Integral shroud blade design

Details Integral shroud blade design Integral shroud blade design

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/22 (2006.01) F01D 5/16 (2006.01)

Patent

CA 2064361

56,308 ABSTRACT OF THE DISCLOSURE An integral shroud blade comprising a root portion for mounting the blade in a row on a turbine rotor; a platform portion; an airfoil portion extending upwardly from the platform portion and having a leading edge, a trailing edge, and a tip; a shroud formed on the tip of the airfoil portion and having two opposite tangential side surfaces and a top surface; and at least one pair of holes, one hole of each pair being formed in each of the tangential sides of the shroud.

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