Spoiler deployment mechanism
作者： Damian Allen
DOI:
关键词:
摘要: An aircraft wing assembly comprising: a (1); spoiler (2) pivotally attached to the wing; and deployment mechanism. The mechanism comprises scissor linkage (7) comprising an upper link (9) at pivot (10), lower (11) (10) central (13). actuator (8) is proximal distal pivot. adjustable between expanded contracted configurations so as vary distance pivots. This opens up angle links of pushes into air-stream above wing.
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