Geared counterrotating turbine/fan propulsion system

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 39162, 60268, 416129, F02K 372

Patent

active

050107291

ABSTRACT:
High by-pass fan jet engine includes counterrotating turbine blade sets for receiving hot combustion gases from a core engine portion and driving the fan blades through a planetary gear-type reduction gear assembly. Lightweight, highspeed, concentric, counterrotating shafts transmit power from both turbine blade sets to the fan via the reduction gear assembly. A pair of planetary gear assemblies with fixed fing gears and a rotatable common planetary gear carrier is used to drive a single set of fan blades via the carrier, and a pair of planetary gear assemblies with a fixed common planetary gear carrier and rotatable ring gears is used to drive two or more counterrotating fan blade sets via the ring gears. A low pressure "booster" compressor feeding the core engine portion can be directly driven from one of the two high speed shafts.

REFERENCES:
patent: 3673802 (1972-07-01), Krebs et al.
patent: 3729957 (1973-05-01), Petrie et al.
patent: 4005575 (1977-02-01), Scott et al.
patent: 4159624 (1979-07-01), Gruner
patent: 4251987 (1981-02-01), Adamson
patent: 4540369 (1985-09-01), Caires
patent: 4751816 (1988-06-01), Perry

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