发明名称 LP TURBINE BLADE AIRFOIL PROFILE
摘要 <p>A single stage low pressure turbine blade includes an airfoil having a profi le 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.</p>
申请公布号 CA2610625(A1) 申请公布日期 2008.05.22
申请号 CA20072610625 申请日期 2007.11.15
申请人 PRATT & WHITNEY CANADA CORP. 发明人 TSIFOURDARIS, PANAGIOTA;GIRGIS, SAMI;MOHAN, KRISHAN
分类号 F01D5/14 主分类号 F01D5/14
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