CBAI Technologies Private Limited

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Classe IPC
B64U 70/83 - Décollage ou atterrissage verticaux, p. ex. utilisant des fusées en utilisant des parachutes, des ballons ou similaires 2
B64U 20/87 - Montage des dispositifs d’imagerie, p. ex. montage des suspensions à cardan 1
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1.

A CONTROLLED AERIAL VEHICLE

      
Numéro d'application IB2023061726
Numéro de publication 2024/110859
Statut Délivré - en vigueur
Date de dépôt 2023-11-21
Date de publication 2024-05-30
Propriétaire CBAI TECHNOLOGIES PRIVATE LIMITED (Inde)
Inventeur(s)
  • Vidyasagar, Rangoju
  • Sairaj, Bayela

Abrégé

The present disclosure relates to a controlled aerial vehicle (100). The controlled aerial vehicle (100) includes a frame (102) defining housing. The frame (102) is configured to house a control module of the controlled aerial vehicle (100). Further, the controlled aerial vehicle (100) includes a plurality of elongated arms (104a, 104b, 104c, 104d) extending outwardly from the frame (102). Further, the vehicle (100) is provided with one or more landing structures (110a, 110b) coupled to the bottom surface (102b) of the frame (102) for providing support for the aerial vehicle during landing and take-off. Furthermore, a mounting means (114) is releasably connectable to the frame configured to receive and support a payload or imaging module (112). The present disclosure provides a controlled aerial vehicle configuration with the payload or imaging module (112) having more clearance to protect the payload during the event of a crash.

Classes IPC  ?

  • B64U 70/83 - Décollage ou atterrissage verticaux, p. ex. utilisant des fusées en utilisant des parachutes, des ballons ou similaires
  • B64U 20/87 - Montage des dispositifs d’imagerie, p. ex. montage des suspensions à cardan

2.

AN APPARATUS FOR SOFT LANDING OF AN UNMANNED AERIAL VEHICLE

      
Numéro d'application IB2023061685
Numéro de publication 2024/105643
Statut Délivré - en vigueur
Date de dépôt 2023-11-20
Date de publication 2024-05-23
Propriétaire CBAI TECHNOLOGIES PRIVATE LIMITED (Inde)
Inventeur(s)
  • Vidyasagar, Rangoju
  • Sairaj, Bayela

Abrégé

Present disclosure discloses an apparatus (100) for soft landing an unmanned aerial vehicle (UAV) (200) comprising a plurality of holders (120) attached to a body (106) of the UAV (200). At least one parachute (140a, 140b) configurable within each of the plurality of holders about at least one canister (132). The plurality of holders comprises at least one provision (126) extending from each holder of the plurality of holders. A connecting member (135) is defined with a sleeve portion (136) and at least one protrusion extends from the sleeve portion. The sleeve portion is configured to receive the at least one canister and the at least one protrusion is receivable within the at least one provision. The connecting member is removably attached to each of the plurality of holders about the at least one provision to accommodate the at least one parachute in a soft landing of the UAV.

Classes IPC  ?

  • B64U 70/83 - Décollage ou atterrissage verticaux, p. ex. utilisant des fusées en utilisant des parachutes, des ballons ou similaires