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公开(公告)号:US07192256B2
公开(公告)日:2007-03-20
申请号:US10792708
申请日:2004-03-05
IPC分类号: F01D5/32
CPC分类号: F01D5/32 , F01D5/3038
摘要: The invention relates to a rotor end piece (1) for rotors (2) of thermal turbomachines with a circumferential slot (3), consisting of two end piece halves (4, 4′) having side faces (5, 5′) opposite one another in the installed state and of a wedge (6) which is pushed in between them and which, in the installed state, is anchored in the side faces (5, 5′) of the end piece halves (4, 4′) in a form-fitting manner, the rotor end piece (1) being arranged in the axial direction of the rotor (2) between two moving blades (7, 7′). It is characterized in that each of the end piece halves (4, 4′) is fastened in the axial direction of the rotor (2) to the two adjacent moving blades (7, 7′) by means of one interlocking connection (8, 8′, 9, 9′) each. These four interlocking connections (8, 8′, 9, 9′), instead of the rotor (2), now absorb the axial forces which are caused by the centrifugal force and the caulked wedge (6). In this way, disturbing rotor vibrations are advantageously avoided.
摘要翻译: 本发明涉及一种用于具有圆周槽(3)的热涡轮机的转子(2)的转子端件(1),由两个端部半部(4,4')组成,两个端部半部(4,4')具有与其相对的侧面 另一个处于安装状态,并且被推入它们之间的楔形件(6),并且在安装状态下将楔子(6)锚固在端部半部(4,4')的侧面(5,5')中 转子端件(1)沿转子(2)的轴向方向布置在两个活动叶片(7,7')之间。 其特征在于,通过一个互锁连接(8,8)将端部半部(4,4')中的每一个在转子(2)的轴向方向上紧固到两个相邻的活动叶片(7,7')上, 8',9,9')。 这四个互锁连接(8,8',9,9')代替转子(2)现在吸收由离心力和铆接楔(6)引起的轴向力。 以这种方式,有利地避免了干扰转子的振动。