发明名称 Tip cambered swept blade
摘要 <p>A fan blade includes an airfoil having opposite pressure and suction sides extending in span between a root and tip, and extending in chord between opposite leading and trailing edges. From root toward tip, the airfoil includes increasing stagger and decreasing camber, and increasing chord length to barrel the airfoil along both the leading and trailing edges. The airfoil further includes forward aerodynamic sweep at the tip, and non-forward aerodynamic sweep between the maximum barrel and the root.</p>
申请公布号 GB0616347(D0) 申请公布日期 2006.09.27
申请号 GB20060016347 申请日期 2006.08.17
申请人 GENERAL ELECTRIC COMPANY 发明人
分类号 主分类号
代理机构 代理人
主权项
地址