An aircraft includes a propulsion supported within an aft portion of a fuselage A thrust reverser is mounted in the aft portion of the fuselage proximate the propulsion system for directing thrust in a direction to slow the aircraft. The thrust reverser includes an upper blocker door movable about a first pivot axis to a deployed position and a lower blocker door movable about a second pivot axis not parallel to the first pivot axis.
ASYMMETRIC THRUST REVERSERS
2015-10-15
Patent
Elektronische Ressource
Englisch
NTRS | 2018
|NTRS | 2017
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