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Turbine blade having a plurality of configurations chamfered squealer tip formed from members and convection cooling holes

机译:涡轮叶片具有多种构型,由构件和对流冷却孔构成的斜切式油压叶梢

摘要

It is available in repair system, and a squealer tip formed from the pressure-side weld rib (12) and the suction-side outer weld rib (14) (10), a pressure-side weld ribs and the suction-side outer weld ribs, the turbine The extending from the tip of the blade (18) (16) radially outward is present in the pressure side and the suction side welded members separated by an intermediate chord members (21) (17, 19) discloses a squealer tip . The pressure side and suction side outer weld ribs, respectively, are positioned along the pressure side of the turbine blade (20) and suction side (22). The pressure side outer welding rib has a chamfered pressure side (24) having film cooling holes (26) having an exhaust outlet positioned therein. The pressure side and suction side welded member is configured to hold the intermediate chord members in position over extended sides.
机译:它可在维修系统中使用,并由压力侧焊接肋(12)和吸力侧外部焊接肋(14)(10),压力侧焊接肋和吸力侧外部焊缝形成的泄油嘴从叶片(18)(16)的尖端径向向外延伸存在于压力侧,并且由中间弦杆(21)(17、19)隔开的吸力侧焊接构件公开了一种压紧器尖端。压力侧和吸气侧外部焊接肋分别沿着涡轮叶片(20)和吸气侧(22)的压力侧定位。压力侧外部焊接肋具有倒角的压力侧(24),该压力侧具有膜冷却孔(26),在膜冷却孔中设有排气口。压力侧和吸力侧焊接构件构造成将中间弦杆构件在延伸侧上保持就位。

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