Moving blade for thermic axial turbomachines
AssigneePolska Akademia Nauk, Instytut Maszyn Przeplywowych
InventorRobert Szewalski
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Abstract
The invention finds application in the manufacture of working blades of a length exceeding that of the blades known so far, without infringing the limitations issuing from flow considerations and strength of the rotor. The blade comprises two different sheets deliminated by a suitably selected intermediary cross section of the blade. Each of the sheets is formed according to a different law dictated by strength and flow considerations. Beginning from the cross-section which delimits the sheets, the sheets are twisted in opposite directions.
Claims1
An axial flow turbomachine rotor blade twisted from root to the tip in order to match fluid angles at entry and exit at different radii, according to a predetermined vortex flow pattern, said blade being tapered simultaneously in order to continuously reduce the cross-section from root to the tip, wherein:
- entry flow angles first diminish continuously from a large value at blade tip down to a minimum value at a predetermined radius of division of the whole blade length into two portions of different vortex-flow patterns, and then said angles increase again down to the root section, and having the exit angle changing continuously from tip to the root in one direction.
Dependencies are inferred from the claim text.