The typical areas of focus for design priorities when considering the strategic approach to power solutions are on the Size, Weight, and Power (SWaP) factors, sometimes also known as SWaP-C (including. the Cost element) factors. SWaP is particularly important in applications for power systems such as
mobility (especially e-mobility), MIL-Aerospace,
portable medical and high-end transportation such as
railway applications. As we shall expand upon, the optimization of these SWaP factors can often be in conflict so there are no universal rules for maximizing each, which makes finding the right balance for your system and application more of a creative art than a rote process.
In many situations, design priority conflicts must contend with physics outside of an engineer’s control. This can be doubly challenging when trying to meet business and performance goals, where simplicity reigns supreme. As such, the benefits of simplified decision processes and costing models can be somewhat at odds with a more accurate, informed process. For example, take the dollar/watt ($/W) metric, which attempts to benchmark power supply costing by evaluating the basic ratio of unit cost to max (continuous) rated output power.
Design engineers throughout the industry are asked to utilize this metric to evaluate power supply designs and to drive the selection process of solutions. However, this metric can become particularly challenging as the power train (and therefore max power rating) of a solution is commonly not the linear driver of TCO costs.
For applications with specialty needs for spacing/safety, hermetic sealing, chassis materials/coatings, filtering, or even connectors – a single one of these specialty components can cost nearly as much as the rest of the power supply BOM and therefore wildly skew the $/W metric. A simple example of this is shown in the figure below, which compares a handful of 300 W, ac-dc solutions.
Fig. 1: Comparison of Multiple Versions of 300 W ac-dc Power Solutions with $/W Metric [1]
A sampling of some application-specific design nuances and challenges can be found in the table below. We will address how to approach some of these design tradeoffs in the following sections of this whitepaper.
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Example Application Specialized design / support requirements |
MIL-AEROSPACE |
- Numerous governmental standards (DO, MIL-STD, etc.) to meet in addition to standard power supply and system qualification requirements (UL, ISO).
- Highest targets for SWaP factors concurrent with highest reliability factors. Every gram of power solution translates directly to fuel/energy costs. Also consider if a soldier must carry.
- Extremes of environmental performance (temperature, humidity, shock, elevation, corrosion/ingress, etc.).
- Supporting redundant power/system implementations.
|
TRANSPORT / RAILWAY |
- Very stringent shock/vibration and other environmental specs to meet (see EN 50155, AEC-Q200 for example).
- “Functional failures” can mean catastrophic damage and loss of life.
- Very large systems make prototype testing challenging and expensive.
- Increased requirement for simulation/modeling.
|
MEDICAL IMAGING |
- Very stringent limits on leakage currents.
- Needs very high isolation voltages (kVs) with increasing spacing specs and stricter safety limits.
- Medical grade EMI limits.
- Systems can be modalities with very sensitive data signals, which may also be susceptible to thermal as well as electrical interference.
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Table 1: Simple Summary of Specialized Requirements for Some Key Application Focus Areas