Curved Gas Turbine Blade Root Attachment for Stress Distribution

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Solution Overview

Problem

Existing gas turbine engine blade attachment systems face challenges in effectively managing loadings and stress distribution during operation, leading to inefficiencies and potential structural issues.

Innovation Solution

The introduction of a gas turbine engine blade with a circumferentially curved root attachment featuring a variable curvature design, which includes a first curvature in the forward portion and a second curvature in the rearward portion, allowing for sliding reception within a wheel slot, and incorporating a lobed feature to prevent radial removal, thereby balancing stresses and enhancing attachment security.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional blade attachment system is used, then the blade can be attached to the wheel, but the stress distribution is uneven leading to potential structural failure

Engineering Contradiction:
Improvestructural integrityVSAvoidstress distribution
Core Design Contradiction:
ReliabilityVSStress or pressure

Solution Approach 1:

The blade root attachment feature employs a curved profile with variable radius of curvature, transitioning from a first radius in the forward portion to a second radius in the rearward portion. This curvature design allows the blade root to conform to the wheel slot geometry, distributing contact stresses more uniformly across the attachment interface and preventing stress concentration that could lead to structural failure.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The attachment feature incorporates different radii of curvature at different locations along the blade root - a first radius for the forward portion and a second radius for the rearward portion. This localized variation in geometric properties optimizes stress distribution at each specific location, with the curvature tailored to match the local wheel slot geometry and loading conditions.

Inventive Principle:
Principle #3Local quality

2Reliability

If a curved root attachment is used, then stress balance is improved, but the manufacturing complexity increases

Engineering Contradiction:
Improvestress balanceVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The curved profile with variable radius is integrated into the blade casting or manufacturing process as a continuous geometric feature. By defining the root attachment geometry through mathematical curvature parameters (first radius, second radius, transition point), the design achieves complex stress-distributing geometry that can be manufactured using modern additive manufacturing or precision casting techniques, balancing manufacturing feasibility with performance requirements.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Reliability

If the blade root is designed with variable curvature, then the attachment security is enhanced, but the device complexity increases

Engineering Contradiction:
Improveattachment securityVSAvoidroot geometry complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The variable curvature profile is defined by a systematic transition from a first radius of curvature to a second radius of curvature along the blade root length. This mathematical definition provides attachment security through optimized contact geometry while maintaining design simplicity through parameter-based specification rather than complex multi-component construction.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The root attachment geometry is characterized by varying key parameters - specifically the radius of curvature - along the length of the blade root. This parameter variation (from first radius to second radius) enables the geometry to adapt to different loading conditions and wheel slot configurations, enhancing attachment security through controlled geometric progression rather than fixed rigid forms.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP2971523B1Attachment feature of a gas turbine engine blade having a curved profile
Publication Date: 2018.11.14 ROLLS ROYCE CORP
  • EP2971523B1 patent drawingFigure 1~2
  • EP2971523B1 patent drawingFigure 3
  • EP2971523B1 patent drawingFigure 4

AI summary

An airfoil member is disclosed having an attachment feature such as a fir tree or dovetail design that includes a curved profile formed from a combination of curves. In one embodiment, the curved profile can be a compound curve formed by a forward curve and a rearward curve that are joined at a point of common tangency. In another embodiment, the curved profile can include curves that do not meet at a common tangency. A cut out can be formed in the curved profile. In some forms, the cut out is formed on a pressure face of the attachment feature.