ROTOR HUB FAIRING SYSTEM FOR A COUNTER-ROTATING, COAXIAL ROTOR SYSTEM |
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| 申请号 | PCT/US2006016401 | 申请日 | 2006-04-28 | 公开(公告)号 | WO2006130287A3 | 公开(公告)日 | 2007-10-04 |
| 申请人 | SIKORSKY AIRCRAFT CORP; | 发明人 | BERTOLOTTI FABIO P; | ||||
| 摘要 | A rotor hub fairing system includes an upper hub fairing, a lower hub fairing and a shaft fairing therebetween. The rotor hub fairing system is sized and configured to reduce the overall drag on a dual, counter-rotating, coaxial rotor system. Preferably, the rotor hub fairing is fully integrated. The shaft fairing preferably includes a minimal thickness at the midsection to reduce drag with an increasing thickness adjacent the upper and lower hub fairings to reduce the flow separation on the hub fairing surfaces without overly excessive drag. Other aerodynamic structures, such as a horizontal splitter and/or a plurality of turning vanes may be mounted to the shaft fairing to facilitate flow around the upper and lower hub fairings to reduce flow separation and drag. | ||||||
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