首页> 外国专利> Helicopter blade for use in hub, has hollow vane end integrated to blade, where vane end is streamlined body for presenting streamlined three-dimensional shape and has lower reinforcement which locks two adjacent lower tapes

Helicopter blade for use in hub, has hollow vane end integrated to blade, where vane end is streamlined body for presenting streamlined three-dimensional shape and has lower reinforcement which locks two adjacent lower tapes

机译:用于轮毂的直升机叶片具有与叶片集成的空心叶片端,叶片端是流线型主体,可呈现流线型三维形状,并具有下部加固装置,可锁定两个相邻的下部胶带

摘要

The blade (1) has a wing tip and a hollow vane end (10). A spar (3) and an outer covering (4, 4`) are arranged along wing span of the blade. The vane end is integrated to the blade, where the spar is made of glass fiber such as roving glass fiber. The vane end has an outer wall with the covering integrated to upper tapes (31) and lower tapes (32) from the spar of the blade. The vane end is a streamlined body to present a streamlined three-dimensional shape coherent with streamlined shape of the blade. The end has lower reinforcement which locks the two adjacent lower tapes (32).
机译:叶片(1)具有翼尖和中空的叶片端(10)。沿叶片的翼展布置有翼梁(3)和外壳(4、4`)。叶片端与叶片成一体,其中翼梁由玻璃纤维(如粗纱玻璃纤维)制成。叶片端具有外壁,覆盖物与叶片翼梁的上带(31)和下带(32)成一体。叶片端是流线型主体,以呈现与叶片的流线型形状连贯的流线型三维形状。该端部具有下部加固物,该下部加固物将两个相邻的下部胶带(32)锁定。

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