Title:
航空機用後部エンジン
Document Type and Number:
Japanese Patent JP6387062
Kind Code:
B2
Abstract:
A propulsion system (100) for an aircraft (10) is provided having an aft engine configured to be mounted to the aircraft (10) at an aft end of the aircraft (10). The aft engine includes a fan (304) rotatable about a central axis of the aft engine having a plurality of fan blades (310) attached to a fan shaft (312). The aft engine also includes a nacelle (306) encircling the plurality of fan blades (310) and a structural support system (308) for mounting the aft engine to the aircraft (10). The structural support system (308) extends from the fuselage (12) of the aircraft (10), through the fan shaft (312), and to the nacelle (306) when the aft engine is mounted to the aircraft (10). The aft engine may increase a net thrust of the aircraft (10) when mounted to the aircraft (10).
Inventors:
Thomas Lee Becker
Kurt David Mallow
Patrick Michael Marinan
Brandon Wayne Miller
Kurt David Mallow
Patrick Michael Marinan
Brandon Wayne Miller
Application Number:
JP2016192434A
Publication Date:
September 05, 2018
Filing Date:
September 30, 2016
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
B64C1/16; B64C11/44; B64C21/06; B64D27/14; B64D27/20; B64D27/24
Domestic Patent References:
| JP2010516546A |
Foreign References:
| US20150000252 | ||||
| GB1211081A |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka