An aircraft (100) equipped with a distributed unducted fan propulsion system (150) is provided. In one aspect, an aircraft (100) includes a body (102) defining a lateral centerline that separates the body (102) into a first side (114) and a second side (116). One or more first unducted fans (162A) are mounted to the first side (114) of the body (102). The one or more first unducted fans (162A) are rotatable in a first direction. One or more second unducted fans (172A) are mounted to the second side (116) of the body (102). The one or more second unducted fans (172A) are rotatable in a second direction that is opposite the first direction.
AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM
FLUGZEUG MIT VERTEILTER GEGENLÄUFIGER DIFFUSER GEBLÄSEANTRIEBSANLAGE
AÉRONEF ÉQUIPÉ D'UN SYSTÈME DE PROPULSION À SOUFFLANTE NON CARÉNÉE À CONTRE-ROTATION RÉPARTI
2022-03-02
Patent
Elektronische Ressource
Englisch
AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM
Europäisches Patentamt | 2022
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