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20150005309 · Lightweight, Efficient Power Converters for Advanced Turboelectric Aircraft Propulsion Systems

NASA · 2014

Open the PDFPublic domain · NASATechnical Reports

Overview

NASA is investigating advanced turboelectric aircraft propulsion systems that use superconducting motors to drive multiple distributed turbofans. Conventional electric motors are too large and heavy to be practical for this application; therefore, superconducting motors are required. In order to…

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Key points

  • NASA is investigating advanced turboelectric aircraft propulsion systems that utilize superconducting motors.
  • Conventional electric motors are deemed too large and heavy for practical use in these systems, necessitating the use of superconducting motors.
  • Variable-speed power converters are essential for improving aircraft maneuverability by throttling power to the turbofans.
  • The project aims to develop cryogenic power conversion technology that is lightweight and efficient, minimizing additional heat load on refrigeration systems.
  • Phase II objectives include designing, fabricating, and testing a cryogenic multichip module and a cryogenic half-bridge inverter.
Frequently asked questions
What is the main focus of NASA's investigation in this document?

The main focus is on advanced turboelectric aircraft propulsion systems that use superconducting motors to drive multiple distributed turbofans.

Why are superconducting motors required for turboelectric aircraft propulsion systems?

Superconducting motors are required because conventional electric motors are too large and heavy to be practical for this application.

What are the Phase II objectives mentioned in the document?

The Phase II objectives include designing, fabricating, and testing a cryogenic multichip module and a cryogenic half-bridge inverter.

How does cryogenic power conversion technology benefit aircraft propulsion systems?

Cryogenic power conversion technology offers small size, low weight, and high efficiency, which are crucial for minimizing heat load on refrigeration systems.

What applications are mentioned for the developed technology?

Applications include turboelectric aircraft propulsion systems, high-power drives for superconducting motors, and utility projects for power transmission.

Document

Lightweight, Efficient Power

Converters for Advanced

Turboelectric Aircraft Propulsion

Systems

Extremely efficient cryogenic power conversion technology

NASA is investigating advanced turboelectric aircraft propulsion systems that use superconducting motors to drive multiple distributed turbofans.

Conventional electric motors are too large and heavy to be practical for this application; therefore, superconducting motors are required. In order to improve aircraft maneuverability, variable-speed power converters are required to throttle power to the turbofans. The low operating temperature and the need for lightweight components that place a minimum of additional heat load on the refrigeration system open the possibility of incorporating extremely efficient cryogenic power conversion technology. This Phase II project is developing critical components required to meet these goals.

Phase II Objectives ` Design, fabricate, and test a cryogenic multichip module, Applications which can be used in applications requiring very high power densities NASA Commercial/Other and efficiencies Government ` Turboelectric aircraft ` Design, fabricate, and test a propulsion systems ` Utility projects to develop super- cryogenic half-bridge inverter using ` High-power drives for conducting power transmission these modules, demonstrating superconducting motors ` Superconducting wind turbine the potential reduction in size and ` High-power and high-power- generators weight for a given power level as density cryogenic and wide ` Distribution systems for large well as ultrahigh efficiency temperature range power buildings (e.g., data centers, conversion systems: manufacturing plants): )LULÄ[ t Interplanetary and interstellar t MTECH Laboratories is spacecraft currently working toward a ` Offers small size, low weight, t Satellites demonstration site of such and high efficiency t Landers a distribution system t Surface base stations on ` U.S. Navy: moons or planets t Cryogenic motor drive system for the All-Electric Ship Firm Contact program MTECH Laboratories, LLC ` U. S. Department of Energy Michael J. Hennessy (DOE): mjhennessy@mtechlabs.com 831 Rte. 67, Bldg. 45C t Equipment for supercon- Ballston Spa, NY 12020–0227 ducting accelerators at DOE Phone: 518–885–6436 national accelerator labs Proposal Number: 09-2: A2.01-9471 N ASA/TM—2014-218497 10

Source & rights

Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

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Document details

Doc number
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20150005309
Publisher
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NASA
Year
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2014
Pages
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1
File size
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147 KB