD-BEARING STRUCTURAL PANEL FOR AIRCRAFT LANDING MATS AND LIKE STRUCTURES
摘要 1,224,851. Welding by fusion. DOW CHEMICAL CO. 5 March, 1969 [6 March, 1968], No. 11823/69. Heading B3R. [Also in Division E1] In an aircraft landing mat or other decking structure composed of a series of interlocking or bolted-together rectangular or other metal panels 10, each panel comprises top and bottom plates 12, 14 connected by webs 16 and provided with a welded-on coupling bar 18 seated on a bevelled tongue whose end face is slanted to the panel plane at an angle A between 65 and 85 degrees, the tongue being formed by (a) sliding rectangular tubes 17 into the channels between the webs 16; (b) bevelling and cutting the parts to the shape shown; and (c) securing the tubes 17 to the webs 16 by welds 28. The bar 18 is secured by walls 20. The panels shown have side interlock formations 22.
申请公布号 GB1224851(A) 申请公布日期 1971.03.10
申请号 GB19690011823 申请日期 1969.03.05
申请人 THE DOW CHEMICAL COMPANY 发明人 GORDON KEITH GLAZA;KARL FRIEDRICH BRAEUNINGER
分类号 E01C5/00;E01C5/16;E01C9/08;F16B5/00 主分类号 E01C5/00
代理机构 代理人
主权项
地址