Multi-Radius Securing Plate for Turbo Engine Blade Axial Locking

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Solution Overview

Problem

Existing turbomachine blade securing mechanisms have a limited contact area between the locking plate and the groove, leading to potential damage from high surface pressure during vibratory movements, which reduces the service life and efficiency of the turbomachine.

Innovation Solution

A securing means with a curved outer contour having different radii is used to increase the contact area between the securing means and the groove wall, reducing surface pressure and the risk of damage, and incorporating an elastic design to dampen impacts and prevent self-locking.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a locking plate with a rounded shape is used to secure the blade axially, then the blade can be secured in the axial direction, but the contact area between the locking plate and the groove is small, leading to high surface pressure and potential damage to the groove wall

Engineering Contradiction:
Improveaxial securing of bladeVSAvoidsurface pressure on groove wall
Core Design Contradiction:
ReliabilityVSStress or pressure

Solution Approach 1:

The locking plate is designed with a curved outer contour having different radii of curvature in different areas, replacing a simple rounded shape with a more complex multi-radius curvature profile that optimizes contact distribution across the groove wall, increasing the contact area and reducing surface pressure

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

Different sections of the locking plate's outer contour have different radii of curvature tailored to match specific regions of the groove wall, optimizing the contact area distribution locally across different zones of the groove to evenly distribute the load and reduce peak surface pressures

Inventive Principle:
Principle #3Local quality

2Ease of manufacture

If the locking plate has a simple rounded shape, then the device is simple to manufacture, but the contact area is limited and damage risk increases under vibratory loads

Engineering Contradiction:
Improvemanufacturing simplicity of locking plateVSAvoidresistance to damage under vibration
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The locking plate employs a curved outer contour with different radii that can be manufactured using standard forming processes while achieving superior contact characteristics, balancing manufacturing feasibility with enhanced reliability under vibratory conditions

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Reliability

If the contact area between the locking plate and groove is increased, then the surface pressure is reduced and damage risk is minimized, but the device complexity increases

Engineering Contradiction:
Improvereduction of damage riskVSAvoidcomplexity of locking plate geometry
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The curved outer contour with different radii is achieved through conventional metal forming techniques, adding geometric complexity but not requiring additional components or assembly steps, thus limiting the increase in overall device complexity while achieving the reliability benefit

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 increased contact area and elastic design enhance the service life of the turbomachine by reducing the risk of damage and maintaining operational efficiency by minimizing high forces and self-locking issues.

Implementation Method 1

incorporating an elastic design to dampen impacts and prevent self-locking

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

elastic design to dampen impacts

Methodology Applied
Scientific EffectDamping: Damping

Implementation Method 3

An outer contour of the securing means, which faces the inner wall of the groove, in particular a groove base facing the groove, is curved at least in some areas, with the outer contour having different radii in some areas

Methodology Applied
Scientific EffectGeometry: Geometry

Data Source

PatentEP2455588B1Securing module for axial securing of a root of a turbo engine blade
Publication Date: 2017.03.01 MTU AERO ENGINES GMBH
  • EP2455588B1 patent drawing
  • EP2455588B1 patent drawing
  • EP2455588B1 patent drawing

AI summary

The securing unit (20) i.e. securing plate, has a partially curved outer contour (24) facing toward a groove wall that is designed as a groove base (33). The outer contour includes different radii (R1-R3), where the first radius is arranged between the second and third radii, and the second radius is larger than the first and third radii. A section of the outer contour forms a securing unit-contact region (21) that is arranged in contact with a groove contact region (31) of the groove wall, where the securing unit includes an elastic material.