Dirisolar

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Classe IPC
B64B 1/00 - Aéronefs plus légers que l'air 2
B64B 1/20 - Dirigeables rigidesDirigeables semi-rigides comportant des ailes ou des surfaces stabilisatrices 2
B64B 1/66 - Fixations d'amarrage 2
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1.

Airship, anchoring device, and landing and mooring method

      
Numéro d'application 14233293
Numéro de brevet 09415852
Statut Délivré - en vigueur
Date de dépôt 2012-07-19
Date de la première publication 2014-06-12
Date d'octroi 2016-08-16
Propriétaire DIRISOLAR (France)
Inventeur(s) Tixier, Philippe

Abrégé

An air vehicle such as an airship is provided, having a rounded top portion, and the bottom portion of which has a substantially planar shape, including a region having a smaller inclination, which is referred to as a bottom surface, and the surface area of which is larger than that of an intermediate region having a greater inclination, referred to as an intermediate surface. The general shape produces, due to relative wind, a resulting overall downward force near the ground. The vehicle also includes a device for anchoring same to the ground, the anchoring device being stationary or controllable from the vehicle, located at the front portion of the vehicle, and projecting downward, in particular a ram including a portion which can be expanded by applying a bar against a translatably movable shoulder. Also included is a landing method implementing such a vehicle.

Classes IPC  ?

  • B64B 1/00 - Aéronefs plus légers que l'air
  • B64B 1/20 - Dirigeables rigidesDirigeables semi-rigides comportant des ailes ou des surfaces stabilisatrices
  • B64B 1/66 - Fixations d'amarrage

2.

AIRSHIP, ANCHORING DEVICE, AND LANDING AND MOORING METHOD

      
Numéro d'application FR2012051710
Numéro de publication 2013/011241
Statut Délivré - en vigueur
Date de dépôt 2012-07-19
Date de publication 2013-01-24
Propriétaire DIRISOLAR (France)
Inventeur(s) Tixier, Philippe

Abrégé

The present invention relates to an air vehicle such as an airship, which has a rounded top portion, and the bottom portion of which has a substantially planar shape (711), specifically consisting of a region which has a smaller inclination, which is referred to as a bottom surface (S2), and the surface area of which is larger or even much larger than that of the intermediate region having a greater inclination, referred to as an intermediate surface (S1). Said general shape produces, due to relative wind (69), a resulting overall downward force (67) near the ground. According to the invention, said vehicle also includes a device for anchoring same to the ground (722), said anchoring device being stationary or controllable from said vehicle, located at the front portion of said vehicle, and projecting downward, in particular a ram (722, 9) including a portion (921, 922) which can be expanded by applying a bar (924) against a translatably movable shoulder (923). The invention also relates to a landing method implementing such a vehicle. Said method involves, as a result of the downward force (67) with compensation (65) by maintaining a nose-up attitude (T711), downward flight until a rear portion (730) of the vehicle makes contact with the ground, followed by reducing the nose-up angle until the anchoring device makes contact with the ground, in particular with a ram (722, 9) sinking into the ground. Preferably, the method also includes docking, in particular by means of an expandable ram (9), while the vehicle is applied against the ground due to the downward force.

Classes IPC  ?

  • B64B 1/20 - Dirigeables rigidesDirigeables semi-rigides comportant des ailes ou des surfaces stabilisatrices
  • B64B 1/66 - Fixations d'amarrage
  • B64B 1/00 - Aéronefs plus légers que l'air