Fan blade protection system

Fluid reaction surfaces (i.e. – impellers) – Plural impellers having relative movement or independent... – Coaxial rotation

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Details

416238, 416170R, B63H 510

Patent

active

052248313

ABSTRACT:
In one type of aircraft propulsion system, propeller blades are mounted on a ring which surrounds a turbine. An annular space exists between the turbine and the ring. If a propeller blade should break free, the unbalanced centrifugal load tends to deform the ring. The invention reduces the deformation, as by locating spacers between the turbine and the ring.

REFERENCES:
patent: 2186064 (1940-01-01), Dekker
patent: 3727998 (1973-04-01), Haworth et al.
patent: 4767271 (1988-08-01), Catlow
patent: 4826403 (1989-05-01), Catlow
patent: 4915586 (1990-04-01), Williams

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