Unconventional integrated propulsion systems and methods for...

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Reexamination Certificate

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C244S060000, C244S062000, C244S05300R

Reexamination Certificate

active

07665689

ABSTRACT:
Integrated propulsion systems and methods for blended wing aircraft are disclosed. In one embodiment, a propulsion system at least one engine operatively disposed within an engine flow duct having an engine inlet and an engine exhaust aperture, and at least one fan operatively disposed within a fan flow duct having a fan inlet and a fan exhaust aperture. The engine and fan rotational axes extending at least approximately along a lengthwise direction of the aircraft, the fan flow duct being separate from the engine flow duct. A transmission assembly is operatively coupled between the at least one engine and the at least one fan, the transmission assembly being configured to transmit a rotary output from the at least one engine to rotate the at least one fan.

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