Title:
航空機用のハイブリッド電気推進システム
Document Type and Number:
Japanese Patent JP6664437
Kind Code:
B2
Abstract:
A propulsion system 100 for an aircraft 10 includes a propulsor 204; a turbomachine 202 mechanically coupled to the propulsor 204 for driving the propulsor 204 during a combustion operating mode of the propulsion system 100 and mechanically decoupled from the propulsor 204 during an electric operating mode of the propulsion system 100; and an electrical power source 246. The propulsion system 100 further includes an electric machine, the electric machine being electrically coupled to the electrical power source 246 and mechanically coupled to the propulsor 204 during the electric operating mode of the propulsion system 100 such that the electric machine drives the propulsor 204 during the electric operating mode of the propulsion system 100.
Inventors:
Mustafa Dinder
Keith Ejay Brodget
Keith Ejay Brodget
Application Number:
JP2018116550A
Publication Date:
March 13, 2020
Filing Date:
June 20, 2018
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
B64D27/24; B64D27/12; B64D33/02; B64D33/04; F02C6/00; F02C6/20
Domestic Patent References:
| JP2016135671A | ||||
| JP2013194636A |
Foreign References:
| US20090293494 | ||||
| EP2962885A1 | ||||
| US20170081035 | ||||
| US20130038057 | ||||
| EP2924247A1 | ||||
| DE102013209538A1 | ||||
| DE102010049885A1 |
Attorney, Agent or Firm:
Masato Iida
Choi
Kenji Tanaka
Arakawa Satoshi
Hirokazu Ogura
Takuto Tanaka
Choi
Kenji Tanaka
Arakawa Satoshi
Hirokazu Ogura
Takuto Tanaka