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    • 12. 发明授权
    • Gas turbine rotor with remote support rings
    • 燃气轮机转子带有远程支撑环
    • US5660526A
    • 1997-08-26
    • US461122
    • 1995-06-05
    • Robert Anthony Ress, Jr.
    • Robert Anthony Ress, Jr.
    • F01D5/08C22C14/00C22C19/03C22C47/00C22C49/00C22C49/08C22C49/11F01D5/02F01D5/06F01D5/28F01D5/30F02C7/00F02C7/16F02C7/18
    • F01D5/02F01D5/025F01D5/06F01D5/28F05D2300/603Y02T50/672
    • A lightweight gas turbine rotor having a pair of high specific strength support ring members positioned fore and aft a center hub member. The unitary center hub member for carrying a plurality of airfoils that extend radially outward therefrom. The pair of high specific strength support ring members are connected to the blade carrying member at a location to compressively transmit the centrifugal force generated by the rotating rotor to a radially inward location on the support ring members. The support ring members being utilized to resist a majority of the centrifugal force generated by the components of the rotor. The center hub member and the pair of support ring members are made of different materials. More particularly the pair of support ring members are made of a metal matrix composite, and the center hub member when utilized in a compressor is formed of a high temperature titanium alloy, and the center hub member when utilized in a turbine is formed of a nickel alloy.
    • 一种轻型燃气轮机转子,其具有一对位于中心毂构件前后的高比重强度的支撑环构件。 用于承载从其径向向外延伸的多个翼型件的单一中心轮毂构件。 一对高比强度支撑环构件在一个位置处连接到刀片承载构件,以将由旋转转子产生的离心力压缩地传递到支撑环构件上的径向向内的位置。 支撑环构件用于抵抗由转子的部件产生的大部分离心力。 中心毂构件和一对支撑环构件由不同的材料制成。 更具体地,一对支撑环构件由金属基复合材料制成,并且当在压缩机中使用时,中心毂构件由高温钛合金形成,并且当在涡轮中使用中心毂构件时,由镍 合金。