View source for 18314414. COWL DAMPER FOR COMBUSTOR simplified abstract (GENERAL ELECTRIC COMPANY)

=COWL DAMPER FOR COMBUSTOR=


==Organization Name==

[[:Category:GENERAL ELECTRIC COMPANY|GENERAL ELECTRIC COMPANY]]


[[Category:GENERAL ELECTRIC COMPANY]]

==Inventor(s)==

[[:Category:Hiranya Nath of Bengaluru (IN)|Hiranya Nath of Bengaluru (IN)]][[Category:Hiranya Nath of Bengaluru (IN)]]

[[:Category:Ravindra Shankar Ganiger of Bengaluru (IN)|Ravindra Shankar Ganiger of Bengaluru (IN)]][[Category:Ravindra Shankar Ganiger of Bengaluru (IN)]]

[[:Category:Sripathi Mohan of Bengaluru (IN)|Sripathi Mohan of Bengaluru (IN)]][[Category:Sripathi Mohan of Bengaluru (IN)]]

[[:Category:Perumallu Vukanti of Bangalore (IN)|Perumallu Vukanti of Bangalore (IN)]][[Category:Perumallu Vukanti of Bangalore (IN)]]

[[:Category:Kwanwoo Kim of Cincinnati OH (US)|Kwanwoo Kim of Cincinnati OH (US)]][[Category:Kwanwoo Kim of Cincinnati OH (US)]]

==COWL DAMPER FOR COMBUSTOR - A simplified explanation of the abstract==


This abstract first appeared for US patent application 18314414 titled 'COWL DAMPER FOR COMBUSTOR

The abstract describes a combustor for a turbomachine engine with a cowl that has an annular shape and a hollow cavity acting as a damper to reduce combustion dynamics.

* The combustor includes a combustion chamber and a cowl with an annular shape.
* The cowl is symmetric around the centerline axis of the turbomachine engine.
* The cowl has a hollow cavity that is in fluid communication with the combustion chamber.
* The hollow cavity acts as a damper to reduce combustion dynamics of the combustor.

Potential Applications:
- Aerospace industry for aircraft engines
- Power generation for gas turbines
- Industrial applications for combustion systems

Problems Solved:
- Reducing combustion dynamics for improved engine performance
- Enhancing stability and efficiency of the combustor

Benefits:
- Improved engine reliability
- Enhanced fuel efficiency
- Reduced emissions

Commercial Applications:
Title: "Innovative Combustor Technology for Turbomachinery"
This technology can be used in aircraft engines, power generation systems, and industrial applications, offering improved performance and efficiency.

Prior Art:
There may be prior art related to combustor designs with dampers or similar features to reduce combustion dynamics in turbomachinery engines.

Frequently Updated Research:
Research on combustion dynamics in turbomachinery engines and the impact of dampers on performance and emissions may be ongoing.

Questions about Combustor Technology:
1. How does the damper in the cowl of the combustor reduce combustion dynamics?
2. What are the specific advantages of using an annular cowl in the combustor design?


==Original Abstract Submitted==

A combustor for a turbomachine engine. The combustor includes a combustion chamber, and a cowl having an annular shape that is symmetric around a centerline axis of the turbomachine engine. The cowl includes a hollow cavity that is in fluid communication with the combustion chamber. The hollow cavity is a damper that reduces combustion dynamics of the combustor.



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