Segmented Shroud Radial Displacement for Rotor Misalignment

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing sealing devices for axial turbomachines fail to compensate for misalignment between the rotor and stator, leading to irreversible clearance variations and efficiency losses, as well as potential engine damage from particle release.

Innovation Solution

A segmented shroud with elastic means, such as elastomeric elements, allows radial movement to accommodate misalignment, ensuring the shroud can conform to changes in alignment and maintain a centered circular shape.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If a fixed shroud is used, then manufacturing precision is improved, but the device cannot compensate for rotor-stator misalignment

Engineering Contradiction:
Improveshroud positioning accuracyVSAvoidmisalignment compensation capability
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The shroud is divided into multiple independent segments that can move radially relative to the casing wall. Each segment is retained by elastic means allowing independent radial displacement, enabling the shroud to adapt to misalignment while maintaining overall structural integrity and manufacturing precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The shroud transitions from a fixed rigid structure to a dynamic structure where segments can radially displace elastically. The elastic retention means allow the segments to move dynamically in response to misalignment forces while returning to their original position when misalignment is removed.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If a segmented shroud with radial movement capability is used, then misalignment compensation is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvemisalignment compensation capabilityVSAvoidshroud structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The shroud is segmented into multiple independent elements that can move radially. Each segment is retained by elastic means (such as elastomeric elements) that provide both retention and radial movement capability. This segmentation allows misalignment compensation while keeping individual segment manufacturing relatively simple.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The elastic means (e.g., elastomeric elements) provide a simple mechanism for radial movement through material elasticity rather than complex mechanical joints. The elastomeric material naturally provides both the retention force and the radial displacement capability, reducing structural complexity.

Inventive Principle:
Principle #35Parameter changes

3Strength

If the shroud is made rigid for structural strength, then strength is improved, but the shroud cannot radially displace to compensate misalignment

Engineering Contradiction:
Improveshroud structural strengthVSAvoidradial displacement capability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The shroud is divided into segments that maintain structural strength through their rigid construction while allowing radial displacement at the retention points. The elastic means (elastomeric elements) provide the displacement mechanism without compromising the overall structural integrity of the shroud segments.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The elastomeric elements act as flexible retention means that allow radial movement while the shroud segments themselves remain rigid for structural strength. The combination of rigid segments and flexible retention creates a structure that is both strong and adaptable.

Inventive Principle:
Principle #30Flexible shells and thin films

4Manufacturing precision

If abradable material is used for the shroud surface, then blade clearance control is improved, but particle release causes engine damage

Engineering Contradiction:
Improveblade clearance controlVSAvoidparticle release
Core Design Contradiction:
Manufacturing precisionVSObject-generated harmful factors

Solution Approach 1:

The shroud segments can dynamically adjust their radial position through elastic displacement, maintaining optimal blade clearance without relying solely on abradable material erosion. This dynamic adjustment reduces the need for excessive abradable material, thereby reducing particle release while maintaining clearance control.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The elastic means provide a cushioning mechanism that allows controlled radial displacement before contact occurs, reducing the impact forces that would otherwise require thick abradable material layers. This pre-cushioning effect minimizes the amount of abradable material needed and consequently reduces particle generation.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

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 solution effectively compensates for misalignment, maintaining efficient operation and preventing engine damage by allowing the shroud to radially displace and return to a centered position, utilizing elastomeric materials for damping and flexibility.

Implementation Method 1

elastic means, such as elastomeric elements, allows radial movement to accommodate misalignment

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

utilizing elastomeric materials for damping and flexibility

Methodology Applied
Scientific EffectDamping: Damping

Data Source

PatentEP2495399B1Segmented shroud assembly suitable for compensating a rotor misalignment relative to the stator
Publication Date: 2016.11.23 SAFRAN AERO BOOSTERS SA
  • EP2495399B1 patent drawingFigure 1~2
  • EP2495399B1 patent drawingFigure 3~5
  • EP2495399B1 patent drawingFigure 6~7

AI summary

The housing (12) has a segmented shell (22) that is structured and operable to enclose a row of blades (24) and supported by a structural wall. Elastically deformable units (30) are positioned between the wall and segments of the shell so as to radially displace the segments in the event of contact with tips of the blades of a rotor and in the event of misalignment of a rotation axis of the rotor relative to an axis of the housing. The deformable units comprise elements made of elastically deformable materials e.g. elastomeric materials. An independent claim is also included for an axial turbomachine compressor.