Turbine Thrust Control via Dynamic Packing Seal Clearance

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Solution Overview

Problem

Turbine systems face instability due to thrust pressures that can approach zero, leading to mechanical stress issues on thrust fittings, which are designed to handle directional thrust but not well-suited for rapid directional changes, particularly under high temperatures and pressures.

Innovation Solution

A control system that includes a controller and sensor to move packing seals to specific clearance positions in response to thrust pressures exceeding target levels, ensuring net positive or negative thrust is maintained, thereby stabilizing the turbine system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If thrust pressure is allowed to approach zero for efficient turbine operation, then operating efficiency is improved, but mechanical stability deteriorates due to inability of thrust fittings to handle rapid directional changes

Engineering Contradiction:
Improveoperating efficiencyVSAvoidmechanical stability
Core Design Contradiction:
ProductivityVSStability of the object's composition

Solution Approach 1:

A controller is introduced as an intermediary between the thrust pressure source and the packing seal. The controller receives thrust pressure measurements and automatically adjusts the packing seal position to maintain stable thrust conditions, eliminating the need for manual intervention while preventing mechanical instability during efficient operation

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

A feedback mechanism is implemented where a sensor continuously measures thrust pressure and feeds this information to the controller. The controller then adjusts the packing seal position based on the measured thrust pressure, creating a closed-loop control system that maintains stability while allowing efficient operation at optimized thrust pressures

Inventive Principle:
Principle #23Feedback

2Reliability

If packing seal clearance is reduced to control thrust pressure, then thrust pressure control is improved, but mechanical stress on thrust fitting increases

Engineering Contradiction:
Improvethrust pressure controlVSAvoidmechanical stress on thrust fitting
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The packing seal position is made dynamically adjustable rather than fixed. The controller can modify the clearance position in real-time based on operating conditions, allowing optimization of thrust pressure control while preventing excessive mechanical stress by adjusting clearance as needed

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The clearance position parameter of the packing seal is changed dynamically by the controller based on measured thrust pressure. By adjusting this geometric parameter, the system achieves reliable thrust pressure control while avoiding conditions that would create excessive mechanical stress on the thrust fitting

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 system effectively manages thrust pressures, preventing instability and mechanical stress on turbine components by dynamically adjusting packing seal positions, ensuring operational stability within permissible temperature and pressure limits.

Implementation Method 1

a sensor coupled to the controller and configured to detect the thrust pressure

Methodology Applied
Scientific EffectPressure detection:

Implementation Method 2

a pressure drop across the packing seal exceeding a target pressure drop; wherein the selected clearance position causes one of a net positive thrust and a net negative thrust against the thrust fitting

Methodology Applied
Scientific EffectPressure drop: Pressure Drop

Implementation Method 3

This thrust force can be created through a combination of the fluid inertia acting on the turbine buckets, and the pressure developed by variation in cross-sectional area acting against portions of the system

Methodology Applied
Scientific EffectFluid inertia: Inertia

Data Source

PatentUS9341073B2Turbine thrust control system
Publication Date: 2016.05.17 GE INFRASTRUCTURE TECH LLC
  • US9341073B2 patent drawing
  • US9341073B2 patent drawing
  • US9341073B2 patent drawing

AI summary

Systems and programs for controlling thrust in a turbine by adjusting the clearance between a packing seal and a rotating component are disclosed. In one embodiment, a system includes a controller configured to move a packing seal to a selected clearance position in response to a thrust pressure exceeding a target pressure, and a sensor coupled to the controller and configured to detect the thrust pressure.