Aircraft of split turbo-prop configuration
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United States of America Patent
Stats
-
Mar 12, 1991
Grant Date -
N/A
app pub date -
May 4, 1989
filing date -
May 5, 1988
priority date (Note) -
Expired
status (Latency Note)
Importance
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.
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