Segmented Carbon Seal Pressure Balancing for Oil Leakage Control

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Solution Overview

Problem

Existing seal systems in gas turbine engines face challenges in effectively isolating oil-containing bearing compartments, particularly in maintaining a sufficient pressure difference to prevent oil leakage, while minimizing wear and ensuring structural integrity.

Innovation Solution

A segmented seal system with arcuate body segments featuring circumferential channels and dams, where the ID face channel has an open end and is deeper and wider than the OD face channel, allowing for efficient airflow and pressure distribution, and a garter spring biasing the segments to maintain contact and structural integrity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If the ID face circumferential channel is made deeper and wider with an open end, then airflow efficiency and pressure distribution are improved, but the complexity of the seal structure increases

Engineering Contradiction:
Improveairflow efficiencyVSAvoidseal structure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The seal is divided into multiple segments that can be assembled together, with each segment containing the complex channel structure. This segmentation allows the complicated ID face circumferential channel with open end to be manufactured and assembled more easily, reducing overall structural complexity while maintaining airflow efficiency

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The ID face circumferential channel is designed with non-uniform characteristics (deeper and wider in specific regions, with an open end) to optimize airflow distribution locally where it is most needed, rather than uniformly throughout the entire seal structure

Inventive Principle:
Principle #3Local quality

2Stress or pressure

If circumferential grooves are added to distribute high pressure gas, then pressure balancing is improved, but the span of dams increases which reduces buffering effectiveness

Engineering Contradiction:
Improvepressure balancingVSAvoidbuffering effectiveness
Core Design Contradiction:
Stress or pressureVSReliability

Solution Approach 1:

The circumferential grooves are positioned and sized to provide sufficient pressure distribution with minimal dam span. By using partial action (grooves at specific locations rather than continuous grooves), the design achieves adequate pressure balancing while minimizing the reduction in buffering effectiveness

Inventive Principle:
Principle #16Partial or excessive action

3Reliability

If the seal operates with pressure difference to limit oil leakage, then sealing performance is improved, but wear increases due to contact between seal segments

Engineering Contradiction:
Improvesealing performanceVSAvoidservice life
Core Design Contradiction:
ReliabilityVSDuration of action of moving object

Solution Approach 1:

The seal design uses the pressure difference across the seal to self-regulate the contact conditions between segments. The high pressure side pushes the segments into light contact with the runner, while the low pressure side allows for clearance, creating a self-adjusting mechanism that maintains sealing performance while minimizing wear over the service life

Inventive Principle:
Principle #25Self-service

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 enhances pressure balancing, tolerance to wear, and structural integrity, reducing oil leakage and maintaining effective sealing performance over the lifespan of the seal.

Implementation Method 1

The segments are biased circumferentially inward via a garter spring (e.g., tension coil spring) encircling the array and captured in an outer diameter (OD) groove of each segment

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

For distribution of high pressure gas (e.g., the buffer air), the seals typically have open passageways along the respective low pressure face and ID face

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Implementation Method 3

a contacting carbon seal allows the required pressure drop

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS12025010B2Pressure-balanced carbon seal
Publication Date: 2024.07.02 RTX CORP
  • US12025010B2 patent drawing
  • US12025010B2 patent drawing
  • US12025010B2 patent drawing

AI summary

A seal segment has an arcuate body having: a first end; a second end circumferentially opposite the first end; a first face; a second face axially opposite the first face; an inner diameter (ID) face; and an outer diameter (OD) face. The seal segment is shaped to interfit with a plurality of identical seal segments first end to second end to form a seal surrounding a central longitudinal axis. The first face has: a circumferential channel closer to the ID face than the OD face; and a plurality of channels extending from the circumferential channel to the OD face. The ID face has: a circumferential channel closer to the first face than the second face; and a plurality of channels extending from the circumferential channel to the second face. The ID face circumferential channel has an open end.