Aircraft of split turbo-prop configuration

Details Aircraft of split turbo-prop configuration Aircraft of split turbo-prop configuration

1989-05-04

1991-03-12

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft power plants

Arrangement

244 53R, 244 54, B64D 2700

Patent

active

049989952

ABSTRACT:
A turbo-prop driven aircraft has the engines (6) and propeller assemblies (10) spatially separated fore and aft of the wing box (4) and interconnected by a drive shaft (27). This arrangement permits the engine to be located away from the wing box without causing excessive overhang of the turbo-prop installation.

REFERENCES:
patent: 2153603 (1939-04-01), Wells
patent: 2162956 (1939-06-01), Lysholm
patent: 2388806 (1945-11-01), Stalker
patent: 2426635 (1947-09-01), Mercier
patent: 2526941 (1950-10-01), Fishbein

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