Segmented Ring Sealing Insert for Turbomachine Leakage Reduction

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Solution Overview

Problem

Turbomachines face challenges in reducing leakage and achieving efficient sealing in turbine modules due to clearance flows between segmented rings, which affect the overall tightness and operational efficiency.

Innovation Solution

A segmented ring design with circumferentially divided segments and radially open pockets allows for axial retention of a sealing insert, enabling efficient sealing while facilitating radial assembly, thereby reducing leakage and enhancing mounting possibilities.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a segmented ring is divided into circumferential segments for easier assembly, then ease of operation is improved, but leakage increases due to clearance flows at the joints

Engineering Contradiction:
Improveease of assemblyVSAvoidsealing tightness
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

A sealing insert is introduced as an intermediary element at the joints between segments. The sealing insert comprises a sealing element that engages with sealing surfaces on the segments to block clearance flows, while also including a retaining structure that anchors it in the radially open pocket. This intermediary component enables both segmented assembly and effective sealing.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The segmented ring is divided into multiple circumferential segments that can be assembled separately and then joined together. Each segment has a pocket structure that receives a sealing insert at the joint, allowing the ring to be assembled in sections while maintaining sealing integrity at the interfaces between segments.

Inventive Principle:
Principle #1Segmentation

2Reliability

If a sealing insert is added to seal the joint, then sealing tightness is improved, but device complexity increases

Engineering Contradiction:
Improvesealing tightnessVSAvoidstructural complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The sealing insert combines multiple functions into a single integrated component: it includes a sealing element for blocking clearance flows and a retaining structure for axial retention in the radially open pocket. By merging these functions into one element, the solution improves sealing without proportionally increasing complexity.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The sealing insert is designed to be self-retaining through its retaining structure that engages with the pocket structure of the segments. The sealing element and retaining structure work together automatically once the insert is positioned, eliminating the need for additional retention mechanisms or complex assembly procedures.

Inventive Principle:
Principle #25Self-service

3Ease of operation

If segments are assembled radially from inside outward, then ease of operation is improved, but achieving complete sealing becomes more difficult

Engineering Contradiction:
Improveease of assemblyVSAvoidsealing completeness
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The sealing insert includes a retaining structure with axial retention capability that extends into the radially open pocket. This adds an axial dimension to the sealing approach, allowing the sealing insert to be retained axially while being assembled radially from inside outward, thus achieving complete sealing through radial assembly.

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

Solution Approach 2:

The sealing insert acts as an intermediary that bridges the joint between segments and is retained in the radially open pocket through its retaining structure. This intermediary element ensures that even with radial assembly from inside, the joint is completely sealed by the sealing element engaging with the sealing surfaces on adjacent segments.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS11125097B2Segmented ring for installation in a turbomachine
Publication Date: 2021.09.21 MTU AERO ENGINES GMBH
  • US11125097B2 patent drawing
  • US11125097B2 patent drawing
  • US11125097B2 patent drawing

AI summary

A segmented ring for installation in a turbomachine, circumferentially divided into segments, considered with respect to a ring axis of the segmented ring, wherein the segmented ring is adapted for installation from radially inside; i.e., the segments can be assembled radially outwardly to form the segmented ring. At least two immediately circumferentially adjacent segments meet in a joint at which a sealing insert is provided. A pocket which is open toward the joint is formed in each of the at least two immediately circumferentially adjacent segments; i.e., two circumferentially mutually facing pockets are provided at the joint. The sealing insert is disposed in the two mutually facing pockets and axially retained therein and extends circumferentially across the joint, and a pocket of the two mutually facing pockets is additionally also open in a radial direction such that this segment can be radially slid onto the sealing insert.