The invention concerns a spar structure (11) for connecting a moveable component (4) to an aircraft. The structure is formed from a single continuous body of material defining a plurality of attachment/actuation brackets (10A-10F) and a pair of continuous hinge lines (6, 7) extending through the body.
本发明涉及一种用于将可移动部件(4)连接到飞机的翼梁结构(11)。该结构由单个连续材料形体以及延伸穿过该形体的一对连续铰链线(6、7)形成,该形体限定多个附接/致动支架(10A至10F)。
HINGE STRUCTURE
铰链结构
08.02.2022
Patent
Elektronische Ressource
Chinesisch