Passively stable hovering system

Motor vehicles – Surface effect vehicles – Having propulsion or control means

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Details

244 23A, 244 23D, B60V 111, B60V 114

Patent

active

050709550

ABSTRACT:
A flight system capable of passively stable hover and horizontal translatory flight, comprises an apparatus defining a vertical axis, and including multiple ducts with substantially vertical axes in hover mode, spaced the axis; fluid momentum generators in the ducts to effect flow of fluid downwardly in the ducts in hover; and fluid flow deflector structure in the path of the flowing duct fluid, and angled to deflect the fluid flow away from the axis, in such manner as to provide stability in hover of the apparatus, as well as stability when the entire device is tilted through approximately 90.degree. to execute horizontal translatory flight.

REFERENCES:
patent: 2953320 (1960-09-01), Parry
patent: 3700189 (1972-10-01), Timperman
patent: 4795111 (1989-01-01), Moller

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