V/STOL Aircraft

Aeronautics and astronautics – Aircraft – steering propulsion

Patent

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Details

244 1R, 244 36, 244 52, B64C 1500

Patent

active

044362617

ABSTRACT:
Various forms of V/STOL aircraft are disclosed, each having a tiltable exterior structure that is in the shape of a pair of connected partial circular conoids. In one general form the conoids house the thrust producing engines, whereas in another form they are immediately downstream thereof. Also provided is a sonic boom concentrator in the form of a fin having curved sidewalls and truncated ends.

REFERENCES:
patent: 1917503 (1933-07-01), Crump
patent: 2922277 (1960-01-01), Bertin
patent: 2939648 (1960-06-01), Fleissner
patent: 3258916 (1966-07-01), Lehmann
patent: 3415216 (1968-12-01), Strobel
patent: 4366936 (1983-01-01), Ferguson

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