Honda motor co., ltd. (20240110703). GAS TURBINE simplified abstract
Contents
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 20240110703 titled 'GAS TURBINE
Simplified Explanation
The gas turbine described in the patent application includes a combustor, an air lead-out member, an outer peripheral cover portion, an inner peripheral cover portion, and a fuel supply unit. The combustor features a guide wall portion that connects adjacent combustion cylinders and guides air from an air flow path to an inner space via a communication path. Through holes in the outer peripheral surface of the combustion cylinders allow air in the inner space to flow into the downstream side of a combustion chamber.
- Combustor with guide wall portion connecting combustion cylinders
- Through holes in combustion cylinders for air flow
- Air lead-out member with lead-out port radially outward of combustor end
- Fuel supply unit for combustion process
Potential Applications
The technology described in this patent application could be applied in gas turbines for power generation, aircraft propulsion, and other industrial applications requiring efficient combustion processes.
Problems Solved
This innovation solves the problem of optimizing air flow within a gas turbine combustor to enhance combustion efficiency and overall performance.
Benefits
The benefits of this technology include improved fuel efficiency, reduced emissions, and increased power output in gas turbine systems.
Potential Commercial Applications
Potential commercial applications for this technology include gas turbine power plants, aircraft engines, and other industrial combustion systems.
Possible Prior Art
One possible prior art for this technology could be similar gas turbine combustor designs with guide wall portions and through holes for air flow optimization.
Unanswered Questions
How does this technology compare to existing gas turbine combustor designs in terms of efficiency and performance?
This article does not provide a direct comparison with existing gas turbine combustor designs to evaluate efficiency and performance improvements.
What are the potential challenges in implementing this technology in existing gas turbine systems?
The article does not address the potential challenges or modifications required to integrate this technology into current gas turbine systems.
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.
