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 |
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代理人 |
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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 |