US Patent 8851402 Fuel injection for gas turbine combustors

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Patent

Patent attributes

Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

8851402

Patent Inventor Names

Constantin Dinu0

Mahesh Bathina0

Ramanand Singh0

Date of Patent

October 7, 2014

Patent Application Number

12369808

Date Filed

February 12, 2009

Patent Citations Received

‌

US Patent 11994293 Impingement cooling apparatus support structure and method of manufacture

‌

US Patent 11767766 Turbomachine airfoil having impingement cooling passages

‌

US Patent 11994292 Impingement cooling apparatus for turbomachine

Patent Primary Examiner

‌

Davis Hwu

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