Turbine blade assembly
A technology of blades and components, applied in the direction of supporting elements of blades, engine elements, machines/engines, etc., which can solve the problems of increased cost of turbomachinery
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[0015] figure 1 Illustrated in is one embodiment of a rotor assembly 10 for use in, for example, a turbine of a turbomachine. The rotor assembly 10 includes a plurality of blade assemblies 12 secured to the rotor 14 at the periphery of the rotor 14 via, for example, a plurality of tenon attachment means 16 .
[0016] see figure 2 As shown in the exploded view, the blade assembly 12 includes an airfoil section 18 and an attachment section 20 . Airfoil segment 18 includes an airfoil 22 and, in some embodiments, a platform 24 that defines an annular flow path for rotor 14 . Airfoil segments 18 may be formed from a variety of materials that are well suited to the high temperature environments in which many rotors 14 operate. For example, airfoil segment 18 may be formed from a ceramic matrix composite (CMC) or a single crystal alloy. Attachment section 20 is formed separately from airfoil section 18 and may be formed from a different material than that used in airfoil section...
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