TURBOMACHINE BLADE PRODUCTION METHOD
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United States of America Patent
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Issued Date -
Aug 28, 2014
app pub date -
Feb 28, 2014
filing date -
Feb 28, 2013
priority date (Note) -
Abandoned
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Abstract
A method of producing a turbomachine blade having a coupling root, and an airfoil-shaped oblong member cantilevered from the coupling root; the airfoil-shaped oblong member having a main plate-like element connected directly to the coupling root, and a cover plate for sealing a hollow weight-reducing seat formed in one of the two major faces of the main plate-like element; the main plate-like element being divided into a lower connecting fin cantilevered from the coupling root, and a plate-like body butt welded to the lower connecting fin to form an extension of the lower connecting fin; the method being characterized by including the steps of twisting and curving a flat plate of constant thickness greater than the maximum thickness of the plate-like body of the blade, to obtain a blank plate, in which the three-dimensional shape of the centerline surface of the blank plate substantially matches the three-dimensional shape of the centerline surface of the plate-like body of the main plate-like element.
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