A gas turbine engine includes a thrust reverser including a plurality of blocker doors moveable between a deployed position and a stowed position. A gap is defined between adjacent blocker doors when in the stowed position. A plurality of divots are mounted forward of the plurality of blocker doors to substantially cover the gap between the adjacent blocker doors when in the stowed position.
DIVOT FOR BLOCKER DOORS OF THRUST REVERSER SYSTEM
30.07.2015
Patent
Elektronische Ressource
Englisch
Innovative Concept for Cascade Thrust Reverser Without Blocker Doors
British Library Conference Proceedings | 1997
|Translating cascade hidden blocker door thrust reverser
Europäisches Patentamt | 2020
|TRANSLATING CASCADE HIDDEN BLOCKER DOOR THRUST REVERSER
Europäisches Patentamt | 2017
|