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Propfan turbo-engine |
 | | In particular, the relatively large hub ratio of the propfan blades, thus the ratio of the inside diameter of the blade to the outside diameter of the blade, is disadvantageously large, since, for aerodynamic reasons, the working turbine must have a certain minimum diameter. |
 | | It is also a disadvantage in the above-noted propfan turbo-engine, that the approach flow conditions of the propfan blades, as a result of the gas turbine body, which is arranged upstream of the propfan blades, during normal flight, are disturbed at least in proximity of the hub of the propfan. |
 | | In the present case, i.e., in the case of the contra-rotating propfan with a shroud, the approach flow Mach number is set by the contour of the shroud and the design of the propfan rotors, i.e., it is independent of the flying speed. |
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