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.
System and method for operating a droop panel using a pin joint linkage assembly
2018-01-30
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SYSTEM AND METHOD FOR OPERATING A DROOP PANEL USING A PIN JOINT LINKAGE ASSEMBLY
Europäisches Patentamt | 2016
|LINKAGE MECHANISM FOR LINKING A FLAPERON TO A DROOP PANEL OF AN AIRCRAFT
Europäisches Patentamt | 2019
|LINKAGE MECHANISM FOR LINKING A FLAPERON TO A DROOP PANEL OF AN AIRCRAFT
Europäisches Patentamt | 2019
|