高阻抗和低阻抗故障保护要求及验证测试用于电动飞机电源系统

High-Impedance and Low-Impedance Fault Protection Requirements and Verification Testing for Electric Aircraft Power Systems

打开原文

AI 导读

本文探讨了eVTOL飞机中高阻抗和低阻抗故障的验证测试方法，对HVDC电源系统的标准制定具有参考价值。研究开发了两种新型故障注入测试系统，有助于提升电源系统的安全性和可靠性。依据来源摘要

正文 · 原文

Document ID

20250003314

Acquisition Source

Glenn Research Center

Document Type

Conference Paper

Authors

Trey D Rupp

(Glenn Research Center Cleveland, United States)

Brian P Malone

(Glenn Research Center Cleveland, United States)

David J Sadey

(Glenn Research Center Cleveland, United States)

Nicolas A Carbone

(Glenn Research Center Cleveland, United States)

Arthur G Birchenough

(HX5 (United States) Cleveland, United States)

Mark D Schmiedlin

(HX5 (United States) Cleveland, United States)

Date Acquired

April 3, 2025

Subject Category

Meeting Information

Meeting: IEEE Transportation Electrification Conference & Expo + Electric Aircraft Technologies Symposium (ITEC + EATS)

Location: Anaheim, CA

Country: US

Start Date: June 18, 2025

End Date: June 20, 2025

Sponsors: Institute of Electrical and Electronics Engineers (IEEE)

Funding Number(s)

Distribution Limits

Public

Public Use Permitted.

Technical Review

Single Expert

Keywords