Modelon Ab · OMXSTO:MODEL

Modelon Ab — Technical Presentation (July 2021)

35 slides from Modelon Ab's technical presentation, July 2021

  1. Slide 1: Fuel System Library Overview

    FUEL SYSTEM LIBRARY Overview

  2. Slide 2: Agenda

    AGENDA ❑ About Fuel System Library ❑ Key Benefits ❑ Key Capabilities ❑ Key Applications ❑ Library Contents ❑ Modelon Compatibility ❑ Latest Release: 2021.2 ©2021 Modelon 2

  3. Slide 3: About Fuel System Library

    ABOUT FUEL SYSTEM LIBRARY • Design and verification of fuel systems of civil and military aircrafts • Analysis and verification of system behavior during various dynamic operating modes and flight conditions, including effects of large variations in acceleration, direction and altitude • Provides si

  4. Slide 4: About Fuel System Library

    ABOUT FUEL SYSTEM LIBRARY Offline simulation of complete Fuel Systems through complete flight envelope and all operating conditions: • Large systems • Controls, sequential and feedback Real-time simulation of the same system models: • Some simplifications, but the same overall model (real time capab

  5. Slide 5: Key Benefits

    KEY BENEFITS ©2021 Modelon 5

  6. Slide 6: Key Benefits

    KEY BENEFITS • High performance and real-time capable • Import of 3D tank geometries from CAD • Physics-based models covering thermal, hydraulics, inerting, evaporation, solubility • Full support for bidirectional flow • Efficient property models of air-fuel mixtures • Easily switch off the thermal

  7. Slide 7: Key Capabilities

    KEY CAPABILITIES ©2021 Modelon 7

  8. Slide 8: Key Capabilities: Medium properties

    KEY CAPABILITIES Medium properties • Jet fuel • Jet-A, Jet-B, JP-4, JP-5, and JP-8 • Liquid medium with slight compressibility • Gas Mixture • Moist air (water with dry air or ideal dry air mixture) • No water condensation (𝜙 < 100%) • Evaporated jet fuel with dry air mixture • Mixture medium • All

  9. Slide 9: Key Capabilities: Multiple Connector types

    KEY CAPABILITIES Multiple Connector types Hollow connector Filled connector • pressure is a time • mass flow rate is continuous state computed from Dp • used in interface of p as state p not as state • used in flowmodel dynamic volumes set position set position interfaces • static eq: m_flow = f(Dp)

  10. Slide 10: Key Capabilities: Position information

    KEY CAPABILITIES Position information Pipes • Receive position information and cross sectional area from connected components • Receive acceleration vector via inner/outer • Optional dynamic momentum balance: pressure drop, static head and resistance losses can be computed from massflow as state All

  11. Slide 11: Key Capabilities: Position information

    KEY CAPABILITIES Position information flow area flow area + 3D-position + 3D-position fuel system valve=general fluid system valve + dynamic volumes (optional) + pipe length + positioning information + projection of acceleration vector on pipe length similar procedure for + fuel system connectors -

  12. Slide 12: Key Capabilities: Fuel tank inerting

    KEY CAPABILITIES Fuel tank inerting Purpose: • Fill air space in tanks with inert gas (N2) to reduce concentrations of oxygen and fuel to prevent combustion Medium properties use dry air mixture with variable composition of O2 and N2 ©2021 Modelon 12

  13. Slide 13: Key Capabilities: Fuel evaporation

    KEY CAPABILITIES Fuel evaporation Purpose: • Track amount of evaporated fuel in ullage Medium properties package for fuel evaporation • Evaporated jet fuel, O2, N2 and liquid jet fuel • Jet-A, JP-4, JP-5, and JP-8 Amount of evaporated fuel is based vapor pressure Jet fuel pseudo compound modeled in

  14. Slide 14: Key Capabilities: Gas solubility

    KEY CAPABILITIES Gas solubility • Tracking trace concentrations of oxygen and nitrogen dissolved in the liquid jet fuel • Assume dissolved gas does not alter thermodynamic properties of fuel or gas • Assume first order rate equation for dissolution and outgassing • Use data from the Aviation Fuel Ha

  15. Slide 15: Key Capabilities: Aggregation of Fuel mass

    KEY CAPABILITIES Aggregation of Fuel mass Automatically tracks total mass of fuel in large systems ©2021 Modelon 15

  16. Slide 16: Key Applications

    KEY APPLICATIONS ©2021 Modelon 16

  17. Slide 17: Key Applications: Real-time

    KEY APPLICATIONS Real-time Scope: • Develop complex and accurate models that can be run in real time • Use the same high-fidelity models throughout the design and validation process Relevant solution features: • Fuel Systems Library real-time mode • Inline integration • Mixed-mode integration ©2021

  18. Slide 18: Key Applications: Inerting

    KEY APPLICATIONS Inerting Scope: • Analyze the dynamic propagation of species like nitrogen and oxygen • Size the inerting system to ensure admissible oxygen concentrations throughout the envelope Relevant solution features: • Dynamic balance equations including full support of flow reversal • Set v

  19. Slide 19: Key Applications: Fuel transfer/refueling

    KEY APPLICATIONS Fuel transfer/refueling Scope: • Dynamically simulate fuel transfer and refueling of aircraft • Validate line, orifice, pump/ejector and balance tube performance • Simulate failure conditions including ejector induced and discharge flow reversal and pump cavitation Relevant solution

  20. Slide 20: Key Applications: Flammability

    KEY APPLICATIONS Flammability Scope: • Dynamically simulate mass and energy balance • Assess temperatures in relation to flash point/lower and upper flammability limits • Model heat transfer, mass transfer, solubility Relevant solution features: • Heat transfer to gas and liquid • Convective transpo

  21. Slide 21: Example: Filling Tank

    EXAMPLE: FILLING TANK Quasi-steady-state components: • Settings_FSL (1), AirData(1), Atmosphere(1) • Pipe (8) • Valve (1) • Sinks/sources (2) Mass and energy storage: • Tank (4) • Dynamic volumes (incl. e.g. moisture condensation) (2) ©2021 Modelon 21

  22. Slide 22: Library Contents

    LIBRARY CONTENTS ©2021 Modelon 22

  23. Slide 23: Components

    COMPONENTS Systems of Aircraft fluid • System settings like altitude, Mach number, etc Boundary conditions • Pressure source/sink • Mass flow source/sink • Options: set parameters, signal inputs, use atmosphere information from system component Pipe • Static head uses connection vector between ports

  24. Slide 24: Components: Tank

    COMPONENTS Tank y • Volume with one pressure and temperature state air + water vapor P1 • Distance of liquid level to port determines + fuel vapor port pressure – iteration variable or additional numerical state • Ports can be left unconnected a L1 ▪ input: P1, P2, a, V_liq L2 ▪ output: L1, L2 P2 V_

  25. Slide 25: Components: Tank with Heat Transfer

    COMPONENTS Tank with Heat Transfer • Volume with one pressure and temperature state • Heat port for each side of the box shaped tank • Calculate wetted surface area for each side • User-defined wet/dry heat transfer coefficient for each side ©2021 Modelon 25

  26. Slide 26: Components: Complex Tank

    COMPONENTS Complex Tank • Geometry defined by sets of vertices and triangles • Supports import of CAD geometries via STL files • Arbitrary number of heat transfer surfaces • Physical free convection heat transfer correlations distinguishing wet vs. dry surface, surface inclination etc. ©2021 Modelon

  27. Slide 27: Components: Multi-Level Tank

    COMPONENTS Multi-Level Tank • Simulate the behavior of a tank where basins are not communicating in certain configurations and thus can have different liquid levels in the same tank system • Tanks are modeled orifice models connected in-between • Geometry defined by sets of vertices and triangles •

  28. Slide 28: Components: Sensors, Volume, Valves

    COMPONENTS Ideal Sensors • Single port sensors: p, T • Two port flow sensors: m_flow, V_flow Volume • Dynamic energy and mass balances • Volume without hydraulic resistance Valves • Check valve • Control valve (Kv-value parameterization) ©2021 Modelon 28

  29. Slide 29: Components: Pump and Ejector

    COMPONENTS Pump • Hydraulic characteristics • Power characteristics • Cavitation influence by a reduction factor by parameterization Ejector • The motive flow is always positive, induced and discharge flow can change flow direction • Choked flow is not reached in the nozzle • Incompressible • Fricti

  30. Slide 30: Modelon Compatibility

    MODELON COMPATIBILITY ©2021 Modelon 30

  31. Slide 31: Recommended Modelon Library Compatibility

    RECOMMENDED MODELON LIBRARY COMPATIBILITY • Environmental Control Library • Moist air • Turbines • Fans • Compressors • Ejector • Aircraft Dynamics Library • Jet Propulsion Library • Liquid Cooling Library • Heat Exchanger Library • Hydraulics Library ©2021 Modelon 31

  32. Slide 32: Example: Modelon Portfolio Multi-Domain System

    EXAMPLE: MODELON PORTFOLIO MULTI-DOMAIN SYSTEM • Electric Power Library • Environmental Control Library • Fuel System Library • Heat Exchanger Library • Hydraulics Library • Liquid Cooling Library • Vapor Cycle Library ©2021 Modelon 32

  33. Slide 33: Latest Release: 2021.2

    LATEST RELEASE: 2021.2 ©2021 Modelon 33

  34. Slide 34: Release 2021.2 New Feature

    RELEASE: 2021.2 New Feature • A new complex geometry tank model supporting multi-level simulations is added. The flow through the tanks are modeled by an orifice approximating a rectangular weir as opening. • Devices to extract only liquid or gas from the multi- level tank are added. • Add ControlVa

  35. Slide 35: Release 2021.2 Enhancements

    RELEASE: 2021.2 Enhancements • Added a Boolean parameter visualize to the tank geometry kernels (ModelicaWithVisualization and ExplicitExternalWithVisualization) which supports 3D visualization. By default, it is set to true. Setting this to false will reduce result file size and simulation time con

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