Reverse pitch fan with divided splitter

Power plants – Reaction motor – Interrelated reaction motors

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Details

60228, F02K 306

Patent

active

040055744

ABSTRACT:
A gas turbofan engine including a variable pitch fan is provided with flow straightening means which are adapted to reduce fan exit swirl in the forward thrust mode. The flow straightening means are so arranged to produce low losses in the fluid entering a core engine during reverse thrust operation while allowing large supercharging of the core engine during forward thrust operation.

REFERENCES:
patent: 3489338 (1970-01-01), Chilman
patent: 3494129 (1970-02-01), Krebs et al.
patent: 3528241 (1970-09-01), Venable et al.
patent: 3720060 (1973-03-01), Davies et al.
patent: 3747343 (1973-07-01), Rosen

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