Invention Grant
US09399918B2 Blade for a continuous-flow machine and a continuous-flow machine 有权
用于连续流动机器和连续流动机器的刀片

Blade for a continuous-flow machine and a continuous-flow machine
Abstract:
A blade for a continuous-flow machine is disclosed, especially an aircraft engine, whereby, starting from the middle section, the cross section of the blade tip is reduced with respect to the middle section, at least over a front partial section in the direction of the leading edge and over at least a rear section in the direction of the trailing edge, and a continuous-flow machine having at least one row of blades including such blades is also disclosed.
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