Thermal-Responsive Turbine Throttle for Cooling Flow Adjustment

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Solution Overview

Problem

Existing throttle mechanisms for turbines, particularly those using supercritical CO2 media, face challenges in easily adjusting the cross-sectional area of the cooling medium flow path according to operating states, leading to inefficiencies in cooling medium supply, especially during startup and rated operation, due to complex configurations and potential leakage issues.

Innovation Solution

A throttle mechanism that autonomously adjusts the cross-sectional area of the flow path by utilizing materials with different linear expansion coefficients or Young's modulus changes in response to temperature, allowing for self-regulation of the flow path without external actuation, thereby optimizing cooling medium flow based on operational conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a valve driven by an actuator is installed in a pipe to change the cross-sectional area of the flow path, then the cross-sectional area can be adjusted according to operating state, but the configuration becomes more complex and installation space is required

Engineering Contradiction:
Improveadjustability of cross-sectional areaVSAvoidconfiguration complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The flow path forming member utilizes its own thermal expansion or elastic deformation in response to temperature changes to automatically adjust the cross-sectional area of the flow path, eliminating the need for external actuators or complex control mechanisms

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The material properties of the flow path forming member (linear expansion coefficient or Young's modulus) are selected to change in response to temperature, causing the cross-sectional area to adjust automatically according to operating conditions

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If a pipe needs to be installed to penetrate through the turbine casing, then the flow path can be adjusted, but leakage of the working medium may occur and cost may increase

Engineering Contradiction:
Improveadjustability of flow pathVSAvoidleakage prevention
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The flow path adjusting function is merged into the turbine rotor structure itself, with the flow path forming member being an integral part of the rotor that does not require penetration through the turbine casing

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The flow path forming member autonomously adjusts the flow path cross-sectional area through thermal expansion or elastic deformation, eliminating the need for external pipes and actuators that would require sealing through the casing

Inventive Principle:
Principle #25Self-service

3Reliability

If the cross-sectional area is adjusted for rated operation time with large differential pressure, then cooling is effective, but the cooling medium does not easily flow to downstream stages at startup time with small differential pressure

Engineering Contradiction:
Improvecooling effectiveness at rated operationVSAvoidcooling medium flow rate at startup
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The cross-sectional area of the flow path is made dynamic by using a flow path forming member that automatically changes its dimensions in response to temperature variations, allowing the flow area to be large at startup (low temperature) and small at rated operation (high temperature)

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The flow path forming member is made of material with specific linear expansion coefficient that causes the member to expand at high temperatures (reducing flow area) and contract at low temperatures (increasing flow area), automatically adapting to operating conditions

Inventive Principle:
Principle #37Thermal expansion

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The solution enables efficient and autonomous adjustment of the cooling medium flow, ensuring sufficient supply to turbine stages during startup and rated operation, reducing complexity and potential leakage, while maintaining operational efficiency and cost-effectiveness.

Implementation Method 1

making a cross-sectional area of the flow path change autonomously according to temperature

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 2

utilizing materials with different linear expansion coefficients or Young's modulus changes in response to temperature

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS11719116B2Throttle mechanism and turbine
Publication Date: 2023.08.08 TOSHIBA ENERGY SYST & SOLUTIONS CORP
  • US11719116B2 patent drawing
  • US11719116B2 patent drawing
  • US11719116B2 patent drawing

AI summary

There are provided a throttle mechanism and the like that are capable of easily changing a cross-sectional area of a flow path according to an operating state. The throttle mechanism in an embodiment is a throttle mechanism that controls a flow rate of a fluid flowing through a flow path, and is configured to make a cross-sectional area of the flow path change autonomously according to temperature.