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Hallo John, hallo Brien,
thanks for your comparison of the diskrotor with the tiltrotor. But despite of nearly 50 years long development, the tiltrotor has two faults: It has not optimal rotors for hovering and not optimal props for cruising. It means, that a tiltrotor lifts less load in hovering than a conventional helicopter and cruise slower than a conventional turboprop airplane with equal installed power. The diskrotor is optimal for hovering because the big disk brings law and order in the aerodynamic of a helicopter rotor and the disk with retracted rotor blades is well suitable for a really fast cruising. Even supersonic speeds are feasible!!! George "brien" wrote in message ... I agree the concept has at least as much merit as a tilt rotor. Brien "John Roncallo" wrote in message ... George Vranek wrote: In the last weeks, there is a big silence in this NG regarding fast flying helicopters. Please have a look at www.vranek.ch/diskrotor.htm and publish your comments and questions if any in this NG. Geoge I see a lot of negativity in this NG about this concept but I feel it has at laest as much merit as a tilt rotor. J. Roncallo My opinions posted on this news group are my own and do not represent the company I work for. |
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