Electric drive of transport-sized aircraft propulsors, with electric power generated by fuel cells or turbo-generators, will require electric motors with much higher power density than conventional room-temperature machines. Cryogenic cooling of the motor windings by the liquid hydrogen fuel offers a possible solution, enabling motors with higher power density than turbine engines. Some context on weights of various systems, which is required to assess the problem, is presented. This context includes a survey of turbine engine weights over a considerable size range, a correlation of gear box weights and some examples of conventional and advanced electric motor weights. The NASA Glenn Research Center program for high power density motors is outlined and some technical results to date are presented. These results include current densities of 5,000 A per square centimeter current density achieved in cryogenic coils, finite element predictions compared to measurements of torque production in a switched reluctance motor, and initial tests of a cryogenic switched reluctance motor.
Product Identifiers
Publisher
Bibliogov
ISBN-13
9781289239213
eBay Product ID (ePID)
9046362764
Product Key Features
Publication Name
NASA Glenn Research Center Program in HIGH POWER Density Motors for Aeropropulsion
Format
Paperback
Language
English
Subject
Government
Publication Year
2013
Type
Textbook
Dimensions
Item Height
246mm
Item Width
189mm
Item Weight
77g
Additional Product Features
Country/Region of Manufacture
United States
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