发明名称 COMPRESSOR SYSTEM AND AIRFOIL ASSEMBLY
摘要 PROBLEM TO BE SOLVED: To provide an airfoil assembly.SOLUTION: An airfoil assembly (44) comprises: at least one airfoil (50) having a leading edge (51) and a trailing edge (52); a band (60, 80) rigidly coupled to the at least one airfoil (50) along a portion of an interface (70) between the band (60, 80) and the at least one airfoil (50) for providing at least a portion of support for the at least one airfoil (50); a relief (72) located in the band (60, 80) at the leading edge (51) or trailing edge (52) of the at least one airfoil (50), the relief (72) defining a stress relief gap (74) between the band (60, 80) and the leading edge (51) or trailing edge (52); and a closure (76) preventing an airflow through the relief (72).SELECTED DRAWING: Figure 1
申请公布号 JP2016211563(A) 申请公布日期 2016.12.15
申请号 JP20160092357 申请日期 2016.05.02
申请人 GENERAL ELECTRIC CO <GE> 发明人 SHAWN PATRICK RILEY;ABIGAIL ROSE VAUGHN;HU HAI-YUN
分类号 F04D29/54 主分类号 F04D29/54
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