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George Thomas and Jonathan Fuzaro Alencar
NASA Glenn Research Center
Power Management and Distribution Branch
March 2020
Electrified aircraft propulsion (EAP) is a prospective advanced propulsion concept to reduce aircraft noise, NOx emissions and aircraft fuel burn. In its most primitive definition, EAP refers to concepts that utilize electrical power in propulsion of the aircraft. This includes hybrid electric, such as the Boeing-General Electric (GE) “Sugar Volt” and turboelectric concepts, such as STARC-ABL, featuring two main engines and an electrically powered aft thruster for boundary layer ingestion. Both hybrid electric and turboelectric concepts utilize an electrical power system to deliver power from an electrical source, e.g. battery or generator, to a motor which drives a propulsor (or aids a turbine) that provides thrust for the vehicle. The electrical power system impacts the overall weight, thermal system requirements, and efficiency of the propulsion system and these tradeoffs need to be considered to meet the design objectives, especially in an optimized fashion. More specifically, this requires the power system to be included in the conceptual design phase of the propulsion system. One of the most widely used tools for conceptual design of propulsion systems is the Numerical Propulsion System Simulation (NPSS). This repository, the NPSS Power System Library (PSL), is designed to enable NPSS to address these needs for modeling EAP systems.
This library contains a set of power system and circuit components, as well as an interpreted electric port, designed to connect power system components together. The electric port . The components are designed to work in a manner similar to baseline NPSS components like compressors, turbines, ducts, and others. Electric machine components, being the motors and generators,
--describe what we do with the solver, especially voltage independents in the node element and other elements (which have internal nodes), also describe the on-design current independents
--describe the prePass shit we do, and the need for cable/breaker blocks to execute before the other blocks (with internal nodes)
--describe things people need to know about how to use power blocks in assemblies, depends on
--describe linkPortsI
--describe the electric power types, and how they affect the solver setup. Describe the power propagation logic once it is completed
To continue reading, see Items Within Library.
This wiki page is intended to serve as documentation for the NPSS Power System Library (PSL). The PSL is maintained by NASA at the NASA Glenn Research Center, and funded by the Revolutionary Vertical Lift Technology (RVLT) project. A detailed table of contents for this page can be found in the Home page.
- Home
- Library Structure
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Fundamental Classes and Components
- Electric Port
- Electric Node (Bus)
- Complex Number
- Inverter & Rectifier Map
- Motor & Generator Map
- E-Thermal Mass
- Interpreted Port
- Electric Element
- Electric Assembly
- Interpreted Assembly
- Modeling Components
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Examples
- baseline
- baseline 1to2Bus
- baseline 2to1Bus
- baseline all_elec
- baseline all_elecMDP
- baseline turboelectric
- baseline turboelectricMDP
- cable_and_duct thermal_test
- cable_test
- cable thermal_test
- power propagation
- run_3phase example
- run_RLC example
- run_R_dc example
- thermal baseline
- thermal test
- transient baseline