Adjusted rotating airfoil

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United States of America Patent

PATENT NO 9890790
SERIAL NO

14087935

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A compressor component having an airfoil with a profile in accordance with Table 1 is disclosed. The compressor component, such as a compressor blade, has an increased surface area over a portion of the airfoil chord length. The increased surface area allows for a greater amount of air to be taken in by the airfoil, thus increasing the air flow through the gas turbine engine.

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Patent Owner(s)

  • ANSALDO ENERGIA SWITZERLAND AG

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Digele, Reiner Jochen Biberstein, CH 2 11
Fiebiger, Stephen Wayne Jupiter, US 5 32
Hecker, Wilm Philipp Baden, CH 2 11
Mattheiss, Andreas Martin Baden-Wuerttemberg, DE 2 11
Miller, Edward Len Jupiter, US 6 47
Smith, Wes Carl West Palm Beach, US 2 11

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