System and method for operating a droop panel using a pin joint linkage assembly
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United States of America Patent
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Jan 30, 2018
Issued Date -
N/A
app pub date -
Sep 19, 2014
filing date -
Sep 19, 2014
priority date (Note) -
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Abstract
A system for operating a droop panel on an air vehicle, the droop panel positioned between a fixed structure and a trailing edge flap on the wing. The system includes a pin joint linkage assembly coupled between and to the fixed structure, the droop panel, and the trailing edge flap. The assembly has a first link attached to the fixed structure; and a second link coupled to the first link, and pivotably connected to a third pin joint, connected to a fourth pin joint, and an angled portion pivotably connected to a second pin joint. The assembly has a third link coupled to the second link, and coupled to the fourth pin joint and to a fifth pin joint attached to the trailing edge flap. The assembly is configured to operate the droop panel by concurrently moving the droop panel and the trailing edge flap in a single coordinated motion.
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