Turbine blade with squealer tip and densified oxide dispersion strengthened layer

Number of patents in Portfolio can not be more than 2000

United States of America

PATENT NO 11319819
APP PUB NO 20200157951A1
SERIAL NO

16616100

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Abstract

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A blade (10) for a turbine engine that includes an internal cooling system (56) formed from at least one cavity (58) positioned within a generally elongated airfoil (12). A squealer tip (36) and at least one densified oxide dispersion strengthened layer (38) extend radially from a radially outer tip cap (70) of the blade (10), the tip cap (70) having a tip cap upper surface (50).

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Patent Owner(s)

Patent OwnerAddress
SIEMENS ENERGY GLOBAL GMBH & CO KGOTTO-HAHN-RING 6 MÜNCHEN 81739

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Lee, Ching-Pang Cincinnati, US 393 10703
Siw, Sin Chien Oviedo, US 9 5
Tham, Kok-Mun Oviedo, US 39 413
Wong, Li Shing Oviedo, US 11 51

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