민간 항공을 위한 지속적인 공기역학 및 엔진 디지털 트윈

AirplaneTwins는 압축기 블레이드 오염과 기체 항력 증가를 분석하여 최적의 엔진 세척 주기를 결정하고 항공유 소비를 절감합니다.

AirplaneTwins Fleet Simulation Architecture

Turbofan Thermodynamic Solver, Transonic Drag Model, and Fleet Optimization

Central System: Fleet Physics Simulation Core - High-Fidelity Engine & Aero Model

Aviation Architecture Nodes

  • Full Authority Digital Engine Control (FADEC) Stream
  • Turbofan Stage Thermodynamic Solver
  • Transonic Surface Roughness Monitor
  • Atmospheric 4D Weather Matcher
  • Cockpit Fuel-Optimal Flight Profile Engine

Architectural Layers & Protocol Stacks

  • FADEC High-Frequency Telemetry Ingestion (ARINC 429 to IP Gateway / Lossless Telemetry Compression / FADEC Adapter): Continuous real-time ingestion of 120+ engine parameters: N1/N2 rotor speeds, exhaust gas temperature (EGT), fuel flow, and variable bleed valve positions.
  • Gas Turbine Thermodynamic Cycle Simulation (Zero-D/1-D Gas Path Analysis / Extended Kalman Filter State Estimation): Physics-based thermodynamic modeling of the Brayton cycle calculating compressor efficiency drops, high-pressure turbine blade creep, and thermal stress.
  • Transonic Aerodynamic Drag Tracking (Euler Aerodynamic Estimator / Machine Learning Drag Penalty Correlator): Continuous evaluation of aircraft lift-to-drag (L/D) ratios against pristine delivery baselines, quantifying drag penalties from bug strikes, rivet gaps, and leading edge erosion.
  • In-Flight Trajectory & Cruise Optimization (Dynamic 4D Trajectory Solver / Satellite CPDLC Uplink / EFB App Interconnect): Broadcasting optimized step-climb altitudes and Cost Index (CI) speed recommendations directly to cockpit electronic flight bags (EFB) in flight.

Flight Telemetry Metrics: 3.8% (Average Fleet Fuel Savings) | ± 0.5°C (Exhaust Gas Temp (EGT) Accuracy) | 100% (FADEC Data Lossless Transmission) | 30 Days (Advance Engine Fault Warning Time)

비트 단위, 비행 단위로 현대 항공기 최적화하기

Every individual aircraft in a fleet flies through varying atmospheric humidity, volcanic aerosols, and thermal cycles, causing unique engine and aerodynamic degradation. AirplaneTwins creates a bespoke digital twin for each tail number, calculating optimal cruise altitudes and engine wash intervals based on real-time physics.

Core Engineering Areas

Technical Publications

Related Cluster Architecture Specifications