ELECTRICITY GENERATION SYSTEM USING A SINGLE-STAGE GAS TURBINE

Abstract

ABSTRACT An electricity generation system (100) using a single-stage gas turbine, comprising: a single-stage turbine configured for power generation; a coolant section integrated within the turbine blades and other components; a coolant distribution system to ensure optimal flow of coolant throughout the turbine; and a control unit for managing the coolant flow and monitoring turbine performance to maintain operational efficiency and prevent thermal damage. <>

Specification

Description:FIELD OF THE DISCLOSURE
[0001] This invention generally relates to a field of gas turbines and, in particular, to a single-stage gas turbine with an efficient coolant section designed to enhance performance and operational efficiency.
BACKGROUND

[0002] The subject matter discussed in the background section should not be assumed to be prior art merely as a result of its mention in the background section. Similarly, a problem mentioned in the background section or associated with the subject matter of the background section should not be assumed to have been previously recognized in the prior art. The subject matter in the background section merely represents different approaches, which in and of themselves may also correspond to implementations of the claimed technology.
[0003] Gas turbines are widely used for power generation and mechanical drive applications due to their high power-to-weight ratio and operational efficiency. Traditional gas turbines typically involve multiple stages of compression and ex , Claims:1. An electricity generation system (100) using a single-stage gas turbine, comprising:
a single-stage turbine configured for power generation;
a coolant section integrated within the turbine blades and other components;
a coolant distribution system to ensure optimal flow of coolant throughout the turbine; and
a control unit for managing the coolant flow and monitoring turbine performance to maintain operational efficiency and prevent thermal damage.

2. The system (100) as claimed in claim 1, wherein the coolant section includes integrated coolant passages within the turbine blades designed to optimize coolant flow and ensure uniform cooling distribution.

3. The system (100) as claimed in claim 1, wherein the control unit directs the flow of coolant to prevent overheating and enhance operational efficiency.

4. The system (100) as claimed in claim 1, wherein the coolant distribution system recirculates the coolant for continuous operation.

Documents