Stator Shroud Mechanical Retention for Gas Turbine Vane Damping

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Solution Overview

Problem

Stator vanes in gas turbine engines often deviate from optimal aerodynamic shapes due to rigid fixation, leading to aeromechanical tuning issues that affect their performance.

Innovation Solution

The use of an arcuate shroud with a shroud pocket and a strap to retain stator vanes, along with potting material, such as rubber, to allow for aerodynamic optimization and secondary retention by straps, enabling the use of different materials for vanes and shrouds for weight reduction and improved damping.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If stator vanes are rigidly fixed to the shroud, then structural stability is improved, but aerodynamic performance deteriorates due to deviation from optimal aerodynamic shape

Engineering Contradiction:
Improvestructural stabilityVSAvoidaerodynamic shape
Core Design Contradiction:
Stability of the object's compositionVSShape

Solution Approach 1:

The patent transitions from rigid fixation to a dynamic retention system using flexible straps and potting material that allow the stator vane to maintain its aerodynamic shape while providing sufficient retention. The flexible strap and compliant potting material enable the vane to assume its optimal aerodynamic configuration without rigid constraints.

Inventive Principle:
Principle #15Dynamics

2Strength

If metal materials are used for both vanes and shrouds, then strength is improved, but weight increases

Engineering Contradiction:
ImprovestrengthVSAvoidweight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent employs composite material selection where stator vanes can be made from lighter materials (such as composites or different alloys) while the metal shroud provides the necessary structural strength. The flexible strap and potting material system enables this material differentiation by providing retention without requiring both components to be made from high-strength metal.

Inventive Principle:
Principle #40Composite materials

3Ease of manufacture

If rigid fixation is used, then manufacturing simplicity is improved, but vibrational damping deteriorates

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidvibrational damping
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The patent changes the physical parameters of the retention system by introducing flexible straps and compliant potting material instead of rigid fixation. This parameter change enables adequate vibrational damping while maintaining manufacturing feasibility through standardized flexible retention components.

Inventive Principle:
Principle #35Parameter changes

4Stability of the object's composition

If aeromechanical tuning is applied to rigidly fixed vanes, then structural integrity is improved, but aerodynamic efficiency deteriorates

Engineering Contradiction:
Improvestructural integrityVSAvoidaerodynamic efficiency
Core Design Contradiction:
Stability of the object's compositionVSProductivity

Solution Approach 1:

The patent resolves this contradiction by implementing a dynamic retention system that allows the stator vane to achieve and maintain its optimal aerodynamic shape without rigid constraints. The flexible strap and potting material provide sufficient retention while permitting the vane to operate at its aerodynamic optimum, eliminating the need for compromising aeromechanical tuning.

Inventive Principle:
Principle #15Dynamics

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

This configuration allows for the formation of stator vanes in an aerodynamically optimized shape, providing necessary vibrational damping and reducing weight by enabling the use of composite materials for vanes while maintaining structural integrity with metal shrouds, enhancing overall engine performance.

Implementation Method 1

enabling the use of different materials for vanes and shrouds for weight reduction and improved damping

Methodology Applied
Scientific EffectVibrational damping: Damping

Data Source

PatentUS10472979B2Stator shroud with mechanical retention
Publication Date: 2019.11.12 RTX CORP
  • US10472979B2 patent drawing
  • US10472979B2 patent drawing
  • US10472979B2 patent drawing

AI summary

A stator assembly for a gas turbine engine includes an arcuate shroud including a shroud pocket, the shroud pocket having a shroud slot extending therethrough. A stator vane is insertable into the shroud pocket and includes a vane slot extending therethrough. A strap extends through the shroud slot and the vane slot to retain the vane to the shroud. A gas turbine engine includes a combustor and a stator and case assembly in in fluid communication with the combustor. The stator and case assembly includes a case defining a working fluid flowpath for the gas turbine engine and a stator assembly secured at the case.