FLADE gas turbine engine with counter-rotatable fans

Power plants – Reaction motor – Including counter rotating rotors

Reexamination Certificate

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Details

C060S039162, C060S226300

Reexamination Certificate

active

10647881

ABSTRACT:
An exemplary embodiment of a FLADE counter-rotating fan aircraft gas turbine engine includes at least one row of FLADE fan blades disposed radially outwardly of and drivingly connected to one of axially spaced-apart first and second counter-rotatable fans. A core engine located downstream and axially aft of the first and second counter-rotatable fans is circumscribed by a fan bypass duct downstream and axially aft of the first and second counter-rotatable fans. The row of FLADE fan blades radially extend across a FLADE duct circumscribed about the first and second counter-rotatable fans and the fan bypass duct. A second low pressure turbine is drivingly connected to the first counter-rotatable fan and a first low pressure turbine is drivingly connected to the second counter-rotatable fan.

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patent: 0 646 721 (1998-12-01), None

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