面向民用航空运输业的连续气动力学与航空推进发动机数字孪生平台

AirplaneTwins 精准解算高压压气机叶片结垢结焦与机翼蒙皮阻力增量，科学决策发动机水洗与维护周期，每年为航司节省巨量航油消耗。

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)

逐比特、逐航班优化现代飞机

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