Compressor Baffle Reduces Reed Valve Stress

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Solution Overview

Problem

Compressor heads with cooling plates and discharge reed valves experience premature failure due to air dynamics-induced flutter near the cooling plate aperture, leading to uneven stress on the reed valves.

Innovation Solution

A baffle with parallel legs and apertures is introduced to direct air flow, reducing turbulence and pressure fluctuations proximate to the reed valves by communicating air from one side of the baffle to the other, thereby minimizing stress on the valves.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If a cooling plate with aperture is used to cool air in compressor head, then cooling efficiency is improved, but airflow turbulence and pressure fluctuation increase causing valve flutter and premature failure

Engineering Contradiction:
Improveair temperatureVSAvoidvalve lifespan
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

A baffle structure is introduced as an intermediary element between the cooling plate aperture and the reed valves. The baffle includes a first leg positioned proximate to a first valve and a second leg positioned proximate to a second valve, with apertures in the legs allowing controlled air communication. This intermediary structure redirects airflow to reduce turbulence and pressure fluctuations at the valve locations while preserving cooling functionality.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If reed valves are positioned on the same side of cooling plate for compact design, then device complexity is reduced, but uneven stress distribution occurs causing one valve to fail before the other

Engineering Contradiction:
Improvevalve arrangementVSAvoiduniform valve lifespan
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The baffle structure provides localized airflow management at each valve position. The first leg is positioned proximate to the first valve and the second leg is positioned proximate to the second valve, with each leg having apertures that control local airflow characteristics. This localized approach ensures that each valve experiences similar airflow conditions and stress levels, achieving uniform lifespan despite their positions on the same side of the cooling plate.

Inventive Principle:
Principle #3Local quality

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 significantly extends the useful life of the reed valves by reducing airflow turbulence and pressure fluctuations, resulting in a 40-fold increase in average valve lifespan compared to compressor heads without the baffle.

Implementation Method 1

A baffle, for directing air within a compressor head, includes a first leg extending along a first direction, positioned proximate to a first valve of the compressor head, and a second leg extending along the first direction and substantially parallel to the first leg, positioned proximate to a second valve of the compressor head

Methodology Applied
Scientific EffectAirflow direction control:

Implementation Method 2

An aperture in the first leg communicates a second portion of the air from the first side of the first leg to the second side of the first leg. A turbulence and/or pressure fluctuation proximate the first valve is reduced by communicating the second portion of the air from the first side to the second side of the first leg

Methodology Applied
Scientific EffectPressure equalization:

Data Source

PatentEP3237755B1System and method for reducing at least one of airflow turbulence and pressure fluctuation proximate a valve
Publication Date: 2019.03.06 BENDIX COMMERCIAL VEHICLE SYSTEMS LLC
  • EP3237755B1 patent drawingFigure 1
  • EP3237755B1 patent drawingFigure 2
  • EP3237755B1 patent drawingFigure 3

AI summary

A baffle, for directing air within a compressor head, includes a first leg extending along a first direction, positioned proximate to a first valve of the compressor head, and a second leg extending along the first direction and substantially parallel to the first leg, positioned proximate to a second valve of the compressor head. A first portion of air from a first side of the first leg is communicated to a second side of the first leg beyond an end of the fi rst leg. An aperture in the first leg communicates a second portion of the air from the first side of the first leg to the second side of the first leg. A turbulence and/or pressure fluctuation proximate the first valve is reduced by communicating the second portion of the air from the first side to the second side of the first leg.