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LINKAGE MECHANISM FOR LINKING A FLAPERON TO A DROOP PANEL OF AN AIRCRAFT
LINKAGE MECHANISM FOR LINKING A FLAPERON TO A DROOP PANEL OF AN AIRCRAFT
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机译:将襟副翼与飞机降落面板链接的链接机制
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摘要
A linkage mechanism for a flaperon includes a support structure linkage, a droop panel linkage, and a flaperon linkage. The support structure linkage is pivotally attached to a support structure of a wing of an aircraft. The droop panel linkage is pivotally attached a droop panel. The flaperon linkage is pivotally attached to a flaperon. A second end of the droop panel linkage and a second end of the flaperon linkage are pivotally attached to a connecting section of the support structure linkage. The connecting section is spaced apart from the pivot end of the support structure linkage such that the linkage mechanism transfers a pivoting motion from the flaperon into a pivoting motion of the droop panel.
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