18473368. 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 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 18473368 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 attached to one of the concave portions.
- The outer peripheral cover portion of the gas turbine is designed with concave and convex portions that interact with the combustion cylinders.
- The auxiliary device member is attached to one of the concave portions of the outer peripheral cover portion.
Potential Applications
The technology described in the patent application could be applied in various gas turbine systems, such as power generation plants, aircraft engines, and industrial machinery.
Problems Solved
This innovation helps improve the efficiency and performance of gas turbines by optimizing the airflow and combustion process within the system.
Benefits
- Enhanced efficiency of gas turbines - Improved combustion process - Increased power output
Potential Commercial Applications
The technology could be utilized in power generation plants, aircraft engines, marine propulsion systems, and other industrial applications.
Possible Prior Art
One possible prior art could be the use of similar outer peripheral cover portions in gas turbines, but with different configurations or functionalities.
Unanswered Questions
How does the design of the outer peripheral cover portion impact the overall performance of the gas turbine?
The design of the outer peripheral cover portion plays a crucial role in optimizing airflow and combustion efficiency within the gas turbine system.
What specific benefits does the attachment of the auxiliary device member to the concave portion provide?
The attachment of the auxiliary device member to the concave portion may enhance the functionality or performance of the gas turbine in a specific way that is not explicitly mentioned 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.
