Novel low-noise highly-skewed ducted propeller
A technology of ducted propeller and large side tilt, which is applied in the direction of rotating propeller and rotating propeller to achieve the effect of reducing vibration and noise
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[0077] (1) Case 1
[0078] For a certain unmanned aerial vehicle, the present invention is adopted as its propulsion device. The diameter of the propeller is 372mm, and the number of blades is 7. The propeller parameters are determined by the following table:
[0079] Table 3.1 Geometric elements of the propeller in Embodiment 1
[0080] Location pitch ratio Side Slope trim ratio Chord ratio camber ratio Maximum Thickness Ratio r / R P / D θs(°) x R / D C / D f m / C t m / C 0.2 1 -14.7 0.002 0.190 0.0377 0.2633 0.3 1 -20.9 -0.004 0.208 0.0346 0.2046 0.4 1 -21.7 -0.013 0.222 0.0309 0.1655 0.5 1 -17.5 -0.026 0.234 0.0272 0.1414 0.6 1 -10.9 -0.033 0.242 0.0238 0.1207
[0081] Location pitch ratio Side Slope trim ratio Chord ratio camber ratio Maximum Thickness Ratio r / R P / D 0s(°) x R / D C / D f m / C t m / C 0.7 1 -3.5 -0.033 0.243 0.0213 0.1049 ...
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