发明名称 SCALING TO CUSTOM-SIZED TURBOMACHINE AIRFOIL METHOD
摘要 A method of engineering a turbomachine airfoil may include providing a master airfoil configuration having a preset outer and inner radius relative to an axis of rotation thereof. The master airfoil configuration may be radially scaled to a custom-sized turbomachine airfoil having an outer radius different than the preset outer radius of the master airfoil configuration, and/or an inner radius different than the preset inner radius of the master airfoil configuration. Tuning a frequency of the custom-sized turbomachine airfoil by changing a parameter of at least one of a part span shroud and a tip shroud may then be performed. Axial scaling may also be performed. The custom-sized turbomachine airfoil may be employed in the turbomachine without performing wheel box testing, and may exhibit substantially similar operational characteristics as the master airfoil configuration.
申请公布号 US2015089809(A1) 申请公布日期 2015.04.02
申请号 US201314039588 申请日期 2013.09.27
申请人 General Electric Company 发明人 Guo Tao;Boisclair Michael Ernest;Cotroneo Joseph Anthony;Hofer Carl Douglas;Mujezinovic Amir;Ostrovskiy Vsevolod Yuriyevich
分类号 B23P15/02;F01D5/14 主分类号 B23P15/02
代理机构 代理人
主权项 1. A method of engineering a turbomachine airfoil, the method comprising: providing a master airfoil configuration having a preset outer radius and a preset inner radius relative to an axis of rotation thereof; and radially scaling the master airfoil configuration to a custom-sized turbomachine airfoil having at least one of: an outer radius different than the preset outer radius of the master airfoil configuration and an inner radius different than the preset inner radius of the master airfoil configuration.
地址 Schenectady NY US