CMC Turbine Vane Attachment Radial Offset Design

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Solution Overview

Problem

The connection between ceramic matrix composite distributors and metal support in turbomachines faces challenges due to significant prestress requirements, leading to premature wear at contact zones and stress concentrations, especially under thermal and aerodynamic forces.

Innovation Solution

A segmented annular distributor sector with a central flange and side flanges, and a metallic support sector with central and lateral hooks, where the central flange and hooks are radially offset, allowing for radial contact and support without high prestress, distributing external stresses homogeneously across the edges and hooks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If high prestress is applied to the connection between ceramic matrix composite distributor and metal support, then the connection reliability is improved, but the mechanical strength of the ceramic matrix composite distributor deteriorates leading to premature wear

Engineering Contradiction:
Improveconnection reliabilityVSAvoidmechanical strength of ceramic matrix composite distributor
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The connection interface is segmented into multiple contact zones: a first contact zone for the upstream rim and upstream hook, and a second contact zone for the downstream rim and downstream hook. This segmentation distributes the prestress across multiple locations rather than concentrating it at a single interface, reducing the stress burden on the ceramic matrix composite material while maintaining overall connection reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The ceramic matrix composite distributor is designed with locally optimized features at the connection interface, including specific rim geometries and thickness variations at the upstream and downstream ends. These local structural adaptations enable the material to better withstand the applied prestress without premature wear, addressing the strength limitation at critical locations while preserving the overall lightweight advantage of using ceramic matrix composite.

Inventive Principle:
Principle #3Local quality

2Stability of the object's composition

If high prestress is applied to prevent flange separation under thermal and aerodynamic forces, then the connection stability is improved, but the localized forces at interfaces increase causing premature wear

Engineering Contradiction:
Improveconnection stabilityVSAvoidlocalized forces at interfaces
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The connection interface is divided into upstream and downstream contact zones, each handling specific portions of the thermal and aerodynamic loads. This segmentation prevents concentration of localized forces at a single interface by distributing them across multiple separated contact regions, thereby reducing wear while maintaining connection stability under operational forces.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The connection design incorporates axial extension of the upstream and downstream rims, adding an axial dimension to the force distribution. By extending the contact surfaces axially, the interface area is increased, which distributes the localized forces over a larger area and reduces stress concentration, thereby preventing premature wear while maintaining stability against thermal expansion and aerodynamic forces.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Data Source

PatentEP3721058B1Connection between a guide vane sector made of cmc material and a metallic support of a turbine of a turbomachine
Publication Date: 2022.03.23 SAFRAN AIRCRAFT ENGINES SAS
  • EP3721058B1 patent drawingFigure 1~2
  • EP3721058B1 patent drawingFigure 3~5

AI summary

Sector (7), made of ceramic matrix composite, of a stator (4) of a turbine (1) of a turbomachine (2) comprising an outer platform (8) and an inner platform (9) that are connected via at least one vane, said outer platform (8) comprising means (10) for attaching to a sector (11) of a metallic support (12), the attachment means (10) comprising at least one central rim and two lateral rims, said central rim being radially offset with respect to said lateral rims along a directrix line such that the central rim is radially on one side of said directrix line and the lateral rims on the other, said central rim and said central hook bearing radially against one another and being located radially on either side of said directrix line, said lateral rim and said corresponding lateral hook bearing radially against one another and being located radially on either side of said directrix line.