View source for General electric company (20240280265). COMBUSTOR FUEL NOZZLE ASSEMBLY simplified abstract

=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 20240280265 titled 'COMBUSTOR FUEL NOZZLE ASSEMBLY

The abstract describes a turbine engine with a compressor section, a combustion section, and a turbine section in a serial flow arrangement. The combustor in the combustion section includes a combustion chamber, a fuel supply fluidly coupled to the combustion chamber, and a fuel nozzle assembly with an air flow passage and a fuel flow passage.

* The turbine engine features a compressor section, a combustion section, and a turbine section in a serial flow arrangement.
* The combustor in the combustion section includes a combustion chamber for fuel combustion.
* A fuel supply is fluidly coupled to the combustion chamber for efficient fuel delivery.
* The fuel nozzle assembly comprises an air flow passage for combustion air and a fuel flow passage for fuel injection.
* This design enhances the efficiency and performance of the turbine engine.

Potential Applications:
- Aircraft propulsion systems
- Power generation plants
- Marine propulsion systems

Problems Solved:
- Improved fuel combustion efficiency
- Enhanced overall performance of the turbine engine

Benefits:
- Increased fuel efficiency
- Higher power output
- Reduced emissions

Commercial Applications:
Title: Advanced Turbine Engine Technology for Enhanced Performance
This technology can be utilized in aircraft engines, power plants, and marine propulsion systems, offering improved efficiency and performance in various commercial applications.

Prior Art:
Readers can explore prior patents related to turbine engine combustors, fuel injection systems, and combustion chamber designs to gain a deeper understanding of the technological advancements in this field.

Frequently Updated Research:
Researchers are constantly working on optimizing fuel injection systems and combustion chamber designs to further enhance the efficiency and performance of turbine engines.

Questions about Turbine Engine Technology:
1. How does the design of the fuel nozzle assembly impact fuel combustion efficiency?
   - The design of the fuel nozzle assembly plays a crucial role in ensuring proper fuel-air mixing for efficient combustion.
2. What are the key factors influencing the performance of the turbine engine in this configuration?
   - Factors such as fuel delivery, combustion chamber design, and turbine efficiency significantly impact the overall performance of the turbine engine.


==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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