An Approach for Utilizing Power Flow Modeling for Simulations of Hybrid Electric Propulsion Systems

Chapman, Jeffryes W ; Litt, Jonathan S

关键词: AIRCRAFT POWER SUPPLIES;    HYBRID PROPULSION;    ELECTRIC PROPULSION;    TURBOGENERATORS;    POWERED MODELS;    LOAD TESTS;    SIMULATION;    FLY BY WIRE CONTROL;    PROPULSION SYSTEM PERFORMANCE;    STEADY STATE;    ELECTRIC CURRENT;   

RP-ID  :  GRC-E-DAA-TN56356

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

This paper describes an approach to creating simulations of the electric components for a hybrid electric propulsion system. The proposed modeling technique is based on power/load flow modeling and is designed to provide a modular framework that includes buses, lines, and other electrical components that can be connected together to form the electrical distribution system. The purpose of this paper is to detail an electric distribution system modeling technique and to demonstrate how these models may be integrated with turbomachinery simulations. These general modeling techniques were created to be utilized for system and control design studies. Additionally, steady-state and dynamic performance for a proposed model example is compared with data from a hardware in the loop simulation.