18472516. GAS TURBINE simplified abstract (HONDA MOTOR CO., LTD.)
Contents
- 1 GAS TURBINE
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 GAS TURBINE - 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 How does this technology compare to existing gas turbine designs in terms of efficiency and emissions reduction?
- 1.11 What are the potential challenges in implementing this technology on a large scale in industrial applications?
- 1.12 Original Abstract Submitted
GAS TURBINE
Organization Name
Inventor(s)
Yasuharu Kamoi of Wako-shi (JP)
Tomoki Shiota of Wako-shi (JP)
Manamu Nishimoto of Wako-shi (JP)
GAS TURBINE - A simplified explanation of the abstract
This abstract first appeared for US patent application 18472516 titled 'GAS TURBINE
Simplified Explanation
The gas turbine described in the patent application includes a combustor with a guide wall portion, an air lead-out member with a lead-out port, outer and inner peripheral cover portions, and a fuel supply unit. Through holes are formed in the outer peripheral surface of each combustion cylinder to allow air in the inner space to flow into the downstream side of a combustion chamber.
- The gas turbine includes a combustor with a guide wall portion connecting combustion cylinders.
- Through holes in the combustion cylinders allow air to flow into the combustion chamber.
Potential Applications
The technology described in the patent application could be applied in gas turbine engines for power generation, aircraft propulsion, and other industrial applications.
Problems Solved
This technology helps improve combustion efficiency and airflow distribution within the gas turbine, leading to better performance and reduced emissions.
Benefits
The benefits of this technology include increased efficiency, improved combustion stability, and reduced environmental impact due to lower emissions.
Potential Commercial Applications
Potential commercial applications of this technology include power plants, aircraft engines, marine propulsion systems, and other industrial gas turbine applications.
Possible Prior Art
One possible prior art for this technology could be similar gas turbine designs with combustion cylinders and guide walls for airflow control.
Unanswered Questions
How does this technology compare to existing gas turbine designs in terms of efficiency and emissions reduction?
The article does not provide a direct comparison with existing gas turbine designs in terms of efficiency and emissions reduction.
What are the potential challenges in implementing this technology on a large scale in industrial applications?
The article does not address the potential challenges in implementing this technology on a large scale in industrial applications.
Original Abstract Submitted
A gas turbine includes a combustor, an air lead-out member, an outer peripheral cover portion, an inner peripheral cover portion, and a fuel supply unit. A lead-out port of the air lead-out member is located radially outward of one end portion of the combustor. The combustor has a guide wall portion which is formed so as to connect mutually-adjacent combustion cylinders and guides air from an air flow path to an inner space via a communication path. Through holes are formed in the outer peripheral surface of each of the combustion cylinders and open to the inner space to allow air in the inner space to flow into the downstream side of a combustion chamber.
