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US Patent 12111056 Combustor with central fuel injection and downstream air mixing

Patent 12111056 was granted and assigned to Pratt & Whitney Canada on October, 2024 by the United States Patent and Trademark Office.

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Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent
1

Patent attributes

Patent Applicant
Pratt & Whitney Canada
Pratt & Whitney Canada
1
Current Assignee
Pratt & Whitney Canada
Pratt & Whitney Canada
1
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
1
Patent Number
121110561
Patent Inventor Names
Hang Xu1
Date of Patent
October 8, 2024
1
Patent Application Number
181049901
Date Filed
February 2, 2023
1
Patent Citations
‌
US Patent 7762073 Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports
1
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US Patent 6865889 Method and apparatus to decrease combustor emissions
1
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US Patent 7117678 Fuel injector head
1
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US Patent 7762070 Pilot nozzle heat shield having internal turbulators
1
‌
US Patent 9771869 Nozzle system and method for starting and operating gas turbines on low-Btu fuels
1
‌
US Patent 9909597 Supersonic compressor with separator
1
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US Patent 9951955 Annular combustion chamber for a turbine engine
1
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US Patent 9976522 Fuel injector for combustion engine and staged fuel delivery method
1
...
Patent Primary Examiner
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Craig Kim
1
CPC Code
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F02C 7/22
1
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F05D 2240/35
1
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F23D 17/002
1
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F23R 3/28
1
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F23R 3/286
1
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F23R 3/14
1
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F23R 3/343
1
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F23R 3/06
1
...
Patent abstract

A combustor has a mixing body with a central fuel passage with a central axis and adapted to be connected to source of fuel. A nose at a forward end includes a plurality of fuel injection passages allowing fuel to flow from the central fuel passage into an area forward of an outlet from the fuel injection passages. An inner air supply radially outwardly of the central fuel passage delivers air into inner slots extending downstream of outlets of the fuel injection passages such that air and fuel can begin to be mixed and move downstream of an end of the nose. An outer air supply delivers air downstream of the inner air outlet such that air from the outer air supply, air from the inner slots and fuel from the fuel injection passages are all driven forwardly into a combustion chamber. A gas turbine engine is also disclosed.

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