Reluctance generator/motor cooling
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorEdward B. Durkin
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AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorEdward B. Durkin
Estimating the term…
A reluctance motor/generator apparatus capable of operation at high rates of revolu-tion and high energy densities with reduced cooling-related windage losses and without incurring thermal damage to motor/generator elements. The apparatus includes an electrical winding-free reluctance rotor having a plurality of windage controlling and heat dissipating divider or barrier elements (which are also referred-to as thermal elements in the descriptions) disposed at opposite ends and periodically along its axial length to definite a plurality of rotor cooling chamber areas. The divider or barrier elements are provided with cooling fluid limiting apertures selected in size to optimize a relationship between rotor cooling effectiveness and windage energy losses. The machine stator is provided with cooling fluid release apertures of predetermined position and size relationship with the rotor cooling chamber areas. Use of the disclosed apparatus in the aircraft dynamoelectric machine environment is also disclosed.
A reduced coolant windage loss salient pole high speed reluctance dynamoelectric machine comprising the combination of:
The method of optimizing a tradeoff between viscous cooling fluid losses and desired cooling effect in a high speed dynamoelectric machine of the salient pole reluctance type, said method comprising the steps of:
Reluctance motor/generator apparatus comprising the combination of:
Dependencies are inferred from the claim text.