Hydrogen-Combustion Turbofans

Engines

Jet-class thrust using compressed gaseous H₂ (350–700 bar), paired with a combustor targeting ultra-low NOx, cert-aligned controls, and airport-ready storage & delivery. Built for rapid iteration—and certification from day one.

Engines first. Aircraft family next. Evidence-driven, exportable across authorities.

Why Engines First

Engines are the certification and performance anchor. Proving ultra-low NOx, stability, and safety unlocks real operations faster than re-inventing the entire aircraft stack upfront.

Known Turbomachinery

Adapt proven cores; focus R&D on combustor, controls, and fuel delivery.

Airport-Ready H₂

Start with gaseous H₂ at 350–700 bar to reduce ground complexity.

Cert From Day One

Evidence aligned to ARP4754A/ARP4761, DO-160, DO-178C and engine norms.

How the System Works

  1. Storage & Delivery: Type-IV tanks store gaseous H₂ at 350–700 bar. Manifolds, PRDs, regulators, ventilation, and leak detection enforce safe delivery to the engine.
  2. Mixing & Combustion: Lean-premix/micromix modules achieve rapid, uniform mixing and stable flame fronts, minimizing thermal NOx and suppressing flashback.
  3. Controls & Transients: Metering and logic manage ignition, start sequences, throttle response, and blowout margins under pressurized conditions.
  4. Evidence Pipeline: Test data flows into NOx/stability maps, HAZOP/FMEA updates, and means-of-compliance artifacts across authorities.
diagram-engine.jpg

Architecture evolves with pressurized single-sector data; modules are designed to be reused across engine families.

Engine Design Principles

Evidence-first engineering that turns every test point into certification artifacts and operational playbooks.

  • Ultra-low NOx: staged mixing, temperature management, and geometry tuning.
  • Flashback-safe: clear stability margins under pressurized hot-fire conditions.
  • Airport-pragmatic: fueling, ventilation, and turnarounds that scale.
  • Controls-led: transients, ignition, and anomaly monitoring.
  • Cert-aligned: ARP4754A/4761 flow from requirements → analysis → test → evidence.

Targets & Metrics

Quantitative goals guide design trades and evidence collection.

NOx Emissions
Ultra-low vs. kerosene baselines
Pressurized map across φ / load.
Flashback Margin
Robust through transients
Ignition/blowout boundaries mapped.
Turnaround Time
< 25 minutes (target)
Rapid refuel, purge, leak detection.
Availability
> 98% test uptime
Hot-swap modules; spares strategy.
Fuel Delivery
Stable to 700 bar
PRD, regulation, ventilation verified.
Control Response
Smooth transients
Command tracking, surge/no-stall margins.
Ops Readiness
Airport-pragmatic
Procedures tested with ops partners.
Data Quality
Automated artifacts
Traceable results → cert packs.

R&D Sequence

  • M1: Single-sector cold-flow + ignition; characterize flashback margins.
  • M2: Pressurized single-sector hot-fire; initial NOx & stability maps.
  • M3: Core-engine H₂ ground-run plan; integration & safety reviews (DOA/ODA partners).
  • M4: Multi-authority cert mapping; airport pilots across 2–3 countries.

Test Assets

  • • Pressurized single-sector rig with optical access
  • • NOx analyzers, high-speed sensing, DAQ & logging
  • • Safety interlocks, purge, ventilation, leak detection
  • • Automated report generation & traceability

Airport Ops Playbook

Procedures and facility interfaces to scale hydrogen operations without cryogenics.

Fueling & PRD
Validated PRD strategies, purge, ventilation
Turnarounds
Refuel & checks under 25 min target
Detection
Leak-before-burst, sensor coverage, alarms
Maintenance
Module swaps, inspection intervals

Certification & Safety Mapping

Artifacts flow cleanly into authority-specific packs

ARP4754A / 4761

System process, FHA/PSSA/SSA; hazards traced to design mitigations and test evidence.

DO-160 / DO-178C

Environmental qualification + software lifecycle. Advisory AI kept out of safety-critical path.

Engine / Airport Norms

Means-of-compliance for engines + ground operations across multiple authorities.

Partner With Us

We co-develop modules and share test data to accelerate certification-ready products.

Combustor Modules
Micromix variants, injectors, liners, optical rigs.
Storage & Delivery
Type-IV tanks, PRD, manifolds, ventilation & detection.
Controls & SW
Transient handling, analytics, advisory AI pipelines.
Airport Pilots
Turnaround playbooks, fueling bays, maintenance flows.

FAQs

Is the aircraft electric?
No. We use hydrogen combustion in turbofans, not fuel cells/propellers.
Why gaseous H₂ instead of liquid?
Removes cryogenic complexity and accelerates testing; 350–700 bar is a practical on-ramp for early deployments.
How do you manage NOx?
Lean-premix/micromix geometry, staged mixing, control regimes—validated with pressurized stability & emissions maps.
Where do you operate?
Liberia, Costa Rica (LIR) for rapid iteration, exporting evidence and playbooks to partners globally.
What about safety?
PRD strategies, ventilation, purge, leak detection, interlocks; HAZOP/FMEA feed authority-specific means-of-compliance.
When flight?
Core-engine ground run precedes flight testbed work with DOA/ODA partners per roadmap.