Pusher propeller installation for turboprop engines

Aeronautics and astronautics – Aircraft power plants

Patent

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Details

244 65, 244 57, 602261, B64D 2900

Patent

active

049307258

ABSTRACT:
A pusher turboprop engine is provided with an interior exhaust duct structure which directs the hot turbine gases through and out of the engine nacelle and around the rear spinner which surrounds the propeller hub. The spinner supports blade-shaped shields which protect the roots of the propeller blades from the hot exhaust gasses.

REFERENCES:
patent: 2456151 (1948-12-01), Sawyer
patent: 2526941 (1950-10-01), Fishbein
patent: 2604276 (1952-07-01), Huben
patent: 2627927 (1953-02-01), Mergen
patent: 2726725 (1955-12-01), Nichols
patent: 3811791 (1974-05-01), Cotton
patent: 4171183 (1979-10-01), Cornell et al.
patent: 4488399 (1984-12-01), Robey et al.

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