Gas turbine engine with an airfoil

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United States of America Patent

PATENT NO 11840939
SERIAL NO

17835091

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A turbine engine includes a compressor section, a combustion section, and a turbine section. Fuel combusted in the combustion section drive stages of airfoils in the turbine section to drive the compressor section. The airfoils can include a geometry near or at the trailing edge with a linear portion provided between the pressure side and a first curved portion, to reduce shock generated in the wake of the airfoils.

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Patent Owner(s)

  • GENERAL ELECTRIC COMPANY

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bhaskaran, Rathakrishnan Niskayuna, US 3 0
Vandeputte, Thomas W Scotia, US 10 108

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