发明名称 ROTOR BLADE TIP PLAN FORM
摘要 A main rotor blade incorporating a rotor blade tip region having a tip chord and a tip taper such that the ratio of the main rotor blade chord to the tip chord is approximately 0.30. The tip taper ratio preferably providing an approximately 28% area of reduction in said outer 10% of said blade span. The tip region preferably further including a hover optimized high lift airfoil and a tip sweep that reaches a constant value of approximately 30 degrees along the quarter chord line.
申请公布号 WO2007102852(A3) 申请公布日期 2007.11.29
申请号 WO2006US40668 申请日期 2006.10.17
申请人 SIKORSKY AIRCRAFT CORPORATION;MOFFITT, ROBERT, C.;EGOLF, THOMAS, ALAN;BEATTY, ROBERT, D.;KARPOWICH, JOHN, K. 发明人 MOFFITT, ROBERT, C.;EGOLF, THOMAS, ALAN;BEATTY, ROBERT, D.;KARPOWICH, JOHN, K.
分类号 B63H1/06 主分类号 B63H1/06
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