Turbo Machine Sealing Assembly for Vane Carrier Gap Leakage

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Solution Overview

Problem

In turbo machines, the leakage of fluid through gaps between vane carriers in the axial direction of the turbine casing reduces conversion efficiency, necessitating a reliable sealing mechanism to minimize fluid leakage and maintain efficient operation.

Innovation Solution

A sealing assembly is introduced, comprising a sealing body and a pressing member that extends and compresses in the circumferential direction, allowing the sealing body to be pressed toward the first vane carrier, thereby maintaining contact and sealing the gap between vane carriers, even during thermal expansion and operational changes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If a sealing assembly is introduced to seal the gap between vane carriers, then fluid leakage is reduced and conversion efficiency is improved, but device complexity increases due to additional sealing components

Engineering Contradiction:
Improvefluid leakageVSAvoidsealing assembly structure
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The sealing body is inserted into a sealing groove formed in the second vane carrier, creating a nested structure where the sealing assembly is integrated within the existing vane carrier geometry rather than adding external components. This reduces overall device complexity while maintaining sealing functionality

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The pressing member acts as an intermediary element between the sealing body and the vane carriers, providing the necessary contact force to maintain sealing without requiring complex fastening mechanisms. The pressing member translates thermal expansion and operational movements into effective sealing pressure

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the sealing body is pressed firmly against the vane carriers to ensure hermetic sealing, then sealing reliability is improved, but the sealing assembly becomes less adaptable to thermal expansion and operational changes

Engineering Contradiction:
Improvesealing performanceVSAvoidaccommodation of thermal expansion
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The pressing member is designed with elastic properties allowing it to dynamically adjust its compression force on the sealing body in response to thermal expansion and operational changes. This dynamic adaptation maintains reliable sealing without requiring overly rigid constraints that would reduce adaptability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The sealing assembly utilizes changes in the pressing member's elastic parameters (compression force) in response to thermal and operational conditions. As temperature and operational states change, the pressing member's elastic deformation adjusts the sealing pressure to maintain hermetic sealing across varying conditions

Inventive Principle:
Principle #35Parameter changes

3Stability of the object's composition

If the pressing member is made rigid to maintain consistent sealing pressure, then sealing stability is improved, but the sealing assembly cannot accommodate thermal expansion and operational changes

Engineering Contradiction:
Improvesealing pressure consistencyVSAvoidresponse to operational changes
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The pressing member is constructed from elastic material rather than rigid structure, allowing it to flex and deform in response to thermal expansion and operational changes while maintaining consistent sealing pressure. This flexibility enables the assembly to adapt to dimensional changes in the vane carriers without compromising sealing stability

Inventive Principle:
Principle #30Flexible shells and thin films

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 sealing assembly ensures consistent hermetic sealing of the gap between vane carriers, maintaining sealing performance while accommodating thermal expansion and operational changes, thus enhancing the efficiency of fluid flow and reducing leakage.

Implementation Method 1

configured to extend and compress in a circumferential direction of the first component

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS11415017B2Rotor and turbo machine including same
Publication Date: 2022.08.16 DOOSAN HEAVY IND & CONSTR CO LTD
  • US11415017B2 patent drawing
  • US11415017B2 patent drawing
  • US11415017B2 patent drawing

AI summary

A sealing assembly for sealing a gap between a first component and a second component is provided. The sealing assembly includes a sealing body disposed between the first component and the second component and a pressing member disposed between the sealing body and the second component, configured to press the sealing body toward the first component, and configured to extend and compress in a circumferential direction of the first component.