Title:
航空機用の推進システム
Document Type and Number:
Japanese Patent JP6435358
Kind Code:
B2
Abstract:
A propulsion system for an aircraft 10 includes an electric generator 56 and a turbomachine 102. The turbomachine is configured to be mounted to a first wing 20 of the aircraft and is operable with the electric generator 56. The propulsion system additionally includes a first propulsor 104 mechanically coupled to a shaft of the turbomachine and a second propulsor assembly 54 configured to be mounted at a location away from the turbomachine 102 and the first propulsor 104. The electric generator 56 is in electrical communication with the second propulsor assembly for powering the second propulsor assembly.
Inventors:
Randy M Vondraer
Matthew Ryan Polakowski
Kurt David Mallow
Glen Crabtree
Matthew Ryan Polakowski
Kurt David Mallow
Glen Crabtree
Application Number:
JP2017029594A
Publication Date:
December 05, 2018
Filing Date:
February 21, 2017
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
B64D27/12; B64D41/00; F02C6/00; F02C7/00; F02C7/32; F02C7/36; F02K3/04
Domestic Patent References:
| JP2006205755A | ||||
| JP2001334998A | ||||
| JP2009528468A |
Foreign References:
| EP2878538A1 | ||||
| US20080184906 | ||||
| US20040211862 | ||||
| US20140010652 | ||||
| WO2013079972A1 | ||||
| FR2915732A1 | ||||
| DE1109533B |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka