Airfoil for a compressor blade

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United States of America Patent

PATENT NO 9291059
APP PUB NO 20110150660A1
SERIAL NO

12646561

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Abstract

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The present disclosure provides an improved first stage airfoil for a compressor blade having a unique chord length (CD), stagger angle (γ) and camber angle (Δβ). The stagger angle (γ) and camber angle (Δβ) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight.

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Patent Owner(s)

Patent OwnerAddress
GENERAL ELECTRIC TECHNOLOGY GMBH5400 BADEN

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Dunkel, Gabriel Birr, CH 3 51
Kappis, Wolfgang Fislisbach, CH 25 270
Micheli, Marco Schoefflisdorf, CH 18 217
Puerta, Luis Frederico Rieden, CH 2 68

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