Comp Air Solutions, LLC

États‑Unis d’Amérique

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        États-Unis 2
        International 1
        Canada 1
Date
2023 1
2022 2
Classe IPC
B64C 25/54 - Flotteurs 4
B64C 35/00 - Hydravions à coqueHydravions à flotteurs 4
B64C 3/26 - Construction, forme ou fixation des revêtements distincts, p. ex. panneaux 2
B64C 3/34 - Réservoirs fabriqués intégralement avec les ailes, p. ex. de carburant ou d'eau 2
B64C 35/02 - Coques d'hydravions 2
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Statut
En Instance 2
Enregistré / En vigueur 2
Résultats pour  brevets

1.

SECONDARY AIRFOIL APPARATUS, SYSTEM, AND METHOD FOR IMPROVING LIFT AND AERODYNAMIC PERFORMANCE OF A FLOATPLANE

      
Numéro d'application 18236773
Statut En instance
Date de dépôt 2023-08-22
Date de la première publication 2023-12-21
Propriétaire Comp Air Solutions, LLC (USA)
Inventeur(s)
  • Lueck, Ronald A.
  • Ryan, Michael

Abrégé

The present disclosure relates to a secondary airfoil apparatus, system and method for improving lift, takeoff, landing and aerodynamic performance of a floatplane. The secondary airfoil is itself of sufficient structural rigidity to withstand any and all forces added by the airfoil during floatplane operation, and is fixedly attached between the floats of the floatplane. The secondary airfoil can be arranged at an optimal angle of incidence and vertical lift position relative to the primary airfoil, or wing of the aircraft, and relative to the floats center of gravity and drag for optimal maneuverability of the floatplane.

Classes IPC  ?

  • B64C 35/00 - Hydravions à coqueHydravions à flotteurs
  • B64C 3/34 - Réservoirs fabriqués intégralement avec les ailes, p. ex. de carburant ou d'eau
  • B64C 25/54 - Flotteurs
  • B64C 3/26 - Construction, forme ou fixation des revêtements distincts, p. ex. panneaux
  • B64D 37/16 - Systèmes de remplissage

2.

SECONDARY AIRFOIL APPARATUS, SYSTEM, AND METHOD FOR IMPROVING LIFT AND AERODYNAMIC PERFORMANCE OF A FLOATPLANE

      
Numéro d'application US2022016807
Numéro de publication 2022/178134
Statut Délivré - en vigueur
Date de dépôt 2022-02-17
Date de publication 2022-08-25
Propriétaire COMP AIR SOLUTIONS, LLC (USA)
Inventeur(s)
  • Lueck, Ronald A.
  • Ryan, Michael

Abrégé

The present disclosure relates to a secondary airfoil apparatus, system and method for improving lift, takeoff, landing and aerodynamic performance of a floatplane. The secondary airfoil can be integrated into the floatplane during manufacture, or retrofitted to an existing floatplane after manufacture. The secondary airfoil is itself of sufficient structural rigidity to withstand any and all forces added by the airfoil during floatplane operation. The secondary airfoil is fixedly attached between the floats of the floatplane, and are purposefully not attached to spreader bars that can exist typically between the floats. The secondary airfoil can be arranged at an optimal angle of incidence and vertical lift position relative to the primary airfoil, or wing of the aircraft, and relative to the floats center of gravity and drag for optimal maneuverability of the floatplane.

Classes IPC  ?

3.

Secondary airfoil apparatus, system, and method for improving lift and aerodynamic performance of a floatplane

      
Numéro d'application 17674542
Numéro de brevet 11731761
Statut Délivré - en vigueur
Date de dépôt 2022-02-17
Date de la première publication 2022-08-18
Date d'octroi 2023-08-22
Propriétaire Comp Air Solutions, LLC (USA)
Inventeur(s)
  • Lueck, Ronald A.
  • Ryan, Michael

Abrégé

The present disclosure relates to a secondary airfoil apparatus, system and method for improving lift, takeoff, landing and aerodynamic performance of a floatplane. The secondary airfoil can be integrated into the floatplane during manufacture, or retrofitted to an existing floatplane after manufacture. The secondary airfoil is itself of sufficient structural rigidity to withstand any and all forces added by the airfoil during floatplane operation. The secondary airfoil is fixedly attached between the floats of the floatplane, and are purposefully not attached to spreader bars that can exist typically between the floats. The secondary airfoil can be arranged at an optimal angle of incidence and vertical lift position relative to the primary airfoil, or wing of the aircraft, and relative to the floats center of gravity and drag for optimal maneuverability of the floatplane.

Classes IPC  ?

  • B64C 35/00 - Hydravions à coqueHydravions à flotteurs
  • B64C 3/34 - Réservoirs fabriqués intégralement avec les ailes, p. ex. de carburant ou d'eau
  • B64C 25/54 - Flotteurs
  • B64C 3/26 - Construction, forme ou fixation des revêtements distincts, p. ex. panneaux
  • B64D 37/16 - Systèmes de remplissage

4.

SECONDARY AIRFOIL APPARATUS, SYSTEM, AND METHOD FOR IMPROVING LIFT AND AERODYNAMIC PERFORMANCE OF A FLOATPLANE

      
Numéro de document 03208836
Statut En instance
Date de dépôt 2022-02-17
Propriétaire COMP AIR SOLUTIONS, LLC (USA)
Inventeur(s)
  • Lueck, Ronald A.
  • Ryan, Michael

Abrégé

The present disclosure relates to a secondary airfoil apparatus, system and method for improving lift, takeoff, landing and aerodynamic performance of a floatplane. The secondary airfoil can be integrated into the floatplane during manufacture, or retrofitted to an existing floatplane after manufacture. The secondary airfoil is itself of sufficient structural rigidity to withstand any and all forces added by the airfoil during floatplane operation. The secondary airfoil is fixedly attached between the floats of the floatplane, and are purposefully not attached to spreader bars that can exist typically between the floats. The secondary airfoil can be arranged at an optimal angle of incidence and vertical lift position relative to the primary airfoil, or wing of the aircraft, and relative to the floats center of gravity and drag for optimal maneuverability of the floatplane.

Classes IPC  ?