航空機用の両面式スタータ/発電機

Japanese Patent JP5483812

B2

An electromagnetic machine for extracting power from a turbine engine (10) includes an outer rotor (76) and an inner rotor (72) rotatably supported adjacent to a stator (66). The stator (66) is disposed between the inner (72) and outer (76) rotors. The stator (66) has an inner set of windings (67) disposed on an inner surface adjacent to the inner rotor (72), and an outer set of windings (65) on an outer surface of the stator adjacent to the outer rotor (76). A plurality of permanent magnets (75) are disposed on an inner surface of the outer rotor (76) element and on an outer surface of the inner rotor element (72). Air gaps (62, 64) are defined between the outer surface of the stator (66) and the outer permanent magnets (75), and between the inner surface of the stator portion (66) and the inner permanent magnets (74). The inner stator windings (67) form a set of multiple-phase windings, and the outer stator windings (65) form a set of multiple-phase windings.

Longai Ku
Way woo
John M Khan
Juan M de Bedoud
Manoi Earl Shah
Ayman Mohammed Fauzi El-Lafayette

JP2007315325A

May 07, 2014

December 06, 2007

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GENERAL ELECTRIC COMPANY

H02K16/00; F02C7/275; F02C7/32; F02C7/36; H02K21/12

JP9175203A
JP2001136606A
JP2004232636A
JP2299452A
JP2001268866A
JP2003164125A
JP2003299391A
JP2001527740A
JP2005186733A

Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka

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