18734374. SHAFT FOR A TURBOMACHINE simplified abstract (General Electric Company)
Contents
SHAFT FOR A TURBOMACHINE
Organization Name
Inventor(s)
Prateek Jalan of Bengaluru (IN)
Kudum Shinde of Bengaluru (IN)
Milind Dhabade of Bengaluru (IN)
Ravindra Shankar Ganiger of Bengaluru (IN)
Tyler F. Hooper of Lynn MA (US)
SHAFT FOR A TURBOMACHINE - A simplified explanation of the abstract
This abstract first appeared for US patent application 18734374 titled 'SHAFT FOR A TURBOMACHINE
Simplified Explanation:
This patent application describes a turbomachine with a turbine rotor, a compressor rotor, and a shaft, along with at least one balance weight assembly connected to the shaft. The balance weight assembly includes chambers and a movable balance weight to help with the rotation of the compressor rotor.
- The turbomachine includes a turbine rotor, a compressor rotor, and a shaft.
- At least one balance weight assembly is connected to the shaft.
- The balance weight assembly includes chambers and a movable balance weight.
- The balance weight helps with the rotation of the compressor rotor.
Potential Applications:
The technology described in this patent application could be used in various turbomachinery applications, such as aircraft engines, power generation systems, and industrial machinery where precise balancing is crucial for efficient operation.
Problems Solved:
This technology addresses the issue of imbalance in turbomachinery, which can lead to reduced efficiency, increased vibrations, and potential damage to the equipment. By incorporating balance weight assemblies, the turbomachine can operate more smoothly and effectively.
Benefits:
The benefits of this technology include improved efficiency, reduced vibrations, extended equipment lifespan, and enhanced overall performance of turbomachinery systems.
Commercial Applications:
With its potential to improve the performance and reliability of turbomachinery, this technology could have significant commercial applications in industries such as aviation, power generation, and manufacturing where turbomachines are essential for various operations.
Questions about Turbomachine Balance Weight Assembly:
1. How does the balance weight assembly contribute to the overall efficiency of the turbomachine? 2. What are the potential challenges in implementing and maintaining balance weight assemblies in turbomachinery systems?
Original Abstract Submitted
A turbomachine including a turbine rotor, a compressor rotor, and a shaft, and at least one balance weight assembly connected to the shaft. The shaft drivingly connects the turbine rotor with the compressor rotor to rotate the compressor rotor about a rotational axis when the turbine rotor rotates about the rotational axis. The at least one balance weight assembly including a first chamber, at least one additional chamber, and a balance weight movable between the first chamber and the at least one additional chamber.
