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    • 7. 发明授权
    • Rotor blade damping structure for axial-flow turbine
    • 轴流式涡轮转子叶片阻尼结构
    • US5511948A
    • 1996-04-30
    • US320545
    • 1994-10-11
    • Atsuhide SuzukiHirotsugu KodamaToshio Suzuki
    • Atsuhide SuzukiHirotsugu KodamaToshio Suzuki
    • F01D5/26F01D5/22F01D5/30F01D5/32F03G4/00
    • F01D5/3046F01D5/225
    • In an axial-flow turbine, at least one of front and rear side contact surfaces of shrouds (3a or 3b) of blades (1a or 1b) with respect to the turbine rotational direction is formed at certain angle with respect to a radial line connecting the rotor center and the contact surface. The shroud (3a) of the blade (1a) of a first kind is formed in a trapezoidal shape converging radially outward in cross section taken in a plane perpendicular to the turbine axial direction, and the shroud (3b) of the blade (1b) of a second kind is formed in an inverted trapezoidal shape converging radially inward in the cross section. Further, half of an angle (2.alpha.) between the front and rear side contact surfaces of the shrouds (3a or 3b) is made smaller than a static frictional angle of the contact surface. Since the shroud contact surfaces of two adjacent blades can be kept in pressure contact with each other under all operating conditions, a large dynamic stress reduction and superior damping properties can be obtained without producing excessive initial stresses at the blade airfoil and blade dovetail attachment portion.
    • 在轴流涡轮机中,相对于涡轮机旋转方向,叶片(1a或1b)的护罩(3a或3b)的前后侧接触表面中的至少一个相对于连接到涡轮机的径向线形成一定角度 转子中心和接触面。 第一种叶片(1a)的护罩(3a)形成为在垂直于涡轮轴线方向的平面截取的横截面中径向向外收敛的梯形形状,并且叶片(1b)的护罩(3b) 第二种形式在横截面中以径向向内收敛的倒梯形形状。 此外,使护罩(3a或3b)的前侧和后侧接触表面之间的角度(2α)的一半被制成小于接触表面的静摩擦角。 由于两个相邻叶片的护罩接触表面可以在所有操作条件下彼此保持压力接触,所以可以获得大的动态应力减小和优异的阻尼性能,而不会在叶片翼型和叶片燕尾形连接部分处产生过大的初始应力。