QDTB® Transformer
All figures are configurator-generated feasibility-level estimates; drawings are schematic deliverables pending refinement by a licensed design institute, not construction documents.
All Solutions

500 kW Airport Power: 400 Hz GPU + Runway Lighting + UPS on a Dual-Feed N+1 Scheme

2×SCB13-500/10 N+1 · 400 kW diesel standby · 150 kVA UPS (15 min) · 400 Hz GPU bridge

1 · TL;DR Conclusion

Conclusion: this 500 kW airport uses a 10 kV feed + 2×SCB13-500/10 dry transformers (N+1), with a 400 kW standby diesel and a 150 kVA UPS covering 100% of the grade-1 runway/ATC load. The 400 Hz GPU bridge drives THDi to 30%, so the 150 kvar PFC is detuned and an APF is recommended — configurator total ≈ $456,014 (feasibility-level).

  • •2×500 kVA SCB13 dry transformers N+1; 84% loading after one-unit loss, within the 60–85% band
  • •Dual-supply chain: grid 10 kV + 400 kW diesel + 150 kVA UPS = 550 kW backup, exactly covering grade-1 (500) + fire (50)
  • •400 Hz GPU converters put 150 kW nonlinear (30% THDi); 150 kvar detuned PFC prevents resonance, an APF clears the limit
  • •150 kVA UPS (120 kW, 15 min, 384 Vdc) holds ATC/comms across the 2 s diesel transfer
  • •Short-circuit 28.9 kA (MV) / 17.6 kA (LV); 300 mm² cable passes thermal check (44 mm² min)

2 · Solution Overview

An airport is a grade-1, high-reliability site: runway/approach lighting, ATC and comms cannot go dark. This 500 kW scheme combines a 10 kV utility feed, N+1 dry transformers, a 400 kW standby diesel and a 150 kVA UPS, with the 400 Hz ground-power (GPU) bridge load modelled as a 150 kW nonlinear source.

2×500 kVA (N+1)
Transformer capacity
SCB13-500/10
Transformer model
10 kV / 0.4 kV
Voltage
400 kW diesel + 150 kVA UPS
Backup
500 kW
Installed load
400 kW (kd 0.8)
Demand
150 kvar (4×38)
PFC
30% (400 Hz GPU)
THDi
SourceRoleShare kWShare
Grid 10 kVbase400 kW100%
Diesel 400 kWbackup0 kW0%
UPS 150 kVAbackup0 kW0%

3 · Design Process & Rationale

1. Requirement identification

An airport is grade-1 — runway lighting, ATC and comms must not lose power; the 400 Hz GPU bridge is a variable-frequency nonlinear load. We set: allowed outage ≤15 s, fire load on a dedicated circuit, and UPS-backed sensitive loads (ATC/radar).

2. Load classification

All 500 kW is treated as grade-1 (airport practice): critical 300 kW, nonlinear 150 kW (400 Hz converters), sensitive 150 kW (ATC), fire 50 kW. This profile drives the source mix and harmonic treatment.

3. Source & mix

Dual-supply structure: grid 10 kV as base (100%), plus a 400 kW standby diesel and a 150 kVA UPS forming the emergency chain — 550 kW backup = grade-1 (500) + fire (50); V9 check reports 100% coverage.

4. Transformer sizing

Apparent demand Sd=400/0.95≈421 kVA → 500 kVA tier; for single-unit-failure continuity we select N+1 → 2×SCB13-500/10 dry-type (indoor, oil-free, fire-friendly), 84% loading.

5. Distribution & protection

MV KYN28A-12 incomer → 2 dry transformers → MNS LV bus (with bus-tie). Protection uses 50/51 overcurrent with 0.3/0.2 s grading; all 5 coordination pairs pass.

6. Reactive & harmonics

Target PF 0.95 needs 150 kvar (4×38 kvar detuned banks). The 400 Hz drives push THDi to 30%, far over the 15% limit: detuned reactors only prevent amplification — an APF is needed to actually clear it.

7. Reliability & special requirements

N+1 keeps 84% loading after one-unit loss; the diesel takes over within 2 s while the UPS holds ATC for 15 min; runway lighting and indoor GPU circuits are fed separately to avoid interference.

Pain Points → Solution → Evidence

Pain

Runway lighting cannot go dark — one feed loss must not black out the airfield

Solution

Dual supply + N+1: grid + 400 kW diesel + 150 kVA UPS emergency chain

Evidence

V9: 550 kW backup = grade-1 500 + fire 50 (100%); V4 N-1 84% loading pass

Pain

400 Hz GPU converters distort the bus and overheat the capacitor bank

Solution

150 kvar detuned reactors prevent resonance, plus an APF to clear the exceedance

Evidence

Load profile THDi 30% (150/500 kW nonlinear), far over the 15% limit

Pain

ATC/comms glitch during the grid-to-diesel transfer

Solution

A 150 kVA UPS (15 min) bridges sensitive loads seamlessly

Evidence

UPS 150 kVA/120 kW · 15 min · 384 Vdc · 97 Ah, spanning the 2 s transfer

Pain

Indoor substation oil/fire risk

Solution

SCB13 dry-type transformer (oil-free, flame-retardant)

Evidence

transModel SCB13-500/10 dry-type — indoor, fire-friendly

4 · Key Parameter Deep-Read

ParameterValueBasisImpact & Boundary
Transformer capacity500 kVA ×2 (N+1)Sd=400/0.95≈421 kVA → 500 kVA tier; N+1 → 2 units84% loading, economical; no outage on single-unit loss
Rise to 630 kVA if demand >450 kW
Backup coverage550 kW (diesel 400 + UPS 150)grade-1 500 + fire 50 = 550V9 100% backup, zero loss for critical loads
Add diesel/UPS if critical load grows
THDi30%400 Hz converters are a concentrated nonlinear load (150 kW)Over the 15% limit; detuned PFC + APF required
APF rating finalised from the harmonic spectrum
UPS rating150 kVA / 120 kWHolds ATC/comms (sensitive) for 15 min384 Vdc battery 97 Ah, zero-gap transfer
Add battery strings for longer runtime
N-1 loading84%Sd 421/500 after one-unit loss2 s transfer ≤ 15 s allowed, verdict pass
Single unit may overload as load grows
Short-circuitMV 28.9 / LV 17.6 kA500 MVA fault level + uk=4% transformerHV 31.5 kA / LV 25 kA breaking (1.1×/1.4× margin)
Confirm actual fault level with grid (toConfirm: ssc)
PFC150 kvar (4×38)avgPf 0.85 → pfTarget 0.95 gapPF compliant, less transformer loading & loss
400 Hz harmonics — detuned to prevent 5th/7th amplification

5 · Drawing Deep-Read

Dwg 3/26Single-line diagram — 10 kV feed → KYN28A-12 → 2×SCB13-500/10 → MNS LV bus → runway / GPU / ATC feeders
Why: The SLD is the backbone: it shows the dual-supply structure — grid, diesel and UPS all feed the LV bus, N+1 means either transformer can drop without outage, and runway lighting vs 400 Hz GPU are on separate feeders. This is the structural guarantee behind “runway lighting cannot go dark”.
Dwg 4/26System topology — Grid 10 kV (base) + 400 kW diesel (backup) + 150 kVA UPS (online) → LV bus
Why: The topology pins each source to its voltage level: grid on MV, diesel and UPS on LV, with any cross-voltage link forced through the transformer. It visually confirms the dual-supply wiring has no conflict.
Dwg 12/26Power quality assessment — THDi 30% > 15% limit · 150 kvar detuned + APF recommended
Why: The PQ drawing quantifies the 400 Hz bridge harmonic risk: THDi 30% is double the 15% limit, so detuned reactors only stop amplification — an APF is mandatory to clear it. This is direct evidence for the “harmonics burn capacitors” pain point.
Dwg 14/26Protection configuration — 50/51 overcurrent · incomer 0.6 s → transformer 0.3 s → feeder 0.1 s, 5 pairs pass
Why: The protection drawing places every stage and setting: MV incomer, transformer, LV incomer and feeder are graded at 0.6/0.3/0.1 s so a downstream fault only trips its own circuit — no single fault blacks out the whole airport.
Dwg 15/26TCC protection coordination curve — Incomer 50/51 (0.6 s) → LV incomer (0.3 s) → feeder (0.1 s), 0.3/0.2 s grading
Why: The TCC proves selectivity: a downstream fault only trips its feeder while the upstream breakers hold. All 5 pairs meet the ≥0.2 s grading criterion.

The following drawings are shown for reference (full set in the configurator “View design document”):

Dwg 1 · Electrical design basisDwg 2 · Symbol legendDwg 3 · Single-line diagramDwg 4 · System topology diagramDwg 5 · Distribution systemDwg 6 · MV distribution systemDwg 7 · LV distribution systemDwg 8 · Short-circuit calculationDwg 9 · Applicable codes & standardsDwg 10 · Main equipment technical dataDwg 11 · Construction & testing requirementsDwg 12 · Power quality assessmentDwg 13 · SCADA architectureDwg 14 · Protection configurationDwg 15 · TCC protection coordination curveDwg 16 · Grounding systemDwg 17 · Lightning & surge protection (LPS/SPD)Dwg 18 · Equipment layout planDwg 19 · Reactive & harmonic compensationDwg 20 · Microgrid grid-tied / islanding transferDwg 21 · Secondary control & signal circuitDwg 22 · Terminal strip (protection & control panels)Dwg 23 · Panel front layout & panel scheduleDwg 24 · DC auxiliary power systemDwg 25 · Fuel oil systemDwg 26 · Earthing system (TN-S)

6 · Operation Demo (Deep-Read)

Energy flow

Grid 400 kW demand → MV switchgear → two SCB13 transformers → LV bus → 14 feeders (runway / GPU / ATC). The dual transformers share ~42% each; on one-unit loss the survivor carries 84%.

Fault & transfer

On grid loss the diesel synchronises within 2 s while the UPS holds ATC for 15 min; a feeder fault trips only that feeder (0.1 s) with the upstream 0.3 s holding — selectivity holds.

Power quality & harmonics

The 400 Hz bridge puts THDi at 30%; compare the harmonic spectrum before/after detuned-reactor + APF treatment to quantify the cause and fix of “harmonics burn capacitors”.

Losses & electricity cost

Dry-type losses p0=1.16 / pk=4.88 kW, ≈102,071 kWh/yr (≈$12,249 @ $0.12/kWh); an SH15 amorphous oil unit would save ≈7,434 kWh/yr but trades away the oil-free safety.

Other views (shown): 24h operation · Voltage profile · Scheme features · Environmental derating

7 · Economics & Payback

Configurator equipment total ≈ $456,014 (feasibility-level, incl. 2×SCB13-500/10 dry transformers, MV/LV switchgear, 500 kVA containerised diesel, 150 kVA UPS, 150 kvar PFC and cables). Economics centre on the reliability premium plus losses: ≈102,071 kWh/yr ($12,249); an SH15 amorphous oil unit would save ≈$892/yr, but indoor airports prefer oil-free dry type — safety over efficiency.

$456,014
Equipment total
102,071 kWh
Annual losses
$12,249/yr
Loss cost
$892/yr
SH15 saving
550 kW (100%)
Backup coverage

8 · FAQ

What transformer size for a 500 kW airport?
At kd=0.8 the demand is 400 kW ≈ 421 kVA → 500 kVA tier; for no-outage on single-unit failure use 2×500 kVA N+1 (84% after one-unit loss).
Why dry-type for an airport?
Indoor airport substations are fire-sensitive; SCB13 dry-type is oil-free and flame-retardant. It costs slightly higher no-load loss than amorphous oil, but safety wins.
How big a standby diesel for an airport?
Grade-1 500 + fire 50 = 550 kW must be 100% covered; diesel 400 kW + UPS 150 kVA = 550 kW, with the diesel realised as a 500 kVA containerised genset.
What is a 400 Hz GPU and why does it affect the design?
The 400 Hz ground-power unit is a frequency converter feeding aircraft on the apron — a concentrated nonlinear load that pushes THDi to 30%, requiring detuned PFC plus an APF.
How long does the UPS hold?
The 150 kVA/120 kW UPS here backs up for 15 min (384 Vdc, 97 Ah) — plenty to span the 2 s diesel transfer; add battery strings for longer runtime.
What backs the runway lighting?
Runway lighting is grade-1: normally fed from the dual-transformer LV bus; on grid loss the 400 kW diesel takes over with the UPS bridging — zero outage.
Why N+1 dual transformers?
An airport cannot stop entirely on a single transformer failure; N+1 gives 84% loading after one-unit loss, 2 s transfer ≤ 15 s allowed — pass.
Is 30% THDi a problem?
Yes — double the 15% limit. Detuned reactors only stop resonance; an APF is required to clear it, otherwise the capacitor bank overheats and fails.
What does the airport package cost?
Configurator total ≈ $456,014 (feasibility-level), covering dual transformers, MV/LV switchgear, diesel, UPS and PFC; contact our engineers for a formal quotation.

Special Considerations

  • System fault level defaults to 500 MVA — confirm the actual value with the grid company (affects protection settings & cable thermal; toConfirm: ssc).
  • THDi ~30% is over the limit; detuned reactors only prevent amplification — add an APF to actually clear the warning.
  • All 500 kW is treated as grade-1; if some terminal loads can be de-rated, the diesel/UPS backup (and cost) can shrink.
  • Feasibility-level estimate; drawings pending a licensed design institute, not construction documents.

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