Helical Heat Exchange Cell Layout to Prevent Gas Bypass

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Solution Overview

Problem

Existing heat exchange cells face inefficiencies in heat transfer due to preferential bypass pathways of combustion gases, leading to reduced thermal power delivery and increased size, while configurations with partition elements compromise on thermal power for improved condensing capacity and axial extension.

Innovation Solution

A heat exchange cell design featuring a separating element mounted externally to the heat exchanger, with a configuration allowing parallel fluid flow between the heat exchanger and collection chambers, and optimized fluid dynamics through strategically positioned passages, enhancing heat exchange efficiency and flexibility.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a helically-shaped heat exchanger is used to increase heat exchange surface area, then heat exchange efficiency is improved, but axial extension increases

Engineering Contradiction:
Improveheat exchange efficiencyVSAvoidaxial extension
Core Design Contradiction:
ProductivityVSLength of moving object

Solution Approach 1:

The patent transitions from a traditional axial helical configuration to a radial arrangement where the heat exchanger coils are positioned perpendicular to the axial direction. This dimensional change allows the heat exchange surface to be distributed radially rather than axially, maintaining high heat exchange efficiency while minimizing axial extension of the device.

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

Solution Approach 2:

The patent employs curved and radial flow paths within the combustion chamber, directing combustion gases to flow radially across the heat exchanger coils. This curved flow pattern increases the effective heat exchange surface area utilization without requiring additional axial length, as the gases follow a radial trajectory through the compact coil arrangement.

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Productivity

If partition elements are added to improve condensing capacity, then heat exchange capacity is improved, but thermal power delivery is reduced

Engineering Contradiction:
Improvecondensing capacityVSAvoidthermal power delivery
Core Design Contradiction:
ProductivityVSPower

Solution Approach 1:

The patent segments the combustion chamber into distinct zones: a primary combustion zone where high-temperature thermal power transfer occurs, and a secondary condensation zone where lower-temperature condensation heat exchange takes place. This spatial segmentation allows both high thermal power delivery and condensing capacity to occur simultaneously in different regions without the trade-off present in partitioned axial designs.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the heat exchanger are optimized for different functions: coils positioned in the primary combustion zone are exposed to high-temperature gases for maximum thermal power transfer, while coils in the secondary zone operate at lower temperatures for condensation. This local optimization of heat exchange conditions in different spatial locations enables both high thermal power and condensing capacity.

Inventive Principle:
Principle #3Local quality

3Productivity

If combustion gases flow radially through heat exchanger coils, then heat exchange efficiency is improved, but preferential bypass pathways reduce effectiveness

Engineering Contradiction:
Improveheat exchange efficiencyVSAvoidenergy loss through bypass
Core Design Contradiction:
ProductivityVSLoss of energy

Solution Approach 1:

The patent introduces a centrally positioned baffle or separator element that acts as an intermediary to block preferential bypass pathways. This baffle forces the combustion gases to follow the intended radial flow path through all heat exchanger coils, preventing short-circuiting and ensuring complete utilization of the heat exchange surface area, thereby eliminating energy loss through bypass.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The radial flow configuration combined with central baffling creates a flow pattern where gases must pass through multiple coil turns in sequence. The flow dynamics naturally create feedback loops where pressure differentials ensure gases traverse the entire heat exchange surface, preventing bypass and maximizing heat extraction efficiency.

Inventive Principle:
Principle #23Feedback

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 achieves high maximum thermal power with minimized axial size, improved heat exchange capacity, and optimized fluid dynamics, reducing axial extension and pressure losses while maintaining overall efficiency.

Implementation Method 1

transfer thermal energy between two fluids

Methodology Applied
Scientific EffectHeat conduction: Conduction (thermal)

Implementation Method 2

heat exchange between a first heat transfer fluid circulating within the heat exchanger, and a second heat transfer fluid flowing in the containment casing externally to the heat exchanger

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

heat exchange cells of the condensation type configured to use both the heat developed as a result of combustion, and the latent condensation heat contained in the combustion gases

Methodology Applied
Scientific EffectCondensation: Condensation

Data Source

PatentEP3139106B1Heat exchange cell and method
Publication Date: 2018.12.26 CONDEVO
  • EP3139106B1 patent drawingFigure 1
  • EP3139106B1 patent drawingFigure 2a~2b
  • EP3139106B1 patent drawingFigure 3

AI summary

A heat exchange cell is described comprising a containment casing (11) comprising a rear wall (11d), a front wall (22) and a peripheral side wall (11c), a helically-shaped heat exchanger (13) comprising at least one tubular duct for the flow of a first heat transfer fluid coiled about a longitudinal axis of the helix according to a plurality of coils and mounted in the containment casing (11); a feeding zone of a second heat transfer fluid, intended for the heat exchange with the first heat transfer fluid, defined in the casing (11) coaxially and internally with respect to the heat exchanger (13); a first chamber (15) for collecting the second heat transfer fluid externally defined with respect to the heat exchanger (13) between a radially outer wall thereof and the peripheral side wall (11c) of the containment casing (11); and a second chamber (16) for collecting the second heat transfer fluid at least partially delimited by at least one separating element (14). The separating element (14) is mounted at an axially external position with respect to the heat exchanger (13) in such a way as to define the second chamber (16) for collecting the second heat transfer fluid between the separating element (14), the peripheral side wall (11c) and the rear wall (11d) or the front wall (22) of the containment casing (11); in this way, the first (15) and the second (16) collection chambers are in fluid communication with each other by means of at least one passage (17a, 17a', 17b-17g; 14e) configured to allow a flow of the second heat transfer fluid substantially in parallel to the peripheral side wall (11c) of the casing (11) and in proximity thereto. The separating element (14) comprises a heat exchange portion in contact with at least one portion of an end coil of the heat exchanger (13) and configured to allow a heat exchange between the coil-shaped portion of the heat exchanger (13) and the second collection chamber (16), while the heat exchange cell (10) further comprises at least one second passage (35) allowing a fluid outlet from the second collection chamber (16) peripherally defined in the second chamber (16) between an axial end (11g) of the peripheral side wall (11c) and the rear wall (11d) or the front wall (22) of the containment casing (11).