Variable Volume Turbine Case Clearance Control

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Solution Overview

Problem

Gas turbine engines face challenges in maintaining a consistent radial tip clearance due to thermal expansion and contraction, which affects engine performance across varying operational conditions.

Innovation Solution

An active clearance control system using a radially adjustable Blade Outer Air Seal (BOAS) system with an accumulator system that includes a pneumatic cylinder and a movable piston to maintain a constant volume between air seal segments and the engine case structure, allowing for passive operation and controlled movement to adjust tip clearance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If hydraulic cylinders and pistons are used for active tip clearance control, then radial tip clearance can be adjusted, but the device complexity and size increase

Engineering Contradiction:
Improveradial tip clearance controlVSAvoidpositioning mechanism complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent extracts the active clearance control function from complex hydraulic positioning mechanisms and implements it through a simplified thermal control system using heated air or gas flow. The thermal expansion of the shroud assembly is controlled by directing hot gas from the turbine to specific regions, eliminating the need for hydraulic cylinders and pistons while maintaining radial tip clearance adjustment capability

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent replaces the mechanical hydraulic positioning system with a thermal field-based control system. Instead of using mechanical force from hydraulic actuators to adjust blade tip clearance, the system uses thermal expansion and contraction of the shroud assembly controlled by heated gas flow, substituting a mechanical system with a thermal field system

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If radial tip clearance is designed for high power operations, then blade tips do not rub against air seal, but clearance increases when engine power is reduced

Engineering Contradiction:
Improveblade tip clearance stabilityVSAvoidengine performance
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent implements a dynamic clearance control system where the shroud assembly's thermal state is continuously adjusted based on engine operating conditions. By controlling the flow of heated gas to specific regions of the shroud, the system dynamically adjusts thermal expansion to maintain optimal radial tip clearance across varying power levels, transitioning from a static design to a dynamic control system

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent changes the thermal parameters of the shroud assembly by controlling the temperature and flow of heated gas applied to different regions. By varying these thermal parameters in response to engine power changes, the system maintains consistent radial tip clearance despite changes in engine operating conditions, preventing both blade rub and excessive clearance

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 maintains a consistent radial tip clearance, reducing the need for larger actuators and improving engine performance by accommodating thermal changes and operational variations.

Implementation Method 1

the thermal environment in the engine varies and may cause thermal expansion and contraction such that the radial tip clearance varies

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 2

an active clearance control system using a radially adjustable Blade Outer Air Seal (BOAS) system with an accumulator system that includes a pneumatic cylinder and a movable piston

Methodology Applied
Scientific EffectPneumatic pressure: Pressure Increase

Data Source

PatentEP2984297B1Gas turbine engine rapid response clearance control system with variable volume turbine case
Publication Date: 2020.04.01 UNITED TECH CORP
  • EP2984297B1 patent drawingFigure 1
  • EP2984297B1 patent drawingFigure 2
  • EP2984297B1 patent drawingFigure 3

AI summary

An active clearance control system of a gas turbine engine includes a radially adjustable blade outer air seal system movable between a radially contracted Blade Outer Air Seal (BOAS) position that defines a first air volume and a radially expanded Blade Outer Air Seal (BOAS) position that defines a second air volume, the second air volume different than the first air volume. An accumulator system accommodate a difference in air volume between the first air volume and the second air volume.