slice bar
- slice bar的基本解释
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[机] 火铲, 火钩
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The structural mélanges is of the shape of a trumpet with its west section more wide and its east section more narrow, being made up of flysch slice, archibathyal silicalite, argillite slice, serpentinite slice, island arc slice, carbonate rock slice, continent-breaken pieces and so on.
该带西宽东窄,呈喇叭状,由复理石岩片、深海硅质岩、泥质岩岩片、蛇纹质岩片、火山岛弧岩片、碳酸盐岩岩片、大陆碎片岩片等组成。其中以复理石岩片为基质包含其它外来构造岩片。
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The Buqingshan — Huashxia superslice is complex, including Middle Proterozoic diorite-facies Kuhai melange slice, ophiolite slice of different times, Early Permian — Early Triassic flysch wedge, basic-acid volcanic slice and carbonate slice and Late Triassic — Early Jurassic Yangqu Fm. terrestrial clastic slice.
布青山一花石峡超岩片组成较复杂,包括中元古界角闪岩相变质的苦海杂岩岩片、不同时代蛇绿岩岩片、早二叠世—早三叠世复理石楔岩片、中酸性火山岩岩片和碳酸盐岩片以及早侏罗世羊曲组的陆相碎屑岩岩片。
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A rotor structure for a rotating wing aircraft having substantially rigid rotor head means and rotor blades or wing means arranged in at least one pair, comprising blade angle bearing means (10, 12, 14, 16) for each rotor blade means, tension bar means (6,8) operatively interconnecting the rotor blade means of a pair which blade means are arranged diametrically opposite each other, said tension bar means having a high bending resistance, whereby transmission of bending moments from the rotor blades to the rotor head means is substantially prevented, each of said blade angle bearing means comprising a structure angularly movable in the wing flap direction and in the wing lead-lag direction, at least one of said blade angle bearing means of a pair comprising means permitting an axial motion of the respective tension bar means supported in said blade angle bearing means, and wherein said blade angle bearing means (10, 12, 14, 16) operatively support said tension bar means (6, 8) on said rotor head means (4) for pitch angle rotation of said tension bar means relative to said rotor head means (4), said rotor structure further comprising means (24) securing said rotor blade means (18) to said tension bar means (6, 8) in a manner rigid against rotation of the blade means about the longitudinal blade axis whereby the securing means prevent flapping, drag and lagging movements of the tension bar means, said tension bar means being constructed as torsion bars which are elastic relative to torsion about said longitudinal blade axis.
1转子结构为旋转翼飞机,有大幅刚性转子头部的手段和转子叶片或机翼的手段安排中至少有一对,组成的叶片角度轴承手段( 10 , 12 , 14 , 16 )为每个转子叶片的手段,拉杆手段( 6,8 )手术互连转子叶片的手段,其中一对刀片的手段都是安排截然相反的对方说,拉杆手段,有一个高弯曲阻力,即传输弯矩从转子叶片向转子头的意思是,大幅防患于未然,每个叶片角度说,轴承的手段组成的一个结构angularly动产在机翼上皮瓣的方向和在机翼导致滞后的方向,至少有一个叶片角度说,轴承是指一对组成的手段,允许轴向的议案,分别紧张酒吧手段,支持在叶片角度说,轴承的手段,其中,叶片角度说,轴承的手段( 10 , 12 , 14 , 16 )手术的支持表示拉杆的手段( 6 , 8 )就表示,转子头部的手段( 4 )为俯仰角轮换说拉杆手段相对说,转子头部的手段( 4 )表示,转子结构进一步组成的手段,( 24 )说,确保转子叶片的手段( 18 )表示,拉杆手段( 6 , 8 )在一个僵化的方式对旋转的叶片即是说,约纵向叶片轴,即确保手段防止扑,拖曳和落后变动的紧张局势,酒吧的手段,说拉杆手段,正在建造的,作为扭杆这是弹性相对扭转约说,纵向叶片轴。