WO2025006383 - GROUND EFFECT AIRCRAFT

National phase entry is expected:
Publication Number WO/2025/006383
Publication Date 02.01.2025
International Application No. PCT/US2024/035242
International Filing Date 24.06.2024
Title **
[English] GROUND EFFECT AIRCRAFT
[French] AÉRONEF À EFFET DE SOL
Applicants **
SUPPES, Galen
Inventors
SUPPES, Adam
Priority Data
63/523,094   25.06.2023   US
63/530,177   01.08.2023   US
63/532,922   16.08.2023   US
63/535,370   30.08.2023   US
63/541,405   29.09.2023   US
63/605,544   03.12.2023   US
63/616,719   31.12.2023   US
63/554,100   15.02.2024   US
63/649,487   20.05.2024   US
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Quotation for National Phase entry

Country StagesTotal
China Filing, Examination, Granting2691
EPO Filing, Examination, Granting10486
Japan Filing, Examination, Granting2309
South Korea Filing, Examination, Granting2731
USA Filing, Examination, Granting4310
MasterCard Visa
Total: 22,527

The term for entry into the National Phase has expired. This quotation is for informational purposes only

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Abstract[English] Aerial platforms, especially ground-effect flight platforms, benefit from common aerial platform embodiments having complementary synergies to create lift-drag ratio efficiencies higher than alternative art. For ground-effect applications, a lower cavity is defined by a trailing-edge flap, side fences, and an effective lower-surface average pitch between zero and 3°. The forward surface is configured to provide induced thrust. The effective lower-surface pitch is substantially equal to the pitch of the line going from forward stagnation point and the lowest part of the trailing-edge flap.[French] Des plateformes aériennes, en particulier des plateformes de vol à effet de sol, bénéficient de modes de réalisation de plateformes aériennes communes ayant des synergies complémentaires pour créer des rendements de rapport de portance-traînée supérieurs à ceux de l'art alternatif. Pour des applications à effet de sol, une cavité inférieure est définie par un volet de bord de fuite, des barrières tribord et un pas moyen de surface inférieure efficace entre zéro et 3°. La surface avant est conçue pour fournir une poussée induite. Le pas de surface inférieure efficace est sensiblement égal au pas de la ligne allant du point de stagnation avant et de la partie la plus basse du volet de bord de fuite.