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US Patent 9010085 Turbine section of high bypass turbofan

Patent 9010085 was granted and assigned to United Technologies on April, 2015 by the United States Patent and Trademark Office.

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Patent abstract

A turbofan engine has an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio ratio is below about 170.

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