Method of providing electric power with thermal protection
AssigneePratt & Whitney Canada Corp.
InventorKevin Allan Dooley
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AssigneePratt & Whitney Canada Corp.
InventorKevin Allan Dooley
Estimating the term…
An electric machine including a magnetic component, forming part of its rotor or stator that loses its magnetic characteristics above a certain chosen temperature is disclosed. This magnetic material forms part of a magnetic circuit that guides flux about the stator. As a result, any magnetic flux emanating with the rotor stops circulating about the stator above this temperature, and the machine stops acting as generator. The component is thermally coupled to windings carrying current from the machine's stator. The material forming the component is selected so that the chosen temperature is lower than the temperature at which the machine would be thermally damaged. This, in turn, limits the operating temperature of the windings, and thus prevents overheating of the machine during operation, typically caused by a fault. Preferably this magnetic material is formed from a ferrite material, such as a Manganese Zinc ferrite material.
A method of thermally protecting an electric generator to prevent overheating, said generator comprising a stator mounted about a rotor, and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising:
A method of providing a thermally limited source of electrical power within an aircraft, said method comprising:
A method of preventing overheating in an electric generator in the presence of an internal fault, said generator having a stator, a rotor and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising:
A method of preventing overheating in an electric generator, said generator having a stator, a rotor and at least one winding about said stator, said stator at least partially defining a magnetic circuit guiding magnetic flux emanating from said rotor, said method comprising:
A method of providing a thermally limited source of electrical power within an aircraft, said method comprising:
Dependencies are inferred from the claim text.