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Résultats pour
 brevets
1.
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Ground effect flight vehicle
| Numéro d'application |
18032470 |
| Numéro de brevet |
12252247 |
| Statut |
Délivré - en vigueur |
| Date de dépôt |
2021-10-12 |
| Date de la première publication |
2023-11-30 |
| Date d'octroi |
2025-03-18 |
| Propriétaire |
Speeder Systems Holding B.V. (Pays‑Bas)
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| Inventeur(s) |
- Kazakli, Ahmet Erdem
- Ozistek, Tadao Deniz
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Abrégé
a fuselage (1), a wing assembly (4, 5), an engine assembly comprising one or more engines or engine sets (6, 7, 8), and a hull (2) for enabling floatation of the vehicle; wherein the wing assembly (4, 5) comprises stabilizer wings (4) and/or the one or more engines (6, 7, 8) are equipped to provide an airflow departing from the engines (6, 7, 8) which is positionable in one of multiple positions, a first position of the multiple positions which is arranged to generate lift for vertical take-off purpose, and a second position of the multiple positions which is for horizontal cruise flight.
Classes IPC ?
- B64C 35/00 - Hydravions à coqueHydravions à flotteurs
- B60V 1/14 - PropulsionCommande à cet effet
- B64C 29/00 - Aéronefs capables d'atterrir ou de décoller à la verticale, p. ex. aéronefs à décollage et atterrissage verticaux [ADAV, en anglais VTOL]
- B64C 39/12 - Avions canards
- B64D 27/24 - Aéronefs caractérisés par le type ou la position des groupes moteurs utilisant la vapeur ou l'énergie de ressorts
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2.
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A GROUND EFFECT FLIGHT VEHICLE
| Numéro de document |
03195776 |
| Statut |
En instance |
| Date de dépôt |
2021-10-12 |
| Date de disponibilité au public |
2022-04-28 |
| Propriétaire |
SPEEDER SYSTEMS HOLDING B.V. (Pays‑Bas)
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| Inventeur(s) |
- Kazakli, Ahmet Erdem
- Ozistek, Tadao Deniz
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Abrégé
A ground effect flight vehicle comprising, a fuselage (1), a wing assembly (4, 5), an engine assembly comprising one or more engines or engine sets (6, 7, 8), and a hull (2) for enabling floatation of the vehicle; wherein the wing assembly (4, 5) comprises stabilizer wings (4) and/or the one or more engines (6, 7, 8) are equipped to provide an airflow departing from the engines (6, 7, 8) which is positionable in one of multiple positions, a first position of the multiple positions which is arranged to generate lift for vertical take-off purpose, and a second position of the multiple positions which is for horizontal cruise flight.
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