18054177. GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES simplified abstract (Honeywell International Inc.)
Contents
- 1 GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Unanswered Questions
- 1.11 Original Abstract Submitted
GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES
Organization Name
Inventor(s)
Rodolphe Dudebout of Phoenix AZ (US)
GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES - A simplified explanation of the abstract
This abstract first appeared for US patent application 18054177 titled 'GASEOUS FUEL NOZZLE FOR USE IN GAS TURBINE ENGINES
Simplified Explanation
The gaseous fuel nozzle described in the abstract includes a main body with inner air injection passages, outer air injection passages, and gaseous fuel injection passages. The gaseous fuel injection outlet ports are arranged concentrically around an axis of symmetry between the inner and outer air injection outlet ports.
- The gaseous fuel nozzle has a main body.
- It includes inner air injection passages with inlet and outlet ports.
- It also has outer air injection passages with inlet and outlet ports.
- The gaseous fuel nozzle features gaseous fuel injection passages with inlet and outlet ports.
- The gaseous fuel injection outlet ports are positioned concentrically around an axis of symmetry.
- They are located between the inner air injection outlet ports and the outer air injection outlet ports.
Potential Applications
The technology could be applied in gas turbine engines, industrial burners, and other combustion systems where precise fuel and air mixing is crucial.
Problems Solved
This innovation solves the challenge of efficiently mixing gaseous fuel with inner and outer air streams in a nozzle configuration, improving combustion efficiency and reducing emissions.
Benefits
The benefits of this technology include enhanced combustion performance, increased fuel efficiency, reduced emissions, and improved overall system reliability.
Potential Commercial Applications
Potential commercial applications of this technology include aerospace propulsion systems, power generation plants, and industrial heating processes.
Possible Prior Art
One possible prior art could be traditional fuel nozzles with less efficient fuel and air mixing capabilities, leading to lower combustion efficiency and higher emissions.
Unanswered Questions
How does this technology compare to existing fuel nozzle designs in terms of performance and efficiency?
The article does not provide a direct comparison with existing fuel nozzle designs to assess performance and efficiency differences.
What are the potential challenges in implementing this technology in different combustion systems?
The article does not address the potential challenges that may arise when implementing this technology in various combustion systems, such as compatibility issues or installation complexities.
Original Abstract Submitted
A gaseous fuel nozzle includes a main body, a plurality of inner air injection passages having inlet and outlet ports, a plurality of outer air injection passages having inlet and outlet ports, and a plurality of gaseous fuel injection passages having inlet and outlet ports. At least the gaseous fuel injection outlet ports are disposed concentrically about an axis of symmetry and between the plurality of inner air injection nozzle outlet ports and the plurality of outer air injection nozzle outlet ports.
