Turbine rotor blade root attachments
A blade root, root technology applied in the direction of blade support elements, engine elements, machines/engines, etc., capable of solving problems such as increased
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[0028] figure 1 and figure 2 Denotes prior art and is described above under the heading "Background". In this design, the stress levels in the disk fingers and blade fingers are equal along the lines of the outer row of pins due to the approximately uniform ratio of disk finger thickness to blade finger thickness. During rotation, the turbine rotor blades experience very large centrifugally induced loads which are reacted by the blade fingers and pins against the disk fingers. As previously mentioned, rotor disk fingers 201 are more susceptible to SCC damage, at least along the outer row of holes 209, than blade fingers 141 made of high alloy steel, since the rotor disk is made of low alloy steel. Made of steel. The concepts disclosed herein reduce the risk of SCC by changing some dimensions of the pinned root fixture, thereby reducing the peak stress exerted by the pins on the disc fingers during disc rotation. image 3 and Figure 4 Dimensional changes due to implement...
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