A trailing edge double fold flap for underwing mounting of an aircraft wing is disclosed. A dual fold flap pivotally coupled to the wing is movable between a stowed position positioned along a lower surface of the wing and a deployed position aft of a trailing edge of the wing. The double fold flap includes a front panel and a rear panel. The rear panel is pivotally coupled to the front panel and is foldable relative to the front panel. The rear panel folds toward the front panel when the double fold flap is in the stowed position. The rear panel deploys from the front panel when the double fold flap is in the deployed position. An outer fillet piece pivotally coupled to the front panel pivots relative to the double fold flap as the double fold flap moves between the stowed position and the deployed position.
公开了一种用于飞机机翼的机翼下安装的后缘双折叠襟翼。枢转地耦接到机翼的双折叠襟翼可在沿着机翼的下表面定位的收起位置和位于机翼的后缘的后方的部署位置之间移动。双折叠襟翼包括前面板和后面板。后面板枢转地耦接到前面板并且可相对于前面板折叠。当双折叠襟翼处于收起位置时,后面板朝向前面板折叠。当双折叠襟翼处于部署位置时,后面板从前面板展开。当双折叠襟翼在收起位置和部署位置之间移动时,枢转地耦接到前面板的外圆角件相对于双折叠襟翼枢转。
Sub-wing mounted trailing edge double fold flap for aircraft wing
用于飞机机翼的机翼下安装的后缘双折叠襟翼
2024-07-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |