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US Patent 8246292 Low noise turbine for geared turbofan engine

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US Patent 12123432 Low noise turbine for geared turbofan engine

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US Patent 11988170 Geared gas turbine engine

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US Patent 11988148 Low noise gas turbine engine

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US Patent 11971052 Modal noise reduction for gas turbine engine

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US Patent 11867195 Gas turbine engine airfoil

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Patent abstract

A gas turbine engine is utilized in combination with a gear reduction to reduce the speed of a fan relative to a low pressure turbine speed. The gas turbine engine is designed such that a blade count in the low pressure turbine multiplied by the speed of the low pressure turbine will result in operational noise that is above a sensitive range for human hearing. A method and turbine module are also disclosed.

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US Patent 11781505 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

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US Patent 11781447 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size

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US Patent 11767856 Gas turbine engine airfoil

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Patent Inventor Names

Bruce L. Morin0

Detlef Korte0

Edits on 13 Sep, 2023

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US Patent 11754094 Modal noise reduction for gas turbine engine

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US Patent 08246292 Low noise turbine for geared turbofan engine US Patent 8246292 Low noise turbine for geared turbofan engine

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Patent Number

08246292

Patent Number

8246292

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US Patent 08246292 Low noise turbine for geared turbofan engine

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Is a

Patent jurisdiction

United States Patent and Trademark Office

Patent number

08246292

Date of patent

August 21, 2012

Patent application number

13403005

Date Filed

February 23, 2012

Patent primary examiner

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