发明名称 HIGH-POSITIONED 2-POSITION VARIABLE CAMBER KRUEGER
摘要 A variable camber Krueger flap deployment linkage mechanism is presented. A first linkage assembly couples a flap assembly and an airfoil, and comprising a first drive arm, a first drive link, and a support arm. A second linkage assembly couples the flap assembly and the first drive arm, and comprises a drive transfer arm, a middle connection segment, and a bullnose link.
申请公布号 US2014312175(A1) 申请公布日期 2014.10.23
申请号 US201313867562 申请日期 2013.04.22
申请人 The Boeing Company 发明人 Sakurai Seiya;Fox Stephen J.;Reyes Victor H.
分类号 B64C13/28;B64C9/24 主分类号 B64C13/28
代理机构 代理人
主权项 1. A variable camber Krueger flap deployment linkage mechanism comprising: a first linkage assembly configured to couple to a flap assembly and an airfoil, the first linkage assembly comprising: a first drive arm configured to couple to an actuator coupled to the airfoil, and configured to rotate in a chord-wise plane;a first drive link coupled to the first drive arm and a trailing end of the flap assembly; anda support arm coupled to a middle link portion of the first drive link and configured to rotatably couple to the airfoil at a rotation joint; and a second linkage assembly configured to couple to the flap assembly and the first drive arm, the second linkage assembly comprising: a drive transfer arm coupled to the flap assembly;a middle connection segment configured to couple the drive transfer arm to the trailing end of the flap assembly; anda bullnose link configured to couple the drive transfer arm to a bullnose portion of the flap assembly.
地址 Chicago IL US