Mechanical Face Seal Thermal Management via Composite Structure

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Solution Overview

Problem

Mechanical face seals in industrial equipment face challenges such as rapid failure due to high temperatures and debris, leading to heat damage and increased costs due to heavy, costly alloy materials with reduced thermal conductivity, and existing monitoring systems only partially address friction variations without mitigating heat build-up.

Innovation Solution

The mechanical face seal design incorporates an annular body with a radially projecting flange, sealing bands, and features like cooling channels and fins to enhance heat dissipation, along with additive manufacturing for lighter and more cost-effective production, allowing for efficient heat management and durability improvements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If solid seal rings are manufactured by casting with heavy alloy materials, then strength and robustness are improved, but weight increases and thermal conductivity decreases

Engineering Contradiction:
Improveseal ring strengthVSAvoidseal ring weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The seal ring is constructed as a composite structure with a reinforcement structure (such as a metallic backbone or framework) and a lining layer (such as a polymer or composite material). This combination provides the necessary strength and robustness while reducing weight compared to solid alloy casting. The reinforcement structure carries the mechanical loads while the lining provides sealing functionality with lower density material.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The seal ring is divided into functionally distinct segments: a reinforcement structure providing structural integrity and a separate lining layer providing sealing functionality. This segmentation allows each component to be optimized independently - the reinforcement can use high-strength, low-weight materials while the lining uses materials optimized for sealing and thermal management.

Inventive Principle:
Principle #1Segmentation

2Strength

If solid seal rings are manufactured by casting with heavy alloy materials, then strength and robustness are improved, but manufacturing cost increases

Engineering Contradiction:
Improveseal ring strengthVSAvoidmanufacturing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The composite construction with reinforcement structure and lining layer allows use of less expensive materials overall. The reinforcement structure can use cost-effective metallic frameworks while the lining can use lower-cost polymer or composite materials, reducing the need for expensive alloy materials required in solid casting while maintaining necessary strength properties.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The segmented design enables separate manufacturing and assembly of components, potentially allowing for more cost-effective production methods. The reinforcement structure and lining can be manufactured using different, optimized processes and then assembled, providing flexibility in selecting cost-effective manufacturing approaches for each component.

Inventive Principle:
Principle #1Segmentation

3Device complexity

If conventional seal ring design is used, then structural simplicity is maintained, but heat dissipation capability is reduced

Engineering Contradiction:
Improveseal ring structural complexityVSAvoidheat dissipation
Core Design Contradiction:
Device complexityVSTemperature

Solution Approach 1:

The seal ring incorporates thermal management features such as cooling channels or heat dissipation fins in specific locations where heat generation occurs. These localized thermal management features are integrated into the reinforcement structure or lining, providing enhanced heat dissipation capability without requiring a complete redesign of the entire seal ring structure.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The invention adds thermal management functionality by incorporating three-dimensional heat dissipation features such as internal cooling channels or external fins. These features add volume and surface area in the third dimension, enabling improved heat dissipation while maintaining a relatively simple two-dimensional footprint and overall structural form.

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

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 reduces heat build-up and weight, enhancing the durability and longevity of mechanical face seals while maintaining operational pressures, allowing for increased machine speed with reduced risk of seal damage and lower manufacturing costs.

Implementation Method 1

features like cooling channels and fins to enhance heat dissipation

Methodology Applied
Scientific EffectHeat conduction: Conduction (thermal)

Implementation Method 2

cooling channels and fins to enhance heat dissipation

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentUS9951872B2Mechanical face seal
Publication Date: 2018.04.24 CATERPILLAR INC
  • US9951872B2 patent drawing
  • US9951872B2 patent drawing
  • US9951872B2 patent drawing

AI summary

A mechanical face seal includes a seal ring, the seal ring including an inner circumferential surface, an outer circumferential surface, and a generally annular body extending between the inner and outer circumferential surfaces. An annular flange projects radially from the annular body to an outer perimeter of the flange and a sealing band is on the annular flange. A slot may extend radially into the seal ring from the inner circumferential surface of the seal ring. A cooling channel may be in and extend generally circumferentially through at least one of the annular body and annular flange.