FIELD: electricity.
SUBSTANCE: method is realised by variation of terminal electric machine stator and rotors design variation, and also by using non-magnet and dielectric materials in bearing structures of the machine, which make it possible to reduce losses from occurrence of vortex currents. Application of up-to-date non-magnet and dielectric materials with sufficient heat resistance and strength exceeding strength of metals, and also with lower volume weight in manufacturing of electric machines will make it possible to wider use terminal electric machines of the proposed design in aircraft building.
EFFECT: improved manufacturability of terminal machines production, higher stiffness of their main parts and increased power indices of a terminal electric machine.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
LINEAR MOTOR | 2011 |
|
RU2517437C2 |
ELECTRICAL MACHINE | 2010 |
|
RU2440659C1 |
STATOR OF ELECTRIC MACHINE | 0 |
|
SU1073844A1 |
ELECTRIC DRIVE OF CARRIERS | 2012 |
|
RU2509665C1 |
ELECTRIC MACHINE | 2008 |
|
RU2360352C1 |
ASYNCHRONOUS ELECTRICAL MACHINE | 2014 |
|
RU2556075C1 |
SYNCHRONOUS ELECTRICAL MACHINE | 2013 |
|
RU2556076C2 |
TERMINAL ELECTRIC MACHINE (VERSIONS) | 2013 |
|
RU2541427C1 |
ELECTRICAL MACHINE | 2008 |
|
RU2396671C1 |
END MOTOR WITH GENERATOR FUNCTION CONTAINING PERMANENT MAGNETS | 2022 |
|
RU2802342C1 |
Authors
Dates
2012-04-20—Published
2011-02-24—Filed