Set 39 — Energy Storage and EV Charging
Set 38 rode through a grid fault by storing half a megajoule in a spinning rotor for a sixth of a second. Extend that idea from milliseconds to hours and from kinetic to electrochemical, and it becomes the technology both renewable sources ultimately depend on — because both produce power when the resource is available rather than when it is wanted.
A battery is a source unlike any so far. It is bidirectional, so the converter must be too. Its voltage swings 40% with state of charge. It degrades according to how it is used, so the control strategy is part of the product's lifetime. And at the currents modern charging demands — hundreds of amps — the losses that were negligible elsewhere become the design's dominant term.
A pack is defined by its series and parallel counts:
\[ V_{pack} = N_sV_{cell}, \qquad E = V_{pack}Q, \qquad \text{C-rate} = \frac{I}{Q} \]A bidirectional half bridge is a boost one way and a buck the other:
\[ D_{boost} = 1-\frac{V_{bat}}{V_{link}}, \qquad \Delta I = \frac{V_{bat}D}{f_sL} \]Interleaving \(n\) phases divides the current and cancels the ripple:
\[ I_{phase} = \frac{I}{n}, \qquad \Delta I_{total} \ll n\Delta I_{phase} \]A dual active bridge transfers power by phase shift:
\[ P = \frac{V_1V_2'\,\phi\left(\pi-\left|\phi\right|\right)}{2\pi^2f_sL} \]Doubling the system voltage quarters the conduction loss:
\[ I = \frac{P}{V}, \qquad P_{loss} \propto I^2 \;\Longrightarrow\; \text{loss} \propto \frac{1}{V^2} \]Pre-charge limits the inrush into the link capacitance:
\[ \tau = RC, \qquad E_R = \tfrac12CV^2, \qquad t \approx 3\tau \]
An EV pack uses 96 lithium cells in series, nominal 3.7 V, 3.0–4.2 V range, storing 75 kWh. Find the pack voltages, the capacity in ampere-hours, the current and C-rate for a 150 kW DC fast charge, and describe the CC–CV profile and why it exists.
The pack voltages:
A 40% voltage swing from empty to full — wider than the PV string's temperature range in Set 37, and every converter connected to the pack must work across all of it. That range is the single most demanding specification a battery converter faces.
The capacity:
Which for a 96-series pack means each cell is 211 Ah — achieved either with large-format cells or by paralleling many small ones. The choice affects the balancing problem, the thermal design and the failure modes, but not the electrical interface.
The fast-charge current:
Two C — the whole pack's energy delivered in half an hour. Four hundred amps is what makes charging cables heavy and, above about 200 A, liquid-cooled. It also makes every milliohm in the path matter: 1 mΩ of contact resistance dissipates 179 W.
The CC–CV profile:
| Phase | Control | Ends when | SoC reached |
|---|---|---|---|
| Constant current | hold \(I\); voltage rises | \(V_{cell} = 4.2\) V | ~80% |
| Constant voltage | hold \(V\); current tapers | \(I < Q/20\) | 100% |
The split explains the familiar charging curve. The first 80% arrives at full power; the last 20% takes as long again as the current tapers away. That is why manufacturers quote "10 to 80%" times — not marketing, but the physics of the CV phase.
Why the voltage must be held rather than the current. The cell voltage limit is a chemical boundary:
Exceeding it does not merely reduce life — it deposits metallic lithium on the anode, which is both a permanent capacity loss and a route to an internal short. The CV phase exists because the cell's terminal voltage includes its internal \(IR\) drop, so holding a safe terminal voltage while the current falls lets the true cell potential approach the limit asymptotically.
Cell balancing. Series cells are never identical:
| Method | Mechanism | Trade |
|---|---|---|
| Passive | bleed the high cells through a resistor | simple; wastes energy, slow |
| Active (capacitive) | shuttle charge between cells | efficient; more components |
| Active (inductive) | a small converter per cell group | fastest; most expensive |
A 2% spread across 96 cells means the pack delivers 2% less than the sum of its cells until balanced. Passive balancing at a few hundred milliamps takes hours — which is acceptable, because a parked vehicle has hours.
A bidirectional converter links the pack to a 700 V DC link at 150 kW. Find the duty ratio range, size the inductor for 20% ripple at 20 kHz, and show what four-phase interleaving achieves.
The topology. A single half-bridge leg with an inductor on the battery side serves both directions:
| Direction | Operates as | Active device |
|---|---|---|
| Discharging | boost (battery → link) | lower switch |
| Charging | buck (link → battery) | upper switch |
The same two devices, the same inductor, the same duty ratio relationship — only which device is modulated changes. It is the two-quadrant chopper of Set 17 with the machine replaced by a battery, and the transition between directions is seamless because the inductor current simply crosses zero.
The duty ratio range:
| State of charge | \(V_{bat}\) | \(D\) |
|---|---|---|
| Empty | 288 V | 0.589 |
| Nominal | 355 V | 0.493 |
| Full | 403 V | 0.424 |
A comfortable range around 0.5 — nowhere near the extremes where a boost converter's efficiency and right-half-plane zero cause trouble. Choosing the link voltage well above the pack's maximum is what buys that comfort.
The inductor, for 20% ripple at the worst case:
Only a hundred microhenries — but carrying 423 A. That combination is what makes it hard: the core must not saturate at 465 A peak, and the winding must carry 423 A with the skin and proximity effects of Set 24 at 20 kHz. It is the exact mirror of the PV inductor in Set 37 — 4.6 mH at 8.9 A.
Interleaving four phases attacks both difficulties at once:
| Benefit | Detail |
|---|---|
| Current per phase quartered | 106 A — standard devices and inductors |
| Ripple cancellation | phases shifted 90° — total ripple far below \(4\Delta I\) |
| Effective frequency \(4\times\) | 80 kHz at the link — smaller capacitors |
| Conduction loss | \(4\times(I/4)^2R = I^2R/4\) — quartered |
| Thermal spreading | four heat sources, not one |
| Phase shedding | run fewer phases at light load for better efficiency |
Set 18 met ripple cancellation in a two-phase buck; here it is doing four jobs at once. The last row is particularly valuable in a vehicle, where the converter spends most of its life far below rated power — shutting down three phases removes their switching and gate-drive losses entirely.
Where the ripple cancellation is perfect:
And the operating range of 0.42–0.59 straddles the null at \(D = 0.5\) — so the input ripple is near zero at nominal state of charge and modest at the extremes. That is not a coincidence; the link voltage was chosen to put the nominal duty ratio there.
The device choice:
| Requirement | Value |
|---|---|
| Blocking voltage | 700 V + margin → 1200 V |
| Current per device | 106 A phase, 120 A peak |
| Technology | SiC MOSFET |
| Why SiC | lower loss, higher \(f_s\), smaller magnetics, no tail current |
| Body diode | used in synchronous rectification — check \(Q_{rr}\) |
Silicon carbide dominates this application, and Set 39's numbers show why: at 423 A the conduction loss is everything, and a SiC MOSFET's resistive conduction beats an IGBT's fixed \(V_{CE(sat)}\) handsomely at partial load — which is where a vehicle lives.
An 11 kW onboard charger uses an active front end and an isolated dual active bridge from a 700 V link to the 400 V pack at 100 kHz. Find the turns ratio and the transformer leakage inductance for a 45° phase shift at rated power, and explain why a DAB rather than an LLC.
The charger's two stages:
| Stage | Function | Why |
|---|---|---|
| Active front end | sinusoidal input current, unity PF | Set 10's diode bridge would draw 100% THD |
| Isolated DC–DC | galvanic isolation, wide voltage range | safety — the pack must float |
Isolation is a safety requirement, not a convenience: an unisolated charger would connect the pack's chassis-referenced structure directly to the mains. Set 22's isolated topologies exist for exactly this.
The turns ratio:
Choosing \(n\) so that the referred voltages match at nominal is deliberate. A DAB is most efficient when \(V_1 = V_2'\) — the circulating current grows as they diverge, which is why the pack's 40% swing is a real efficiency problem for this topology.
The power transfer law. A DAB moves power by phase-shifting one bridge's square wave against the other's:
The inductor \(L\) — usually just the transformer's leakage — is the energy transfer element, exactly as it was in the LLC of Set 29. Power flows from the leading bridge to the lagging one, so reversing the sign of \(\phi\) reverses the power. That is the whole bidirectional mechanism: one variable, both directions.
Size the inductance for rated power at a 45° shift:
Forty-two microhenries, which a transformer of this rating can provide as leakage alone — so no external inductor is needed. As with the LLC, a parasitic has become a design element.
Why 45° and not more. The power law peaks at \(\phi = \pi/2\):
| \(\phi\) | Relative power | Note |
|---|---|---|
| 30° | 0.74 | — |
| 45° | 0.94 | design point — headroom retained |
| 60° | 1.00 | — |
| 90° | 1.13 (maximum) | no control margin; high circulating current |
Designing at 90° would leave no headroom — any dip in link voltage could not be compensated. Forty-five degrees keeps a comfortable margin while staying in the region where circulating current, and therefore conduction loss, is modest.
DAB against the LLC of Set 29:
| Property | DAB | LLC |
|---|---|---|
| Bidirectional | inherently — reverse \(\phi\) | no (CLLC needed) |
| Control variable | phase shift | frequency |
| Switching frequency | fixed | variable |
| Wide voltage range | moderate — ZVS is lost off-nominal | good |
| Peak efficiency | ~97% | ~98% |
| Circulating current | higher off-nominal | lower |
The first row decides it for a charger that must also support vehicle-to-grid. A DAB reverses power by changing the sign of one variable; an LLC's rectifier is a diode bridge and cannot. The CLLC — a symmetric resonant tank on both sides — is the LLC's bidirectional answer, and modern chargers increasingly use it.
The complete 11 kW specification:
| Item | Value |
|---|---|
| Input | 3-phase 400 V, 16 A |
| Front end | 6-switch active rectifier, THD < 5% |
| Link | 700 V |
| Isolation | DAB or CLLC at 100 kHz |
| Turns ratio | 1.75 |
| Leakage inductance | 42 µH |
| Output | 288–403 V, up to 38 A |
| Efficiency | ~95% overall (two stages) |
| Devices | SiC throughout |
Compare 400 V and 800 V vehicle architectures for a 350 kW charge: find the currents and the relative conduction loss, and identify what else changes and what it costs.
The currents:
Eight hundred and seventy-five amps through a cable a person must lift and plug in. That number alone is why 800 V architectures exist — it is at the edge of what liquid cooling can manage in a handheld connector.
The loss ratio:
Four times the conduction loss for the same delivered power, in every resistive element: the cable, the connector, the contactors, the busbars, the device channels and the motor windings. It is the same argument that put transmission lines at hundreds of kilovolts, applied inside a car.
What that buys, item by item:
| Benefit | Detail |
|---|---|
| Charging cable | lighter, possibly not liquid-cooled |
| Conduction losses | \(4\times\) lower everywhere |
| Cable and busbar mass | halved — significant in a vehicle |
| SiC devices become natural | 1200 V SiC is a mature, high-performance part |
| Motor efficiency | lower current, thinner conductors, less copper |
| Charging time | 350 kW becomes practical rather than heroic |
The fourth row is a quiet but decisive advantage. At 400 V the natural device is a 650 V part, where silicon IGBTs and MOSFETs remain competitive; at 800 V it is a 1200 V part, where SiC's advantage over silicon is large. The architecture change and the device change reinforce each other.
And what it costs:
| Cost | Detail |
|---|---|
| More cells in series | ~192 instead of 96 — more balancing channels |
| Higher-voltage components | contactors, fuses, insulation, sensors |
| Compatibility with 400 V chargers | needs a boost stage or a split-pack trick |
| Insulation coordination | creepage and clearance throughout |
| Service safety | 800 V DC is substantially more hazardous |
| Auxiliary loads | 12 V and 400 V accessories need conversion |
The third row is the practical obstacle. Most installed public chargers are 400 V class, so an 800 V vehicle must be able to accept them — solved either with an extra boost converter or, elegantly, by reconfiguring the traction inverter and motor windings as a boost stage during charging, using hardware the car already carries.
The charging standards landscape:
| Mode | Power | Converter location |
|---|---|---|
| AC Level 1 | 1.4–2 kW | onboard |
| AC Level 2 | 7–22 kW | onboard — Problem 3 |
| DC fast | 50–150 kW | off-board |
| DC ultra-fast | 150–350 kW | off-board, liquid-cooled cable |
| Megawatt (trucks) | > 1 MW | off-board, 1500 V class |
The division is about mass. An onboard charger must be carried everywhere and is therefore limited to a few tens of kilograms; a DC charger sits on the ground and can weigh whatever it needs to. That is why DC charging bypasses the vehicle's converter entirely and talks straight to the pack.
What limits charging speed in practice. Not the converter:
| Limit | Consequence |
|---|---|
| Lithium plating | permanent capacity loss; worse when cold |
| Heat generation | \(I^2R_{internal}\) — needs active cooling |
| CV taper | the last 20% cannot be hurried — Problem 1 |
| Cell temperature | the pack is pre-conditioned before a fast charge |
A well-designed 350 kW charger will still deliver far less than 350 kW to a cold pack, because the battery management system limits the current to protect the cells. Vehicles now pre-condition the pack en route to a charger for exactly this reason — heating the battery so it can accept the power on arrival.
Assess the impact of a site with four 350 kW chargers on a distribution network, describe how stationary storage buffers it, and explain what vehicle-to-grid offers and what it costs the battery.
The connected load:
Comparable with a small factory, appearing at a motorway service area or a supermarket car park — locations whose existing supply was sized for lighting and refrigeration. The connection upgrade, not the chargers, is usually the dominant project cost.
What makes it harder than a factory load:
| Characteristic | Consequence |
|---|---|
| Very low diversity | all four can start within seconds of each other |
| Fast ramps | 0 to 350 kW in seconds — voltage step |
| Coincident with evening peak | drivers charge when they arrive home or stop |
| Low utilisation | 1.4 MW connection used a few hours a day |
| Harmonics | manageable — active front ends |
The fourth row is the economic problem. Paying for a 1.4 MW connection that is used at 15% capacity factor is expensive, which is precisely the gap that on-site storage fills.
Buffering with stationary storage. Size a battery to cover a charging session from a modest grid connection:
A 370 kWh buffer — about five vehicle packs — lets a 300 kW connection serve a 1.4 MW site, recharging between sessions. The economics compare the storage cost against the connection upgrade, and at many sites the battery wins outright.
Vehicle-to-grid inverts the relationship. A parked fleet is a large distributed battery:
| V2G service | Value | Energy throughput |
|---|---|---|
| Frequency response | highest paid | very low — seconds at a time |
| Peak shaving | moderate | moderate |
| Energy arbitrage | lowest | high — full cycles |
| Backup power (V2H) | situational | occasional |
Read the first and third rows together. Frequency response pays best and cycles the battery least — a few kilowatt-hours moved back and forth per day — while arbitrage pays least and consumes real cycle life. The economics therefore favour the service that barely touches the battery.
The cost to the battery, which V2G proposals often understate:
Nearly seven pence per kilowatt-hour of throughput, before any efficiency loss — which exceeds the arbitrage spread in most markets. That single figure explains why V2G deployment has concentrated on frequency response and why energy arbitrage from vehicle batteries remains largely theoretical.
What makes it work anyway:
| Enabler | Detail |
|---|---|
| Bidirectional charger | the DAB of Problem 3 — no extra cost |
| Aggregation | thousands of vehicles as one dispatchable resource |
| Smart charging first | shifting when to charge captures most of the value with no degradation |
| Falling cell cost | reduces the degradation charge per kWh |
| Second-life packs | retired vehicle batteries as stationary storage |
The third row deserves emphasis. Simply choosing when to charge — overnight rather than at the evening peak — delivers most of the grid benefit of V2G with none of the extra cycling. Unidirectional smart charging is the low-hanging fruit, and V2G is the refinement.
Specify the battery management and safety system: state-of-charge estimation, the pre-charge circuit for a 500 µF link at 400 V, isolation monitoring and the contactor sequence. Compute the pre-charge time and resistor energy.
State of charge estimation. No sensor measures it directly, so it must be inferred:
| Method | Principle | Weakness |
|---|---|---|
| Coulomb counting | \(\text{SoC} = \text{SoC}_0-\frac{1}{Q}\int i\,dt\) | drifts — an open integrator |
| Open-circuit voltage | lookup against a curve | needs hours of rest; flat for LFP |
| Impedance | measure internal resistance | temperature-dependent |
| Kalman filter | a model corrected by voltage measurement | the standard approach |
Coulomb counting is accurate in the short term and drifts without bound — the same integrator problem as the sensorless flux estimator of Set 35. Combining it with an OCV correction in a Kalman filter gives the short-term accuracy of the integral with the long-term anchoring of the measurement.
The pre-charge problem. Closing a contactor onto a discharged link capacitor is a short circuit:
The contactor welds shut, which is a dangerous failure: a welded main contactor cannot disconnect the pack in a crash or a fault. Pre-charge is a safety system, not merely a component protection.
The pre-charge circuit:
Exactly half the energy delivered ends up in the resistor regardless of its value — a classic result. Forty joules in 150 ms is 267 W average, so the resistor is rated for a pulse rather than continuously, exactly like the soft starter of Set 30 and the wind chopper of Set 38.
The contactor sequence:
| Step | Action | Check |
|---|---|---|
| 1 | Close the negative contactor | — |
| 2 | Close the pre-charge contactor | — |
| 3 | Wait 150 ms | verify \(V_{link} > 95\%\) of \(V_{bat}\) |
| 4 | Close the main positive contactor | — |
| 5 | Open the pre-charge contactor | — |
| 6 | Enable the inverter | — |
Step 3's check is essential. If the link voltage does not rise, something is drawing current — a short in the inverter, a failed capacitor — and closing the main contactor onto that fault would be destructive. The pre-charge doubles as a diagnostic.
Isolation monitoring. The pack floats relative to the vehicle chassis:
Measured continuously, because a single insulation failure is not itself hazardous — a floating system tolerates one fault — but a second one completes a circuit through the chassis. The monitor's job is to catch the first fault before the second arrives, which is the same philosophy as an IT earthing system in a hospital.
The complete BMS:
| Function | Purpose |
|---|---|
| Cell voltage monitoring | all 96, to a few millivolts |
| Temperature monitoring | multiple points — gradients matter |
| Current measurement | for coulomb counting and protection |
| SoC and SoH estimation | range prediction and degradation tracking |
| Cell balancing | Problem 1 |
| Thermal management | cooling under charge, heating before fast charge |
| Contactor and pre-charge control | the sequence above |
| Isolation monitoring | continuous |
| Charge/discharge current limits | as functions of SoC and temperature |
| Fault detection and logging | diagnostics and warranty |
The last functional row is what actually governs the vehicle's behaviour: the BMS publishes a maximum permitted current that varies with temperature and state of charge, and every converter in the vehicle obeys it. The 350 kW charger of Problem 4 delivers whatever the BMS allows.
Key Formulas
| Quantity | Relation | Notes |
|---|---|---|
| Pack voltage | \(V = N_sV_{cell}\) | 288–403 V for 96S |
| Capacity | \(Q = E/V_{nom}\) | 211 Ah |
| C-rate | \(I/Q\) | 2C at 150 kW |
| CC–CV | CC to \(V_{max}\), then CV | ~80% at the transition |
| Bidirectional duty | \(D = 1-V_{bat}/V_{link}\) | 0.42–0.59 |
| Inductor | \(L = \dfrac{V_{bat}D}{f_s\Delta I}\) | 104 µH at 423 A |
| Interleaving | \(I_{phase} = I/n\); loss \(\propto 1/n\) | Ripple nulls at \(D = k/n\) |
| DAB power | \(P = \dfrac{V_1V_2'\phi(\pi-|\phi|)}{2\pi^2f_sL}\) | Sign of \(\phi\) reverses it |
| DAB inductance | \(L = \dfrac{V_1V_2'\phi(\pi-\phi)}{2\pi^2f_sP}\) | 41.8 µH |
| DAB maximum | at \(\phi = \pi/2\) | Design at 45° for margin |
| Voltage and loss | \(P_{loss} \propto 1/V^2\) | 800 V quarters it |
| Fast-charge current | \(I = P/V\) | 875 A at 400 V, 438 at 800 |
| Buffer storage | \(E = \left(P_{peak}-P_{grid}\right)t\) | 367 kWh |
| Degradation cost | \(\dfrac{\text{pack cost}}{\text{cycles}\times\text{usable kWh}}\) | ~£0.067/kWh |
| Pre-charge | \(\tau = RC,\ t \approx 3\tau,\ E_R = \tfrac12CV^2\) | 50 ms, 150 ms, 40 J |
| Isolation | \(R_{iso} \ge 100\ \Omega/\text{V}\) | 40 kΩ at 400 V |
Common Mistakes
Designing a battery converter for nominal voltage only. The pack swings 40% from empty to full — Problem 1.
Assuming charge time scales inversely with power. The CV taper adds as long again past 80% — Problem 1.
Ignoring cell balancing. The weakest cell terminates the charge for all 96 — Problem 1.
Sizing a single-phase converter for 423 A. Interleaving makes the inductor and devices ordinary — Problem 2.
Choosing a DAB turns ratio away from the nominal match. Circulating current and loss of ZVS follow — Problem 3.
Designing a DAB at 90° phase shift. It is the maximum, so no control margin remains — Problem 3.
Using an LLC where bidirectional flow is needed. Its output rectifier blocks — a CLLC or DAB is required — Problem 3.
Assuming an 800 V vehicle can ignore 400 V chargers. Most public infrastructure is 400 V class — Problem 4.
Costing V2G without battery degradation. Around 7p per kWh cycled exceeds most arbitrage spreads — Problem 5.
Omitting pre-charge. The main contactor welds, and a welded contactor cannot disconnect the pack — Problem 6.
Six problems on the technology that both renewable sources depend on. A 40% voltage swing shaped every converter around the pack; a 423 A inductor became four ordinary ones through interleaving; a dual active bridge reversed 11 kW by changing the sign of one variable; doubling the system voltage quartered the loss in every conductor; and a battery management system turned out to set the limits that every converter in the vehicle obeys.
What connects Sets 37 to 39 is that all three sources are converter-connected. A photovoltaic array, a wind turbine and a battery each reach the grid through a controlled inverter rather than through a synchronous machine bolted to it — and that changes the network fundamentally. A converter contributes almost no inertia, limits its fault current to about its rating, and can be told to do things a generator cannot: inject reactive power at zero output, respond to frequency in milliseconds, or transmit power along a cable that no AC line could use.
Next: Set 40 closes the book — HVDC, FACTS and Power Quality, where a modular multilevel converter stacks 1920 submodules to reach 321 output levels with no filter at all, a STATCOM is shown to hold its current where an SVC's collapses with voltage, series compensation doubles a line's capability and risks resonating with a turbine shaft, and an active filter is sized against the very rectifier that Set 10 built.