Composite Cylinder Liner Insert for Combustion Heat Retention

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing cylinder liners for internal combustion engines face challenges in managing heat transfer and maintaining dimensional tolerances after thermal barrier coatings are applied, particularly on the outer diameter, which complicates the manufacturing process.

Innovation Solution

A cylinder liner design incorporating an insert body with an inner portion made of iron-based material and an outer portion made of a material with thermal conductivity not greater than 3.5 W/mK, such as ceria stabilized zirconia, to trap heat in the combustion chamber while providing a normal surface for piston rings, and a thermal barrier coating to interrupt heat flow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If a thermal barrier coating is applied to the outer diameter of the cylinder liner, then heat transfer management is improved, but dimensional tolerance control deteriorates

Engineering Contradiction:
Improveheat transfer managementVSAvoiddimensional tolerance
Core Design Contradiction:
TemperatureVSManufacturing precision

Solution Approach 1:

The cylinder liner is divided into two distinct segments: an inner portion made of iron-based material and an outer portion made of material with thermal conductivity ≤3.5 W/mK. This segmentation allows each portion to serve its specific function - the inner portion maintains dimensional tolerance for piston ring contact while the outer portion provides thermal barrier properties, resolving the contradiction between heat transfer management and dimensional precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention uses composite construction by combining two different materials - iron-based material for the inner portion and low thermal conductivity material (such as ceria stabilized zirconia) for the outer portion. This composite approach enables simultaneous achievement of dimensional stability (from the iron-based inner layer) and effective thermal barrier performance (from the outer insulating layer) without the trade-off present in conventional single-material liners with coatings.

Inventive Principle:
Principle #40Composite materials

2Temperature

If an insert body with low thermal conductivity material is used, then thermal performance is improved, but device complexity increases

Engineering Contradiction:
Improvethermal performanceVSAvoidstructural complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The invention merges the insert body (inner portion) and the thermal barrier layer (outer portion) into a single integrated cylindrical structure that functions as one component within the cylinder liner assembly. This merging reduces overall device complexity compared to separate insert and coating systems, while still achieving superior thermal performance through the composite material structure.

Inventive Principle:
Principle #5Merging (Combining)

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 design effectively manages heat transfer and maintains dimensional stability, enhancing the thermal performance and manufacturing precision of the cylinder liner.

Implementation Method 1

The outer surface of the outer portion is formed of a material having a thermal conductivity of not greater than 3.5 W/mK

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 2

a thermal barrier coating to interrupt heat flow

Methodology Applied
Scientific EffectThermal barrier: Thermal Insulation

Data Source

PatentEP3887662B1Thermal barrier cylinder liner insert
Publication Date: 2025.12.31 FEDERAL MOGUL POWERTRAIN INC
  • EP3887662B1 patent drawingFigure 1~2
  • EP3887662B1 patent drawingFigure 2A~2B

AI summary

An insert for a cylinder liner which is capable of trapping heat in the combustion chamber is provided. The insert extends circumferentially around a center axis and longitudinally from an upper end to a lower end. The insert includes an inner portion presenting an inner surface facing the center axis and an outer portion presenting an outer surface facing away from the center axis. The inner portion is formed of an iron-based material, such as steel, and the outer portion is formed of a material having a thermal conductivity of not greater than 3.5 W/mK, for example ceria stabilized zirconia. The inner and outer portions each present a thickness, and the thickness can form a gradient between the upper end and the lower end of the insert. For example, the thickness of the outer portion can be greater at the upper end than at the lower end of the insert.