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US 2021/0316878 A1Published application
Electric generator
AssigneeGeneral Electric Company
InventorsHao Huang, David Dimitri Karipides, Jia Xiaochuan
Life of this patent
Estimating the term…
Abstract
An electric generator assembly for an aircraft is provided. The electric generator assembly includes: a main generator having a main rotor and a main stator, the main stator comprising a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees
Claims20
An electric generator assembly for an aircraft comprising:
- a main generator comprising a main rotor and a main stator, the main stator comprising a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees.
An aircraft electrical system comprising:
- a combustion engine;
- and
- an electric generator assembly comprising a main generator comprising a main rotor and a main stator, the main generator rotor driven directly or indirectly by the combustion engine, the main stator comprising a first three-phase winding and a second three-phase winding, the first and second three-phase windings each configured to have a voltage induced therein by the main rotor, the first three-phase winding defining a phase shift from the second three-phase winding greater than zero degrees.
Dependencies are inferred from the claim text.