首页> 外国专利> Blade for rotating wing of helicopter is divided in three zones, with width of blade maximal in first zone, decreasing linearly in second one, and decreasing following parabolic function in third one

Blade for rotating wing of helicopter is divided in three zones, with width of blade maximal in first zone, decreasing linearly in second one, and decreasing following parabolic function in third one

机译:直升机旋转翼的叶片分为三个区域,叶片宽度在第一区域最大,在第二区域线性减小,在第三区域跟随抛物线函数减小

摘要

Blade (1) is subdivided in three zones (Z1, Z2, Z3) along its length. First zone (Z1) extends front inner edge (R0) to section situated at around 90% of its total length (R1); second zone (Z2) extends from section R1 to section situated at around 95 % of total length (R2); and third zone (Z3) extends from section R2 to free end (R) of blade. Width (L) is maximum, and slightly constant in first zone, decreases linearly in second zone, and decreases following parabolic function in third zone.
机译:刀片(1)沿其长度分为三个区域(Z1,Z2,Z3)。第一区域(Z1)延伸前内边缘(R0)到位于其总长度(R1)大约90%处的部分;第二区域(Z2)从部分R1延伸到位于总长度(R2)约95%的部分。第三区域(Z3)从部分R2延伸到叶片的自由端(R)。宽度(L)最大,在第一个区域中稍为恒定,在第二个区域中线性减小,在第三个区域中遵循抛物线函数减小。

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