Title:
スラストリバーサを備えたガスタービンエンジン及び動作の方法
Document Type and Number:
Japanese Patent JP6903369
Kind Code:
B2
Abstract:
A gas turbine engine 10 and thrust reverse assembly 44 having a set of outer doors 48 movable between a stowed position and an deployed position, where the set of outer doors 48 extends outwards from the nacelle 12 and a set of blocker doors 50 movable between a stowed position and an deployed position, where the set of blocker door extends into an air flow conduit 31 defined by the bypass duct 30 to deflect air outwards.
More Like This:
| WO/2014/207410 | DUAL-GRID REVERSER WITHOUT RODS IN THE DUCT |
| WO/2012/045970 | THRUST REVERSER |
| WO/2021/156477 | DEVICE FOR ATTACHING A CONNECTING ROD SMALL END FOR A THRUST REVERSAL CASCADE FLAP |
Inventors:
Graham Frank Howarth
Andrew Michael Roach
Timothy Robert Biesmann
Andrew Michael Roach
Timothy Robert Biesmann
Application Number:
JP2017092205A
Publication Date:
July 14, 2021
Filing Date:
May 08, 2017
Export Citation:
Assignee:
MRA Systems LLC
International Classes:
F02K1/72; B64D33/00; F02K3/06
Domestic Patent References:
| JP9250394A |
Foreign References:
| US4073440 |
Attorney, Agent or Firm:
Masato Iida
Choi
Kenji Tanaka
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Choi
Kenji Tanaka
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka