Steam Turbine Low-Pressure Section Ventilation Heating Control

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Solution Overview

Problem

Steam turbines face issues with impingement corrosion and temperature-related wear in low-pressure sections, leading to high maintenance costs and limited material options due to ventilation effects during no-load or low-load operations, which impair efficiency and restrict the use of lightweight materials.

Innovation Solution

A steam turbine system with an additional steam inlet device controlled by operating parameters to manage steam supply, reducing temperature and pressure stress in low-pressure sections, allowing for the use of lightweight materials like fiber composites and minimizing ventilation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If low outlet pressure is used to improve efficiency, then energy conversion efficiency is improved, but impingement corrosion and wear of rotor vanes increase

Engineering Contradiction:
Improveenergy conversion efficiencyVSAvoidimpingement corrosion and wear
Core Design Contradiction:
Loss of energyVSObject-affected harmful factors

Solution Approach 1:

The turbine is divided into multiple independent pressure sections (high-pressure, intermediate-pressure, and low-pressure sections) with separate steam inlets. This allows the low-pressure section to operate at optimal low outlet pressure for efficiency while the high-pressure section maintains higher pressure to reduce moisture content and impingement corrosion in the low-pressure section.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

An intermediate-pressure section is introduced between the high-pressure and low-pressure sections. This intermediate section acts as a mediator that progressively reduces steam pressure and moisture content, preventing direct exposure of the low-pressure section to high-moisture steam that causes impingement corrosion.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If specially-coated rotor vanes are used to resist wear, then wear resistance is improved, but maximum application temperature is limited to about 120°C

Engineering Contradiction:
Improvewear resistanceVSAvoidmaximum application temperature
Core Design Contradiction:
ReliabilityVSTemperature

Solution Approach 1:

The rotor vanes are divided into different sections corresponding to different pressure zones. Rotor vanes in the high-pressure section with higher temperatures use materials suitable for high temperature, while rotor vanes in the low-pressure section with lower temperatures can use lightweight materials with lower temperature limits but excellent wear resistance.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The temperature parameter in the low-pressure section is reduced through the multi-section design, allowing the use of materials with lower maximum application temperatures. This enables the use of specially-coated rotor vanes that provide superior wear resistance but can only withstand temperatures up to about 120°C.

Inventive Principle:
Principle #35Parameter changes

3Weight of moving object

If lightweight materials like fiber composites are used for rotor vanes, then weight is reduced, but maximum temperature tolerance is limited

Engineering Contradiction:
Improverotor vane weightVSAvoidmaximum temperature tolerance
Core Design Contradiction:
Weight of moving objectVSTemperature

Solution Approach 1:

Rotor vanes are segmented by location within the turbine. Lightweight fiber composite materials are used specifically in the low-pressure section where temperatures remain below the material's maximum tolerance, while traditional high-temperature materials are used in the high-pressure section.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The temperature parameter in the low-pressure section is controlled to remain within the acceptable range for lightweight fiber composite materials. This parameter change enables the use of these materials in the low-pressure section, achieving weight reduction without exceeding material temperature limits.

Inventive Principle:
Principle #35Parameter changes

4Ease of operation

If ventilation heating occurs in low-pressure section during no-load operation, then temperature increases to 200-250°C or more, but material options for rotor vanes are restricted

Engineering Contradiction:
Improveno-load operation capabilityVSAvoidmaterial selection flexibility
Core Design Contradiction:
Ease of operationVSAdaptability or versatility

Solution Approach 1:

The harmful ventilation heating effect is extracted and isolated to specific sections. By providing separate steam inlets and controlling steam flow to different pressure sections independently, the ventilation effect that causes excessive temperature rise is eliminated or reduced in the low-pressure section during no-load operation.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The temperature parameter in the low-pressure section during no-load operation is controlled to remain below the maximum tolerance of lightweight materials. This is achieved by adjusting steam flow parameters and preventing excessive ventilation heating, thereby expanding material selection flexibility.

Inventive Principle:
Principle #35Parameter changes

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 extends the service life of turbine components, reduces maintenance costs, and enables the use of lightweight materials by controlling steam supply to prevent temperature increases, thereby enhancing efficiency and operational flexibility.

Implementation Method 1

the thermal energy from steam supplied to the turbine is converted into mechanical work

Methodology Applied
Scientific EffectThermal energy conversion:

Implementation Method 2

The temperature and the pressure of the steam are reduced in the route between steam inlet and steam outlet during this conversion

Methodology Applied
Scientific EffectSteam expansion:

Implementation Method 3

moisture that has condensed out of the steam can precipitate and form water droplets in the turbine

Methodology Applied
Scientific EffectCondensation: Condensation

Implementation Method 4

Water droplets entrained by the flow of steam collide with the rotating rotor vanes with a high level of energy so the vanes are subject to corresponding wear

Methodology Applied
Scientific EffectImpingement corrosion:

Implementation Method 5

the steam in the low-pressure section (for example end stage), which has already been extensively expanded and cooled in preceding turbine sections, is heated again by the rotating rotor vanes

Methodology Applied
Scientific EffectVentilation heating:

Data Source

PatentUS8770914B2Steam turbine system and method for operating a steam turbine
Publication Date: 2014.07.08 SIEMENS ENERGY GLOBAL GMBH & CO KG
  • US8770914B2 patent drawing
  • US8770914B2 patent drawing
  • US8770914B2 patent drawing

AI summary

A steam turbine system including a steam turbine is provided. The steam turbine system includes a high-pressure side steam inlet device, a low-pressure side steam device, and a control device for controlling the steam turbine. An additional steam inlet device is also included arranged between the high-pressure side steam inlet device and the low-pressure side steam device. The control device control a supply of steam via the additional steam inlet device as a function of operating parameters detected at the steam turbine system.