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US 2014/0227102 A1Published application
Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
AssigneeMTU Aero Engines AG
InventorHarald Schoenenborn
Life of this patent
Estimating the term…
Abstract
A rotor blade for a compressor of a turbomachine is disclosed, the rotor blade having an airfoil having a leading edge, a trailing edge, an airfoil tip, as well as a pressure side and a suction side extending therebetween, provision being made for a profile variation on the pressure side, the profile variation extending into the trailing edge and into the airfoil tip. Also disclosed are a compressor and a turbomachine.
Claims12
1-11. (canceled)
A rotor blade for a compressor of a turbomachine, comprising:
- an airfoil having a leading edge, a trailing edge, and an airfoil tip (12), the airfoil having a pressure side and a suction side extending therebetween, and a profile variation on the pressure side, the profile variation extending into the trailing edge and into the airfoil tip.
Dependencies are inferred from the claim text.