This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
High-Reactance Permanent Magnet Machine for High-Performance Power Generation Systems
Technical Paper
2006-01-3076
ISSN: 0148-7191, e-ISSN: 2688-3627
Annotation ability available
Sector:
Event:
Power Systems Conference
Language:
English
Abstract
Honeywell is currently working on several projects utilizing high-reactance permanent magnet machines (HRPMM) to develop advanced, high-performance power generation systems (HPPGS).
These power generation systems (PGS), offer greatly increased safety and reduced operating costs compared to previous hardware. The approach utilizes an HRPMM that presents reduced short-circuit currents with simplified power topology and specifically developed control algorithms. These architectures offer inherent fail-safe features in that the maximum possible short-circuit current is not significantly higher than the normal operating current. Control approaches are discussed. Methodologies for system optimization to achieve top performance and robust operation are included.
These power generators support implementation of on-shaft integration with the plant. A gearless/oilless system can be obtained, resulting in elimination of the gearbox, lubrication system, and in some applications even the cooling systems. The benefits are reduced weight and volume with substantial improvement of reliability and maintainability.
Specific implementations applicable to military aircraft and spacecraft are included. These designs are compliant with the respective specifications for power quality and EMI.
Recommended Content
Technical Paper | Improving Peak Power Capability of an Aircraft |
Technical Paper | Advanced Electric Generators for Aerospace More Electric Architectures |
Technical Paper | Computer Utilization for Aircraft Contour Determination |
Topic
Citation
Ganev, E., "High-Reactance Permanent Magnet Machine for High-Performance Power Generation Systems," SAE Technical Paper 2006-01-3076, 2006, https://doi.org/10.4271/2006-01-3076.Also In
References
- Ensworth Primary and Source Auxiliary Power Selection for Reusable Launch Vehicles
- Reaves Freudenberger Reusable Launch Vehicle (RLV) Power Generation Systems Trail from 1 st to 2 nd Generation
- Honeywell NGLT Turbine Power Unit Final Design Review 11 18-19 2003
- Koerner Ganev Freudenberger A Turbine-Driven Electric Power Generation System for Launch Vehicles and other High-Power Space Applications SAE 2004-01-3185 Power Systems Conference November 2-4 2004 Reno, Nevada, USA
- An Electric Power Generation System For Launch Vehicles Koerner Mike Ganev Evgeni Honeywell International, Engines Systems & Services Torrance, CA SAE 2004, Power Systems Conference New Orleans, Louisiana, USA November 7-9 2006