Title:
航空機用後部エンジン
Document Type and Number:
Japanese Patent JP6401759
Kind Code:
B2
Abstract:
A propulsion system 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). The aft engine also includes a nacelle (306) encircling the plurality of fan blades (310) with one or more structural members (308) extending between the nacelle (306) and the mean line (15) of the aircraft (10) at a location forward of the plurality of fan blades (310) 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).
More Like This:
Inventors:
Thomas Lee Becker
Kurt David Mallow
Patrick Michael Marinan
Brandon Wayne Miller
Kurt David Mallow
Patrick Michael Marinan
Brandon Wayne Miller
Application Number:
JP2016178125A
Publication Date:
October 10, 2018
Filing Date:
September 13, 2016
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
B64D27/02; B64C21/06; F02C3/073; F02C3/107; F02C7/00; F02C7/042; F02C7/057; F02C9/54; F02K1/04; F02K3/06
Domestic Patent References:
| JP11034990A | ||||
| JP2015503705A |
Foreign References:
| US4371133 | ||||
| WO2014072615A1 | ||||
| US20150183523 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka