CPC B64C 7/02 (2013.01) [B64C 29/0025 (2013.01)] | 20 Claims |
1. A lift nacelle, comprising:
an airflow generator;
a sidewall system coupled to the airflow generator and spanning in a first direction, wherein the sidewall system at least partially defines a nacelle interior space,
wherein the airflow generator at least partially defines one of a forward boundary or an aft boundary of the nacelle interior space; and
a lift body comprising an internal rotor disposed in the nacelle interior space,
wherein the airflow generator is configured to accelerate airflow in the nacelle interior space to contact the lift body.
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