Board-Level Thermal Analysis
Theory: the board as a heat spreader
Overview
In board thermal analysis, must copper traces and planes be modelled in detail?
Usually an effective conductivity reflecting each layer's copper suffices — but treating the board as anisotropic is essential, since in-plane and through-plane conductivities differ completely. Copper spreads heat well in-plane, but through-plane heat must cross FR-4 layers. The number of copper layers sets how far heat spreads around a hot component, and with it the component temperature. Let's calculate a 1 W component on a 50 mm board.
Effective conductivity
In-plane is parallel, through-plane series. Even a few percent of copper (390 W/mK) by thickness multiplies in-plane conductivity tens of times, while through-plane remains set by FR-4 (0.3 W/mK).
Spreading in the plate
The board is solved in 2D as a thin plate (fin) losing heat from both faces. The rise $\Delta T_{min}$ for a uniformly hot board is a floor that no amount of spreading can beat.
When boards became heat paths
In older electronics, component heat left mainly to the surrounding air. As surface-mount parts shrank and designs soldered bottom thermal pads to the board, most heat began flowing into the board. In board thermal design, copper planes placed for power and ground become the main heat spreaders too, so entering the stack-up and copper content correctly became essential.
Worked example: 1 W at the centre of a 50 mm board
1.6 mm thick; FR-4 0.8 in-plane, 0.3 through-plane W/mK; 35 µm copper. A 5 mm, 1 W component; both faces lose heat to 25 °C air; solved as a 2D plate ignoring through-thickness gradients.
| Stack-up | In-plane | Through-plane | Peak rise h = 10 | Peak rise h = 30 |
|---|---|---|---|---|
| 2-layer, 30% surface copper | 5.9 W/mK | 0.31 W/mK | 61.7 K | 42.4 K |
| 2-layer, full surface copper | 17.8 W/mK | 0.31 W/mK | 36.8 K | 20.5 K |
| 4-layer, two inner planes | 22.9 W/mK | 0.33 W/mK | 33.9 K | 17.8 K |
| 6-layer, four inner planes | 40.0 W/mK | 0.35 W/mK | 29.6 K | 13.7 K |
Heat transfer coefficients in W/m²K. The floor for a uniformly hot board is 20 K at h = 10 and 6.7 K at h = 30.
Under natural convection, even 6 layers only reach 30 K, already near the 20 K floor.
Board temperature rise has two stages: spreading heat around the component, and releasing it from the board surface to air. More copper layers improve the first, cutting 62 K (2-layer, 30% copper) to 30 K. But the second depends only on board area and h; at natural-convection 10 W/m²K a fully spread board still rises 20 K, leaving the 6-layer board only 10 K to gain. With airflow (h = 30) every stack-up drops a lot — 14 K for 6 layers. Identifying the bottleneck is the first step of thermal design.
Analysis tips
- Compute in-plane and through-plane effective conductivities from each layer's copper thickness and coverage.
- Model thermal vias and pads in detail under hot components.
- Compare with the uniform-board floor to find the bottleneck.
- Inside enclosures, use the internal air temperature, which is elevated.
- Solve the whole board, including mutual heating between neighbouring parts.
“Splitting a power plane made it hotter”
In one board revision, inner planes were finely split to add power rails, and a hot component ran over 10 K hotter. Electrically the change was fine, but the fragmented planes broke the in-plane heat-spreading path. Moving the splits away from hot components to preserve a heat path restored the temperature. Layout changes affect heat too.
Common mistakes
Mistakes and fixes
| Mistake | Effect | Fix |
|---|---|---|
| Isotropic board | Through-plane overrated | Use anisotropy |
| FR-4-only conductivity | Temperatures too high | Include copper |
| Assuming 100% coverage | Temperatures too low | Actual coverage |
| Adding copper, ignoring air side | Diminishing returns | Compare with the floor |
| Ignoring plane splits | Local hot spots | Reflect actual pattern |
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