Turboengine blading member
A technology for turbine engines, components, applied in the direction of engine elements, machines/engines, support elements for blades, etc.
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[0049] figure 1A general side view of a turbine engine blade arrangement component 1 as described herein is shown. The blade means 1 comprises an airfoil 2 and a platform 31 arranged at the base of the airfoil 2 . The airfoil 2 comprises a leading edge 21 and a trailing edge 22 . Thus, the hot working fluid flow 4 is expected to flow along the airfoil 2 from the leading edge 21 to the trailing edge 22 and along the working fluid exposed surface 32 of the platform. Typically, attachment features 34 are provided at the coolant side 33 of the platform for attaching the blading member 1 to the rotor or stator. The attachment features are shown in schematic depiction only and are well known features to those skilled in the art. Typically, coolant is provided on the coolant side 33 at the platform 31 during operation of the engine. Said coolant can be used in a manner known per se to cool the platform, but, as is well known to those skilled in the art, can also be directed into ...
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