View source for 18452958. COMBUSTOR FUEL NOZZLE ASSEMBLY simplified abstract (General Electric Company)

=COMBUSTOR FUEL NOZZLE ASSEMBLY=


==Organization Name==

[[:Category:General Electric Company|General Electric Company]]


[[Category:General Electric Company]]

==Inventor(s)==

[[:Category:Nayan Vinod Patel of Liberty Township OH (US)|Nayan Vinod Patel of Liberty Township OH (US)]][[Category:Nayan Vinod Patel of Liberty Township OH (US)]]

[[:Category:Michael A. Benjamin of Cincinnati OH (US)|Michael A. Benjamin of Cincinnati OH (US)]][[Category:Michael A. Benjamin of Cincinnati OH (US)]]

==COMBUSTOR FUEL NOZZLE ASSEMBLY - A simplified explanation of the abstract==


This abstract first appeared for US patent application 18452958 titled 'COMBUSTOR FUEL NOZZLE ASSEMBLY

'''Simplified Explanation''': 

This patent application describes a turbine engine with a compressor section, a combustion section, and a turbine section arranged in series. The combustion section includes a combustor with a combustion chamber, a fuel supply connected to the chamber, and a fuel nozzle assembly with air and fuel passages.

'''Key Features and Innovation''':
* Turbine engine with compressor, combustion, and turbine sections in series
* Combustor with combustion chamber and fuel supply
* Fuel nozzle assembly with air and fuel passages

'''Potential Applications''':
The technology can be used in aircraft engines, power generation systems, and other industrial applications requiring efficient combustion processes.

'''Problems Solved''':
This technology addresses the need for improved fuel combustion efficiency and performance in turbine engines.

'''Benefits''':
* Enhanced fuel combustion efficiency
* Improved overall performance of turbine engines
* Potential for reduced emissions

'''Commercial Applications''':
Potential commercial applications include aircraft propulsion systems, power plants, and marine propulsion systems.

'''Prior Art''':
Readers can explore prior patents related to turbine engine combustion systems and fuel injection technologies to understand the existing knowledge in this field.

'''Frequently Updated Research''':
Researchers may find updated studies on fuel combustion technologies, turbine engine efficiency, and combustion chamber design relevant to this technology.

'''Questions about Turbine Engine Combustion Systems''':
1. What are the key components of a turbine engine combustion system?
2. How does the design of fuel nozzles impact combustion efficiency in turbine engines?


==Original Abstract Submitted==

A turbine engine can include a compressor section, a combustion section, and a turbine section in serial flow arrangement. A combustor in the combustion section can include a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly. The fuel nozzle assembly can include an air flow passage and a fuel flow passage.



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