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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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