Spiral Oil Separator for Engine Blow-by Gas

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Solution Overview

Problem

Existing oil separation devices for internal combustion engines face limitations in improving oil separation performance due to increased flow resistance and reduced blow-by gas velocity when attempting to enhance oil separation through more baffle plates, tortuous passages, or longer lengths, which restricts the effectiveness of oil removal from blow-by gas.

Innovation Solution

The design incorporates a spiral passage within the gas liquid separation chamber with inclined walls and partition walls that create a swirl flow, minimizing flow resistance and reducing velocity, while promoting oil adherence to the walls through centrifugal force, allowing for improved oil separation performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If the number of baffle plates is increased to improve oil separation performance, then oil separation performance is improved, but flow resistance increases and gas velocity decreases

Engineering Contradiction:
Improveoil separation performanceVSAvoidflow resistance
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The patent employs a spiral passage configuration instead of straight or angular baffle plates. The curved, spiral path of the passage allows gas to flow in a rotational pattern, generating centrifugal force that enhances oil separation while maintaining smoother flow transitions that reduce flow resistance compared to sharp-angle baffle arrangements.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The invention transitions from a two-dimensional arrangement of parallel baffle plates to a three-dimensional spiral passage structure. This dimensional change allows the gas flow to utilize both linear progression and rotational motion, achieving enhanced separation performance through centrifugal effects while maintaining adequate flow velocity through the spiral geometry.

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

2Manufacturing precision

If the passage length is increased to improve oil separation performance, then oil separation performance is improved, but flow resistance increases and gas velocity decreases

Engineering Contradiction:
Improveoil separation performanceVSAvoidpassage length
Core Design Contradiction:
Manufacturing precisionVSLength of moving object

Solution Approach 1:

The spiral passage uses curved geometry to achieve extended flow path length within a compact volume. The rotational spiral configuration allows the gas to traverse a longer effective path for separation without requiring a proportionally longer linear passage, thereby maintaining gas velocity while achieving adequate separation distance.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Manufacturing precision

If the degree of tortuousness is increased to improve oil separation performance, then oil separation performance is improved, but flow resistance increases and gas velocity decreases

Engineering Contradiction:
Improveoil separation performanceVSAvoidpassage tortuousness
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The spiral passage provides a controlled tortuous path through uniform rotational curvature rather than complex multi-directional bends. This regular spiral geometry achieves adequate tortuousness for separation while maintaining predictable flow characteristics and avoiding the excessive flow resistance associated with highly tortuous, irregular passage configurations.

Inventive Principle:
Principle #14Spheroidality (Curvature)

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 configuration enhances oil separation efficiency by reducing flow resistance and maintaining blow-by gas velocity, effectively separating oil from the gas while maintaining efficient gas flow, thus improving overall oil separation performance.

Implementation Method 1

a spiral passage extending in a lengthwise direction of the gas liquid separation passage is defined by the lower partition walls and the upper partition walls; and wherein the spiral passage with a certain turn is defined by the lower partition walls and the upper partition walls for causing a swirl flow as gas flows from the gas inlet to the gas outlet

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

the spiral passage with a certain turn is defined by the lower partition walls and the upper partition walls for causing a swirl flow as gas flows from the gas inlet to the gas outlet

Methodology Applied
Scientific EffectSwirl flow: Vortex Ring

Implementation Method 3

the lower wall is inclined with respect to a horizontal plane such that an upstream part of the lower wall is lower than a downstream part of the lower wall when viewed in a direction of the swirl flow

Methodology Applied
Scientific EffectInertia: Inertia

Data Source

PatentUS10533470B2Oil separation device for internal combustion engine
Publication Date: 2020.01.14 HONDA MOTOR CO LTD
  • US10533470B2 patent drawing
  • US10533470B2 patent drawing
  • US10533470B2 patent drawing

AI summary

To improve the oil separation performance in an oil separation device for an internal combustion engine. The oil separation device (10) comprises a gas liquid separation passage (56) internally defined by a lower wall, an upper wall and a pair of side walls, and extending in a horizontal direction, a gas inlet (54) and a gas outlet (63) provided on either end of the gas liquid separation passage, a plurality of lower partition walls (56H) projecting upward from the lower wall, and a plurality of upper partition walls (56J) projecting downward from the upper wall. The lower partition walls and the upper partition wall are tilted with respective the length wise direction in plan view so as to define a spiral passage. The lower wall is inclined with respect to a horizontal plane such that an upstream part of the lower wall is lower than a downstream part of the lower wall with respect to a direction of the swirl flow.