Offset Cooling Fins for Power Electronics Thermal Management

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing cooling methods for power-electronic components, such as pin fin arrangements, fail to fully utilize the heat transfer potential of coolants due to inefficient coolant flow, resulting in a large 'lee zone' and reduced heat transfer efficiency.

Innovation Solution

Cylindrical and conical cooling fins are arranged offset relative to each other, ensuring that the coolant impinges on the fins over their full area, reducing the 'lee zone' and enhancing heat transfer by creating turbulence and mixed streamlines.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If cooling fins are arranged in straight diagonal milling lines at 45 degrees to the flow direction, then the structure is simple to manufacture, but the coolant does not impinge upon the cooling fins effectively and heat transfer potential is not fully exhausted

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidheat transfer efficiency
Core Design Contradiction:
Ease of manufactureVSLoss of energy

Solution Approach 1:

The patent applies asymmetry by offsetting adjacent rows of cooling fins relative to each other, creating an asymmetric pattern that disrupts diagonal flow paths. This asymmetric arrangement forces the coolant to impinge upon the cooling fins more effectively, converting the symmetric diagonal flow pattern into a more effective heat transfer configuration while maintaining manufacturing simplicity through regular offset patterns.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent introduces a new dimensional aspect by adding the offset parameter between adjacent rows, transforming the simple linear arrangement into a two-dimensional offset grid pattern. This dimensional change creates a more complex flow interaction that improves coolant impingement on cooling fins without significantly complicating the manufacturing process.

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

2Device complexity

If cooling fins are arranged in parallel rows with straight diagonal milling lines, then the device complexity is low, but a large lee zone forms behind the cooling fins reducing cooling effectiveness

Engineering Contradiction:
Improvestructural complexityVSAvoidcooling effectiveness
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The asymmetric offset arrangement of cooling fins between adjacent rows disrupts the formation of large lee zones by creating staggered flow paths. This prevents the coolant from creating large low-velocity zones behind the fins, thereby improving cooling effectiveness while maintaining relatively simple device structure through regular offset patterns.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent applies hydraulic principles by optimizing the coolant flow path through the offset fin arrangement. The staggered configuration creates a more uniform distribution of coolant velocity and pressure across the cooling surface, preventing stagnation zones and improving overall hydraulic efficiency of the cooling system.

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Loss of energy

If cooling fins are arranged to maximize coolant contact area, then heat transfer efficiency improves, but the manufacturing precision requirements increase

Engineering Contradiction:
Improveheat transfer efficiencyVSAvoidfin positioning precision
Core Design Contradiction:
Loss of energyVSManufacturing precision

Solution Approach 1:

The patent segments the cooling fin structure into multiple offset rows, where each row can be manufactured and positioned independently. This segmentation allows for modular manufacturing processes that can achieve the required precision through standardized components and assembly procedures, rather than requiring high precision in a single complex structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses parameter changes by specifying the offset distance as a design parameter that can be optimized for manufacturing capabilities. By adjusting the offset parameter within certain ranges, the system achieves effective coolant impingement while accommodating variations in manufacturing precision, making the design robust to manufacturing tolerances.

Inventive Principle:
Principle #35Parameter changes

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 increases heat transfer efficiency by ensuring full contact of the coolant with the cooling fins and reduces the 'lee zone', leading to improved thermal management in power-electronic systems.

Implementation Method 1

coolant flowing past is 'swirled' more effectively, thus providing that the coolant impinges upon the cooling fins over the full area thereof

Methodology Applied
Scientific EffectTurbulence: Turbulence

Implementation Method 2

heat transfer from the heatsink to the coolant is increased

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 3

heat transfer from the heatsink to the coolant is increased over known solutions

Methodology Applied
Scientific EffectHeat transfer: Convection

Implementation Method 4

cylindrical and/or conical cooling fins are formed in a main body, around which a coolant can flow

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Data Source

PatentUS11856739B2Cooling components, converter, and aircraft
Publication Date: 2023.12.26 ROLLS ROYCE DEUT LTD & CO KG
  • US11856739B2 patent drawing
  • US11856739B2 patent drawing
  • US11856739B2 patent drawing

AI summary

The disclosure relates to a device for cooling components. The device includes a main body and cylindrical and/or conical cooling fins which are formed in the main body and around which a coolant may flow, wherein the cooling fins are formed in parallel first rows and equally spaced apart from one another. Neighboring first rows are arranged offset from one another in the row direction in such a way that the axes of neighboring cooling fins of the neighboring first rows are offset by at least 25% of the hydraulic diameter of the cooling fins. The disclosure also relates to a converter and an aircraft including a device of this type.