Single-Engine Hovercraft Control System and Method

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United States of America Patent

APP PUB NO 20230365114A1
SERIAL NO

18317557

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Abstract

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A control system of a hovercraft that includes one engine and one propulsion fan enclosed in a duct in which swivel side flaps are located is described. The control system includes, downstream of the duct, at least three rudders. Each of the rudders operates in the full range of angular position, regardless of the position of the swivel side flaps. A control method of such a hovercraft is also described.

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Patent Owner(s)

Patent OwnerAddress
LUKASIEWICZ RESEARCH NETWORK - INSTITUTE OF AVIATIONAL KRAKOWSKA 110/114 WARSAW 02-256

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Janiszewski, Marcin Pruszków, PL 1 0
Kozaczuk, Konrad Siemien, PL 1 0
Szafran, Krzysztof Nadarzyn, PL 1 0
Zalewski, Wieslaw Bialobrzegi, PL 1 0

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