Asymmetric Cylinder Liner Support for Coolant Flow and Thrust Load

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Solution Overview

Problem

Existing cylinder liners face challenges with mechanical and thermal stresses, particularly at the lower end where coolant can escape into the crankcase, leading to potential damage and reduced reliability due to inadequate support and coolant flow.

Innovation Solution

A cylinder liner design featuring a hollow cylindrical body with a lower liner support having an asymmetric configuration in the circumferential direction, providing reduced clearance around the thrust/anti-thrust plane for increased support and increased clearance around the perpendicular plane for improved coolant flow, incorporating lower seal grooves and members to manage piston side thrusts and heat dissipation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a tight clearance is provided between the cylinder liner and the cylinder bore to provide structural support, then the mechanical strength and stability of the liner is improved, but the coolant flow is restricted leading to thermal stress and potential pitting

Engineering Contradiction:
Improvestructural supportVSAvoidcoolant flow
Core Design Contradiction:
StrengthVSLoss of energy

Solution Approach 1:

The patent applies local quality by providing different clearance characteristics at different locations of the cylinder liner. The lower portion (first region) has a first clearance characteristic optimized for structural support, while the upper portion (second region) has a second clearance characteristic optimized for coolant flow. This allows each region to have the appropriate clearance for its specific functional requirements without compromising the other.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent segments the cylinder liner into distinct regions with different clearance characteristics. The lower region near the crankcase is separated from the upper region, allowing independent optimization of clearance in each zone. This segmentation enables the lower portion to provide mechanical support while the upper portion maintains adequate coolant circulation.

Inventive Principle:
Principle #1Segmentation

2Ease of manufacture

If the cylinder liner has uniform clearance around the entire circumference, then the manufacturing is simplified, but the mechanical support under piston thrust is insufficient leading to liner displacement and damage

Engineering Contradiction:
Improveclearance uniformityVSAvoidliner stability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent employs asymmetry by providing different clearance characteristics at different circumferential locations of the cylinder liner. The lower portion has reduced clearance in the region corresponding to piston thrust directions to prevent liner displacement, while other regions maintain larger clearance. This asymmetric clearance distribution optimizes mechanical support where needed without uniformly complicating the manufacturing process.

Inventive Principle:
Principle #4Asymmetry

3Temperature

If the clearance is increased to improve coolant flow and prevent thermal stress, then the cooling efficiency is improved, but the mechanical support is reduced leading to increased liner displacement under piston thrust

Engineering Contradiction:
Improvecoolant circulationVSAvoidliner position
Core Design Contradiction:
TemperatureVSStability of the object's composition

Solution Approach 1:

The patent applies local quality by providing different clearance characteristics at different locations of the cylinder liner. The lower portion (first region) has a first clearance characteristic optimized for structural support, while the upper portion (second region) has a second clearance characteristic optimized for coolant flow. This allows each region to have the appropriate clearance for its specific functional requirements without compromising the other.

Inventive Principle:
Principle #3Local quality

4Shape

If a symmetric clearance configuration is used around the cylinder liner, then the structural balance is maintained, but the support under piston side thrust is inadequate causing liner damage

Engineering Contradiction:
Improveclearance symmetryVSAvoidthrust support
Core Design Contradiction:
ShapeVSStrength

Solution Approach 1:

The patent employs asymmetry by providing different clearance characteristics at different circumferential locations of the cylinder liner. The lower portion has reduced clearance in the region corresponding to piston thrust directions to prevent liner displacement, while other regions maintain larger clearance. This asymmetric clearance distribution optimizes mechanical support where needed without uniformly complicating the manufacturing process.

Inventive Principle:
Principle #4Asymmetry

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

This design enhances the structural support of the cylinder liner, reduces stress and displacement caused by piston thrusts, while ensuring effective coolant circulation and flow, thereby increasing the reliability and operating life of the engine by minimizing the risk of pitting and corrosion.

Implementation Method 1

an outer surface of the cylinder liner can form a coolant circulation space for cooling the cylinder liner

Methodology Applied
Scientific EffectHeat dissipation: Convection

Implementation Method 2

A plurality of lower seal grooves are provided in the outer surface of the cylinder liner each of which includes a respective lower seal member. The lower seal grooves are arranged between the coolant cavity and the lower end of the cylindrical body

Methodology Applied
Scientific EffectSealing:

Implementation Method 3

The lower liner support has an asymmetric configuration in a circumferential direction such that a clearance between the sidewall of the cylinder bore and the outer surface of the cylindrical body is relatively less in a first area surrounding the thrust/anti-thrust plane

Methodology Applied
Scientific EffectMechanical support:

Data Source

PatentUS10895218B2Liner for engine cylinder with lower liner support
Publication Date: 2021.01.19 CATERPILLAR INC
  • US10895218B2 patent drawing
  • US10895218B2 patent drawing
  • US10895218B2 patent drawing

AI summary

A cylinder liner for a cylinder bore of an internal combustion engine is provided. The cylinder liner including a hollow cylindrical body and a coolant cavity defined between a sidewall of the cylinder bore and an outer surface of the cylinder liner. A plurality of lower seal grooves are provided in the outer surface of the cylinder liner. A lower liner support is arranged between an uppermost one of the lower seal grooves and the coolant cavity. The lower liner support has an asymmetric configuration in a circumferential direction such that a clearance between the sidewall of the cylinder bore and the outer surface of the cylindrical body is relatively less in an area surrounding a thrust/anti-thrust plane and is relatively more in an area surrounding a perpendicular plane.