View source for 18314418. COMPONENTS FOR COMBUSTOR simplified abstract (GENERAL ELECTRIC COMPANY)

=COMPONENTS FOR COMBUSTOR=


==Organization Name==

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


[[Category:GENERAL ELECTRIC COMPANY]]

==Inventor(s)==

[[:Category:Karthikeyan Sampath of Bengaluru (IN)|Karthikeyan Sampath of Bengaluru (IN)]][[Category:Karthikeyan Sampath of Bengaluru (IN)]]

[[:Category:Rimple Rangrej of Bengaluru (IN)|Rimple Rangrej of Bengaluru (IN)]][[Category:Rimple Rangrej of Bengaluru (IN)]]

[[:Category:Pradeep Naik of Bengaluru (IN)|Pradeep Naik of Bengaluru (IN)]][[Category:Pradeep Naik of Bengaluru (IN)]]

[[:Category:Saket Singh of Bengaluru (IN)|Saket Singh of Bengaluru (IN)]][[Category:Saket Singh of Bengaluru (IN)]]

[[:Category:Deepak Ghiya of Bengaluru (IN)|Deepak Ghiya of Bengaluru (IN)]][[Category:Deepak Ghiya of Bengaluru (IN)]]

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

==COMPONENTS FOR COMBUSTOR - A simplified explanation of the abstract==


This abstract first appeared for US patent application 18314418 titled 'COMPONENTS FOR COMBUSTOR

The patent application describes a combustor for a turbomachine engine that includes a component with a porous structure to reduce combustion dynamics and improve backflow margin of cooling air.

* The component in the combustor has a porous structure defining multiple channels to act as a damper, reducing combustion dynamics.
* A support structure positioned between the diffuser and the combustor component also has a porous structure with multiple channels to improve the backflow margin of cooling air by reducing turbulence.

Potential Applications:
- Aerospace industry for turbomachine engines
- Gas turbines
- Power generation systems

Problems Solved:
- Reducing combustion dynamics in a combustor
- Improving backflow margin of cooling air

Benefits:
- Enhanced engine performance
- Increased efficiency
- Improved durability of components

Commercial Applications:
- Aircraft engines
- Industrial gas turbines
- Power plants

Prior Art:
- Previous patents related to combustor components and support structures in turbomachine engines.

Frequently Updated Research:
- Ongoing studies on combustor design for turbomachine engines and their impact on engine performance.

Questions about Combustor for Turbomachine Engine:
1. How does the porous structure of the component reduce combustion dynamics?
2. What are the specific benefits of improving the backflow margin of cooling air in a turbomachine engine?


==Original Abstract Submitted==

In one aspect, a combustor for a turbomachine engine includes a combustion chamber and a component in operable flow with the combustion chamber. The component has a porous structure that defines multiple channels, that are adapted to configure the component as a damper to reduce combustion dynamics of the combustor. In another aspect, a combustor of a turbomachine engine includes a diffuser, a combustor component positioned aft of the diffuser to receive cooling air therefrom, and a support structure in operable flow with the diffuser and the combustor component and positioned therebetween. The support structure has a porous structure that defines multiple channels, which are adapted to improve a backflow margin of the cooling air by reducing turbulence of the cooling air.



[[Category:F23R3/00]]
[[Category:F23R3/60]]
[[Category:CPC_F23R3/002]]