首页> 外国专利> Rotor blade for a helicopter comprises a rotor blade profile and a bending actuator which is to be fixed with a first end to an end region of a profile base body and with a second end protruding freely from the profile base body

Rotor blade for a helicopter comprises a rotor blade profile and a bending actuator which is to be fixed with a first end to an end region of a profile base body and with a second end protruding freely from the profile base body

机译:用于直升机的旋翼桨叶包括旋翼桨叶轮廓和弯曲致动器,该弯曲致动器的第一端固定到轮廓基体的端部区域,第二端从轮廓基体自由突出。

摘要

Rotor blade (20) comprises a rotor blade profile and a bending actuator (26) which is to be fixed with a first end to an end region of a profile base body (20a) and with a second end protruding freely from the profile base body and its end region toward the rear edge. The rotor blade profile has a nose region, the base body with a profile core (22) and a covering skin (30) enclosing the profile core and a rear edge region (23) with a rear edge (40). An independent claim is also included for a helicopter with the above rotor blade. Preferred Features: The bending actuator is a flat, plate-like and/or strip-like bending actuator. The actuator is arranged on a support layer, preferably made from a plastic material reinforced with glass fibers.
机译:转子叶片(20)包括转子叶片轮廓和弯曲致动器(26),弯曲致动器(26)的第一端固定到轮廓基体(20a)的端部区域,第二端从轮廓基体自由突出。并且其末端区域朝向后边缘。转子叶片轮廓具有鼻部区域,具有轮廓核心(22)的基体和包围轮廓核心的覆盖蒙皮(30)以及具有后边缘(40)的后边缘区域(23)。具有上述旋翼桨叶的直升机也包括独立权利要求。优选特征:弯曲致动器是平坦的,板状和/或条状的弯曲致动器。致动器布置在支撑层上,支撑层优选地由用玻璃纤维增​​强的塑料材料制成。

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