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    • 3. 发明授权
    • Support structure in a turbine or compressor device and a method for assembling the structure
    • 涡轮或压缩机装置中的支撑结构以及组装结构的方法
    • US07544040B2
    • 2009-06-09
    • US11551707
    • 2006-10-21
    • Gunnar MarkeJan-Erik AndreassonBo Johansson
    • Gunnar MarkeJan-Erik AndreassonBo Johansson
    • B23P15/04
    • F01D9/06F01D25/16F01D25/162F05D2230/11F05D2230/12F05D2230/21F05D2230/23F05D2230/61Y10T29/49323
    • The present invention relates to a support structure and a method for assembling a support structure in a turbine or compressor engine for rotatably supporting a rotor member in a stator member. The support structure includes an inner ring, an outer ring and a plurality of struts which extend radially between the inner ring and the outer ring. The inner ring has integrated portions projecting in the direction of the struts and forming end connections for the struts. The integrated end connecting portions of the inner ring are together with the ring made by a metal alloy having initially oversized cross sectional dimensions relative to the cross sectional dimensions of corresponding strut, followed by working at least one lateral surface for removing material. The purpose is to achieve final dimensions and position to conform to the cross sectional dimensions and correct position of each corresponding strut.
    • 本发明涉及一种用于在涡轮或压缩机发动机中组装支撑结构的支撑结构和方法,用于将定子构件中的转子构件可旋转地支撑。 支撑结构包括内环,外环和在内环和外环之间径向延伸的多个支柱。 内环具有沿支柱的方向突出的一体化部分并形成支柱的端部连接。 内圈的一体化的端部连接部分与由具有相对于相应的支柱的横截面尺寸的具有初始尺寸过大的横截面尺寸的金属合金制成的环一起,然后工作至少一个用于去除材料的侧表面。 目的是达到最终的尺寸和位置以符合每个对应支柱的横截面尺寸和正确的位置。