Turbine Case Seal Baffle for Cantilever Wall Vibration Damping

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Solution Overview

Problem

Existing aircraft engine turbine case structures face challenges in managing dynamic excitation and vibration-induced stress due to the cantilevered configuration of inner walls, which can lead to crack formation and increased stress levels.

Innovation Solution

Incorporation of a damping seal baffle, such as a compliant sheet metal body, mounted to the inner case and configured to move along a seal platform surface, which dampens the inner wall's deflection and reduces vibration-induced stresses by maintaining contact over varying thermal conditions, with an axial baffle stopper limiting further deflection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a cantilevered inner wall configuration is used in the turbine case, then the structural support for the turbine section is improved, but vibration-induced stress and deflection increase leading to potential crack formation

Engineering Contradiction:
Improvestructural supportVSAvoidvibration-induced stress
Core Design Contradiction:
StrengthVSStress or pressure

Solution Approach 1:

A damping seal baffle is introduced as an intermediary component between the inner case and the cantilevered inner wall. This baffle acts as a mediator that absorbs and dissipates vibration-induced stresses through friction and deformation, preventing stress transmission to the cantilevered wall while maintaining structural support. The baffle includes a damping portion that contacts the inner wall and a seal portion that maintains sealing while allowing controlled movement.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The damping seal baffle utilizes material parameter changes through elastomeric or compliant materials that can deform and absorb vibrations. The baffle's material properties are selected to provide optimal damping characteristics, changing its stiffness and friction characteristics based on thermal and vibrational conditions to reduce stress on the cantilevered structure.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If a rigid seal structure is used at the interface between inner case and cantilevered wall, then sealing is maintained, but thermal expansion and contraction cause stress and potential failure

Engineering Contradiction:
ImprovesealingVSAvoidthermal stability
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The seal portion of the damping seal baffle is designed to be dynamic rather than rigid, allowing it to move axially and radially in response to thermal expansion and contraction. The seal maintains contact with the cantilevered inner wall through controlled elastic deformation, accommodating thermal movements while maintaining sealing effectiveness throughout the operating temperature range.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The damping seal baffle incorporates flexible elastomeric or compliant material portions that can deform to maintain sealing contact. The seal portion acts as a flexible element that conforms to thermal expansion and contraction of the metal components, maintaining reliable sealing without transmitting thermal stress to the cantilevered structure.

Inventive Principle:
Principle #30Flexible shells and thin films

3Stress or pressure

If the damping seal baffle is allowed to move freely along the seal platform surface, then vibration damping is improved, but excessive deflection may occur

Engineering Contradiction:
Improvevibration-induced stressVSAvoiddeflection
Core Design Contradiction:
Stress or pressureVSLength of moving object

Solution Approach 1:

A stopper feature is provided that preliminarily prevents excessive deflection of the damping seal baffle. The stopper acts as a mechanical constraint that engages if the baffle deflects beyond a predetermined amount, providing counter-action to prevent excessive movement while allowing normal vibration damping operation within safe deflection limits.

Inventive Principle:
Principle #9Preliminary anti-action

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 damping seal baffle effectively reduces vibration-induced stresses and maintains structural integrity by damping the inner wall's deflection, thereby preventing crack formation and enhancing the durability of the turbine case structure.

Implementation Method 1

The damping seal baffle is disposed in contact with the seal platform surface and configured to move along the seal platform surface, which dampens the inner wall's deflection and reduces vibration-induced stresses

Methodology Applied
Scientific EffectVibration damping: Damping

Implementation Method 2

The damping seal baffle... configured to move along the seal platform surface, which dampens the inner wall's deflection and reduces vibration-induced stresses

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 3

maintaining contact over varying thermal conditions

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 4

Incorporation of a damping seal baffle, such as a compliant sheet metal body

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS12565846B1Turbine case structure for an aircraft propulsion system engine
Publication Date: 2026.03.03 PRATT & WHITNEY CANADA CORP
  • US12565846B1 patent drawing
  • US12565846B1 patent drawing
  • US12565846B1 patent drawing

AI summary

A gas turbine engine includes a turbine section, a turbine case, an inner case, and a damping seal baffle. The turbine section extends along a rotational axis of the gas turbine engine. The turbine case includes a cantilevered inner wall. The cantilevered inner wall extends circumferentially about the rotational axis. The cantilevered inner wall extends between and to an upstream axial end and a downstream axial end. The upstream axial end is disposed at and downstream of the turbine section. The cantilevered inner wall forms a seal platform surface. The inner case extends circumferentially about the rotational axis. The inner case is disposed radially inward of the upstream axial end. The damping seal baffle extends circumferentially about the rotational axis. The damping seal baffle is mounted to the inner case. The damping seal baffle is disposed in contact with the seal platform surface.