发明名称 HP TURBINE VANE AIRFOIL PROFILE
摘要 <p>A high pressure turbine vane includes an airfoil 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. The design of the airfoil equalizes the static pressure gradient in the spanwise direction. This allows to minimize secondary losses.</p>
申请公布号 CA2610539(C) 申请公布日期 2015.11.24
申请号 CA20072610539 申请日期 2007.11.14
申请人 PRATT & WHITNEY CANADA CORP. 发明人 MOHAN, KRISHAN;GIRGIS, SAMI
分类号 F01D5/14;F01D9/02 主分类号 F01D5/14
代理机构 代理人
主权项
地址