Invention Grant
US08128020B2 Active twisting of an aircraft lifting surface via modulated clamping of substructure 有权
通过调节夹紧子结构主动扭转飞机提升表面

Active twisting of an aircraft lifting surface via modulated clamping of substructure
Abstract:
A system and method for enabling controlled twisting of a tip of a wing in response to the aerodynamic forces experienced by the wing. The structural stiffness of the wing is modulated to modulate the twist of the wing in the presence of aerodynamic forces.
Information query
Patent Agency Ranking
0/0