发明名称 Cascade rotor blade for low noise
摘要 Low-noise airfoils and methods of reducing noise. One embodiment provides an aerodynamic member that includes two body portions coupled to each other. The second body portion includes a plurality of airfoil members in a fixed relationship with each other. Optionally, the airfoil members may define an open end of the second body portion. In the alternative, the member can include a third body portion that has an airfoil shape and that is coupled to the second body portion opposite the first body portion. Preferably, the first portion, the airfoil members, and third portion are 12%, 8%, and 2% thickness/chord airfoils respectively. Further, the aerodynamic member may be a rotor blade on a tandem helicopter. Another embodiment provides a cambered airfoil with two coupled body portions one of which has air foil members. One of the body portions includes a slot there through with airfoil members on opposite sides of the slot.
申请公布号 US2006257261(A1) 申请公布日期 2006.11.16
申请号 US20050129594 申请日期 2005.05.13
申请人 THE BOEING COMPANY 发明人 ZIENTEK THOMAS A.
分类号 A23L3/18 主分类号 A23L3/18
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