Honda motor co., ltd. (20240110505). GAS TURBINE simplified abstract
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 Unanswered Questions
- 1.11 Original Abstract Submitted
GAS TURBINE
Organization Name
Inventor(s)
Yasuharu Kamoi of Wako-shi (JP)
GAS TURBINE - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240110505 titled 'GAS TURBINE
Simplified Explanation
The gas turbine described in the patent application includes a unique outer peripheral cover portion with concave and convex portions that interact with the combustion cylinders. An auxiliary device member is also attached to one of the concave portions.
- The outer peripheral cover portion of the gas turbine has concave and convex portions that interact with the combustion cylinders.
- An auxiliary device member is attached to one of the concave portions.
Potential Applications
The technology described in the patent application could be applied in gas turbines for power generation, aircraft propulsion, and other industrial applications.
Problems Solved
This innovation helps improve the efficiency and performance of gas turbines by optimizing the airflow and combustion process within the system.
Benefits
The benefits of this technology include increased efficiency, reduced emissions, and improved overall performance of gas turbines.
Potential Commercial Applications
The technology could be commercialized for use in power plants, aircraft engines, marine propulsion systems, and other industrial gas turbine applications.
Possible Prior Art
One possible prior art could be the use of similar outer peripheral cover portions in gas turbines, but the specific design and arrangement described in this patent application may be unique.
Unanswered Questions
How does the arrangement of the concave and convex portions impact the overall efficiency of the gas turbine?
The specific design of the concave and convex portions in relation to the combustion cylinders may play a crucial role in optimizing airflow and combustion processes, but further details on this aspect are not provided in the abstract.
What materials are used in the construction of the outer peripheral cover portion and the auxiliary device member?
The materials used in these components could affect the durability, performance, and cost of the gas turbine, but this information is not specified in the abstract.
Original Abstract Submitted
a gas turbine includes a compressor, a combustor, an air lead-out member, an outer peripheral cover portion, and an auxiliary device member. the outer peripheral cover portion includes outer peripheral concave portions and outer peripheral convex portions, and is formed in a manner so that the outer peripheral concave portions recessed radially inward of the combustor so as to enter between mutually-adjacent combustion cylinders among the plurality of combustion cylinders and the outer peripheral convex portions protruding radially outward of the combustor so as to extend along outer peripheral surfaces of the plurality of combustion cylinders are alternately and continuously arranged in a circumferential direction of the combustor. the auxiliary device member is attached to one of the outer peripheral concave portions.
