An aircraft equipped with a distributed unducted fan propulsion system is provided. In one aspect, an aircraft includes a body defining a lateral centerline that separates the body into a first side and a second side. One or more first unducted fans are mounted to the first side of the body. The one or more first unducted fans are rotatable in a first direction. One or more second unducted fans are mounted to the second side of the body. The one or more second unducted fans are rotatable in a second direction that is opposite the first direction.
AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM
03.03.2022
Patent
Elektronische Ressource
Englisch
AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM
Europäisches Patentamt | 2022
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