Compressor blade of a gas turbine as well as method for manufacturing said blade

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United States of America Patent

PATENT NO 9828860
APP PUB NO 20140030106A1
SERIAL NO

13953944

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A compressor blade of a gas turbine includes an airfoil made of a fiber-reinforced plastic and a leading-edge element connected to said airfoil. The leading-edge element includes two partial elements, which are fabricated as separate elements and connected to one another, with the leading-edge element being connected to the airfoil essentially using the clamping effect of the two partial elements.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE DEUTSCHLAND LTD & CO KGESCHENWEG 11 OT DAHLEWITZ 15827 BLANKENFELDE-MAHLOW 15827

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Schreiber, Karl Am Mellensee, DE 50 314

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