公开(公告)号：US10683102B2

公开(公告)日：2020-06-16

申请号：US16280476

申请日：2019-02-20

Applicant: Wing Aviation LLC

Inventor： Joanna Cohen ,  Parsa Dormiani ,  Mathias Samuel Fleck ,  James Ryan Burgess ,  Sean Mullaney

IPC: B64F1/00 ,  B64F1/04 ,  B64F1/02 ,  B64F1/18 ,  B64C39/02

Abstract: Described herein are apparatuses that provided various features related to unmanned aerial vehicles (UAVs). An example apparatus may include, among other features, (i) a launch system for a UAV, (ii) a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight, and (iii) a mechanical battery-replacement system that is configured to (a) remove a first battery from the UAV, and (b) after removal of the first battery, install a second battery in the UAV.

公开(公告)号：US20190248509A1

公开(公告)日：2019-08-15

申请号：US16280476

申请日：2019-02-20

Applicant: Wing Aviation LLC

Inventor： Joanna Cohen ,  Parsa Dormiani ,  Mathias Samuel Fleck ,  James Ryan Burgess ,  Sean Mullaney

IPC: B64F1/04 ,  B64F1/18 ,  B64F1/02 ,  B64C39/02

Abstract: Described herein are apparatuses that provided various features related to unmanned aerial vehicles (UAVs). An example apparatus may include, among other features, (i) a launch system for a UAV, (ii) a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight, and (iii) a mechanical battery-replacement system that is configured to (a) remove a first battery from the UAV, and (b) after removal of the first battery, install a second battery in the UAV.

公开(公告)号：US10239638B1

公开(公告)日：2019-03-26

申请号：US14619673

申请日：2015-02-11

Applicant: Wing Aviation LLC

Inventor： Joanna Cohen ,  Parsa Dormiani ,  Mathias Samuel Fleck ,  James Ryan Burgess ,  Sean Mullaney

IPC: B64F1/00 ,  B64F1/02 ,  B64F1/04 ,  B64F1/18 ,  B64C39/02

Abstract: Described herein are apparatuses that provided various features related to unmanned aerial vehicles (UAVs). An example apparatus may include, among other features, (i) a launch system for a UAV, (ii) a landing feature that is arranged on the apparatus so as to receive the UAV when the UAV returns from a flight, and (iii) a mechanical battery-replacement system that is configured to (a) remove a first battery from the UAV, and (b) after removal of the first battery, install a second battery in the UAV.