首页> 外国专利> Location for propeller blade made of fibre cpd. - has loop rail with bearing shaft extending through propeller blade root with loop rail extending around bearing shaft

Location for propeller blade made of fibre cpd. - has loop rail with bearing shaft extending through propeller blade root with loop rail extending around bearing shaft

机译:纤维cpd制成的螺旋桨叶片的位置。 -带有滑轨,轴承轴穿过螺旋桨叶片根部延伸,而滑轨在轴承轴周围延伸

摘要

The bearing shaft (2) is formed at approximately 90 deg. to the longitudinal axis of the propeller blade and the loop rail (12) is of one-piece construction. The loop rail is arranged at approximately 90 deg. to the profile longitudinal axis parallel to the bearing shaft (2) on the propeller blade rail (1). The propeller blade root (13) is rectangular and to accommodate the bearing shaft has a bearing bush (8). On the outside (14) of the propeller blade root damping elements are arranged (5). The accommodation aperture (15) of the propeller blade casing (4) for the propeller blade root (13) widens outwards in the area of the damping elements (5). USE/ADVANTAGE - A propeller blade location for aircraft and of ground effect vehicles in which the bearing shaft is arranged at 90 deg. to the profile longitudinal axis of the propeller blade, with the loop rail being of one-piece construction.
机译:轴承轴(2)形成大约90度。螺旋桨叶片的纵轴和环轨(12)呈一体式结构。环形滑轨的位置大约为90度。平行于螺旋桨叶轨(1)上轴承轴(2)的轮廓纵轴。螺旋桨叶根(13)为矩形,为容纳轴承轴,轴颈带有一个轴承衬套(8)。在螺旋桨叶片的外侧(14)上布置了根部阻尼元件(5)。螺旋桨叶片壳体(4)的螺旋桨叶片根部(13)的容纳孔(15)在阻尼元件(5)的区域内向外加宽。使用/优点-飞机和地面飞行器的螺旋桨叶片位置,轴承轴以90度角布置。螺旋桨与螺旋桨叶片的轮廓纵轴成直角,其中环轨为一件式结构。

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