发明名称 Turbine exhaust strut airfoil profile
摘要 A turbine exhaust thin strut includes an airfoil section having a profile substantially in accordance with at least an intermediate portion of the Cartesian coordinate values of X, Y and Z set forth in Table 2. The X and Y values are distances, which when smoothly connected by an appropriate continuing curve, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape.
申请公布号 US7857594(B2) 申请公布日期 2010.12.28
申请号 US20060563783 申请日期 2006.11.28
申请人 PRATT & WHITNEY CANADA CORP. 发明人 KIDIKIAN JOHN;VLASIC EDWARD;GIRGIS SAMI
分类号 B63H1/26;B63H7/02;B64C11/16;B64C27/46;F01D5/14;F03B7/00;F03D11/02;F04D29/38 主分类号 B63H1/26
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