Heat transfer fin

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Solution Overview

Problem

Conventional heat exchangers with staggered heat transfer tubes experience inefficient heating due to repeated temperature rise and fall of the heat medium caused by alternating combustion exhaust gas and air flow, leading to suboptimal heat transfer.

Innovation Solution

A heat transfer fin design with heat-transfer-tube insertion holes aligned in a single stage, featuring downstream cut portions recessed toward the upstream side, downstream flanges, and alternately protruding first and second cut-and-raised pieces to promote turbulent flow and extended contact time with combustion exhaust gas.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If heat transfer tubes are arranged in staggered stages in the direction of gas flow, then heat transfer efficiency is improved, but temperature fluctuations of the heat medium occur due to alternating combustion exhaust gas and air flow

Engineering Contradiction:
Improveheat transfer efficiencyVSAvoidtemperature fluctuations of heat medium
Core Design Contradiction:
ProductivityVSTemperature

Solution Approach 1:

The heat transfer tubes are segmented into multiple stages arranged in the gas flow direction, with each stage processing the heat medium sequentially. This segmentation allows the heat medium to progressively absorb heat while minimizing temperature fluctuations through the staged configuration.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the heat transfer fin are given different functions: the upstream region handles combustion exhaust gas heating, while the downstream region handles combustion air heating. This local differentiation prevents mixed temperature effects on the heat medium.

Inventive Principle:
Principle #3Local quality

2Duration of action of moving object

If downstream cut portions are recessed toward the upstream side, then contact time with combustion exhaust gas is extended, but device complexity increases

Engineering Contradiction:
Improvecontact time with combustion exhaust gasVSAvoidstructural complexity of heat transfer fin
Core Design Contradiction:
Duration of action of moving objectVSDevice complexity

Solution Approach 1:

The downstream cut portions are formed with curved or recessed profiles instead of straight edges, creating a tapered configuration that naturally extends the gas flow path and contact time without requiring additional mechanical components.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The cut portions extend in the thickness direction of the heat transfer fin, creating a three-dimensional recessed structure that increases contact time through the fin's depth rather than requiring longer lateral paths.

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

This design enhances heat transfer efficiency by reducing temperature fluctuations and promoting turbulent flow, ensuring consistent heating of the heat medium despite partial combustion conditions.

Implementation Method 1

combustion exhaust gas generated from a burner flows through a heat exchanger

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

heat in the combustion exhaust gas to efficiently transfer to the heat medium flowing in the heat transfer tubes

Methodology Applied
Scientific EffectHeat conduction: Conduction (thermal)

Implementation Method 3

downstream cut portions recessed toward the upstream side, downstream flanges, and alternately protruding first and second cut-and-raised pieces to promote turbulent flow

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS11333397B2Heat transfer fin
Publication Date: 2022.05.17 RINNAI CORP
  • US11333397B2 patent drawing
  • US11333397B2 patent drawing
  • US11333397B2 patent drawing

AI summary

A heat transfer fin (1) includes a plurality of heat-transfer-tube insertion holes (10) aligned in a single stage, a downstream cut portion (3) formed so as to be recessed toward an upstream side of a gas flow passage of combustion exhaust gas, a downstream flange (13) formed on a peripheral edge of the downstream cut portion (3) so as to protrude from one surface of the heat transfer fin (1), and a plurality of first protruding pieces (4a) (4b) (4c) formed between the heat-transfer-tube insertion hole (10) and the downstream flange (13) so as to protrude alternately from both surfaces of the heat transfer fin (1).