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Rotor blades of steam turbines for SECTIONS OF LOW PRESSURE steam turbine

机译:低压蒸汽轮机部分的蒸汽轮机转子叶片

摘要

1. The rotor blade (20) of a steam turbine, comprising: portion (42) of the airfoil; ! section (44) of the shank fixed to one end portion (42) of the airfoil; ! section (40) in a dovetail protruding from the section (44) of the shank, wherein the section (40) into a dovetail portion includes a tapered dovetail with axial zavodki; ! section (46) ring attached to a portion (42) of the airfoil at the end opposite the section (44) of the shank; ! shroud flange (48) integrally formed as part of the section (46) ring; ! a shelf (50) attached at an intermediate portion of the section (42) of the airfoil between its ends; ! wherein the blade (20) has an annular outlet section area ratio of 4.43 m2 or more. ! 2. The blade according to claim 1, wherein the chamfered portion (40) in the form of a dovetail with axial winding of a taper angle of 19 °. ! 3. The blade according to claim 1, wherein the portion (42) of the airfoil has a length of approximately 68.1 cm or more. ! 4. The blade according to claim 1, wherein the shroud flange (48) comprises a planar section extending from the front edge (34) of a portion (42) of the airfoil at a predetermined distance from it toward the trailing edge (36) of a portion (42) of the airfoil, wherein the shroud flange (48) has a width decreasing substantially from the end located at a predetermined distance from the leading edge (34) to a location substantially in the center with respect to the trailing edge (36) and the front edge (34 ), and the width of the shroud flange (48) increases from the center (58) to the rear kro MKE (36), and the width of the shroud flange (48) at an end raspolozhennog
机译:1.一种蒸汽涡轮机的转子叶片(20),包括:所述翼型的部分(42);以及所述翼型的一部分。 !固定在翼型的一个端部(42)上的杆的部分(44); !在从柄的部分(44)突出的燕尾中的部分(40),其中进入燕尾部分的部分(40)包括带有轴向zavodki的锥形燕尾; !在与柄的部分(44)相对的端部上附接到翼型部分(42)的部分(46)环; !作为部分环(46)的一部分整体形成的护罩凸缘(48); !架子(50),其连接在翼型部分(42)两端之间的中间部分; !其中叶片(20)具有4.43m2或更大的环形出口截面面积比。 ! 2.根据权利要求1所述的叶片,其特征在于,倒角部分(40)为燕尾形,其轴向缠绕的锥角为19°。 ! 3.根据权利要求1所述的叶片,其中,所述翼型件的所述部分(42)具有大约68.1cm或更长的长度。 ! 4.根据权利要求1所述的叶片,其中,所述护罩凸缘(48)包括从所述翼型件的一部分(42)的前边缘(34)以预定距离从其朝向所述后缘(36)延伸的平面部分。翼型件的一部分(42)的轮廓,其中,护罩凸缘(48)的宽度从从位于距前缘(34)预定距离的端部到相对于后缘基本上在中心的位置基本上减小(36)和前边缘(34),并且护罩法兰(48)的宽度从中心(58)到后kro MKE(36)增加,并且护罩法兰(48)的宽度在一端覆盆子

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