发明名称 BEAM
摘要 <p>A beam (20) comprising first and second flanges (23, 24), the beam (20) having a first region (28, 30) extending between the flanges (23, 24) and a second region (26) extending between the flanges. The first region (28, 30) is designed to support an applied concentrated shear load and the second region (26) is designed to support a predominantly bending load. The first region comprises a fan-shaped truss comprising a hub (36) adjacent the first flange and a plurality of struts (37) which extend substantially radially from the hub (36), and the second region (26) comprises either a truss structure which is substantially regular in the longitudinal beam direction or a shear web. The beam may, for example, be used as a floor beam for an aircraft fuselage.</p>
申请公布号 WO2012007449(A1) 申请公布日期 2012.01.19
申请号 WO2011EP61835 申请日期 2011.07.12
申请人 AIRBUS OPERATIONS LIMITED;AIRBUS OPERATIONS GMBH;AIRBUS OPERATIONS SAS;KROG, LARS;AIRBUS OPERATIONS SL;MARASCO, ANDREA;GRIHONS, STEPHANE;JUERGENS, MANUELA;RYAN, GARY;BATES, STUART 发明人 KROG, LARS;MARASCO, ANDREA;GRIHONS, STEPHANE;JUERGENS, MANUELA;RYAN, GARY;BATES, STUART
分类号 B64C1/18 主分类号 B64C1/18
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