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Turbine overspeed limit arrangement

机译:涡轮机超速限制安排

摘要

The invention relates to a turbomachinery turbine overspeed limiter. The turbine comprises a disk rotating around a longitudinal axis (AX) and a rotating blade (11),And a distributor (13) with fixed blades (12),Each rotating blade (11) comprises a free end terminated by a heel (19) carrying at least one ratchet wheel (23),Each guide vane (12) has a radial outer platform (29) through which it is connected to the crankcase component (9). Each platform (29) has an upstream end with a friction surface (36) relative to the left-handed body (23),When the turntable moves downward (AV), the left wheel (23) leans against the friction surface (36). The friction surface (36) has a radial cylindrical upstream portion which is the same as or farther from the free end of the left-handed body (23),And a tapered downstream portion inclined to the upstream (AM) direction along a longitudinal centerline (AX) away from the downstream (AV).Abstract figure: Figure 3
机译:本发明涉及一种涡轮机械涡轮机超速限制器。涡轮机包括围绕纵向轴线(AX)和旋转刀片(11)旋转的盘,以及具有固定叶片(12)的分配器(13),每个旋转刀片(11)包括由鞋跟终止的自由端(19载有至少一个棘轮(23),每个导向叶片(12)具有径向外平台(29),通过该径向外部平台(29),通过其连接到曲轴箱部件(9)。每个平台(29)具有相对于左手体(23)的摩擦表面(36)的上游端,当转盘向下移动(AV)时,左轮(23)倾斜摩擦表面(36) 。摩擦表面(36)具有径向圆柱形上游部分,其与左手主体(23)的自由端相同或更远,以及沿着纵向中心线倾斜于上游(AM)方向的锥形下游部分(斧头)远离下游(AV)。抽象图:图3

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