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 |
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代理人 |
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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 |