发明名称 INCREASING LIFT ON HELICOPTER ROTOR BLADES AND AIRPLANE PROPELLERS
摘要 A rotary airscrew having a central hub (9) with coaxial first and second counter-rotating drive shafts (10, 11), a first set of a plurality of non-lift blades (10) connected to the first drive shaft (10) for rotation to be rotated for moving air therewith, a second set of a plurality of primary airfoil blades (2) connected to the second drive shaft (11), to be rotated counter to the rotation direction of the plurality of non-lift blades, and spaced apart from the non-lift blades with a small clearance distance to allow non-contacting counter-rotation, and a ring (3) for supporting the first and second sets of blades with a small clearance distance between the ends as they are rotated.
申请公布号 WO9405545(A1) 申请公布日期 1994.03.17
申请号 WO1992US07437 申请日期 1992.09.03
申请人 KREPAK, JOHN, C. 发明人 KREPAK, JOHN, C.
分类号 B64C11/00;B64C27/10;B64C27/20;(IPC1-7):B64C27/10 主分类号 B64C11/00
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