公开(公告)号：USD1044677S1

公开(公告)日：2024-10-01

申请号：US29706119

申请日：2019-09-18

Applicant: Wing Aviation LLC

Designer： Trevor Shannon ,  Evan Twyford ,  Giulia Pantalone

Abstract: FIG. 1 is a perspective view of a fairing showing our new design;
FIG. 2 is a front view thereof;
FIG. 3 is a rear view thereof;
FIG. 4 is a left side view thereof;
FIG. 5 is a right side view thereof;
FIG. 6 is a top view thereof; and,
FIG. 7 is a bottom view thereof.
The broken lines in the drawings depict portions of the fairing that form no part of the claimed design.

公开(公告)号：USD1034312S1

公开(公告)日：2024-07-09

申请号：US29875105

申请日：2023-04-28

Applicant: Wing Aviation LLC

Designer： André Prager ,  Giulia Pantalone ,  Evan Twyford

Abstract: FIG. 1 is a top view of an unmanned aerial vehicle (“UAV”);
FIG. 2 is a bottom view thereof;
FIG. 3 is a left side view thereof;
FIG. 4 is a right side view thereof;
FIG. 5 is a front view thereof;
FIG. 6 is a back view thereof;
FIG. 7 is a front perspective view thereof; and,
FIG. 8 is a back perspective view thereof.
The broken lines are included for the purpose of illustrating portions of the vehicle that form no part of the claimed design.

公开(公告)号：US11891164B1

公开(公告)日：2024-02-06

申请号：US17957750

申请日：2022-09-30

Applicant: WING Aviation LLC

Inventor： Adam Woodworth ,  Giulia Pantalone ,  Michelle Suen ,  Luis Prado

IPC: B64C19/02 ,  B64C39/02 ,  B64C5/08 ,  B64C9/18 ,  B64C3/32 ,  B64U10/25 ,  B64U101/60

CPC classification number: B64C19/02 ,  B64C3/32 ,  B64C5/08 ,  B64C9/18 ,  B64C39/024 ,  B64U10/25 ,  B64U2101/60 ,  B64U2201/10

Abstract: A technique of operating an unmanned aerial vehicle (UAV) adapted for a package delivery mission includes: powering distributed propulsion units during takeoff and landing segments of the package delivery mission and idling at least a portion of the distributed propulsion units while powering a pair of outboard propulsion units during a cruise segment of the package delivery mission. The distributed propulsion units are mounted below fixed wings of the UAV and have first propellers mounted fore of the fixed wings. The outboard propulsion units are each mounted to a corresponding one of the fixed wings outboard of the distributed propulsion units. The outboard propulsion units include outboard propellers having a larger diameter than the first propellers.

公开(公告)号：US20220024569A1

公开(公告)日：2022-01-27

申请号：US16937279

申请日：2020-07-23

Applicant: Wing Aviation LLC

Inventor： Giulia Pantalone ,  André Prager

IPC: B64C27/57 ,  B64C27/46 ,  B64C27/473 ,  B64C11/20 ,  B64C27/39 ,  B64C39/02

Abstract: A propeller blade for an unmanned aerial vehicle (“UAV”) is disclosed. The UAV includes a plurality of lift propellers and at least one thrust propeller. Each of the plurality of thrust propellers includes a thrust propeller blade coupled to a hub of the thrust propeller. The thrust propeller blade is configured such that a centrifugal force acting on the thrust propeller blade causes a thrust propeller disk area to increase from a first disk area when the UAV is in a first operational state to a second disk area when the UAV is in a second operational state.

公开(公告)号：US20210276704A1

公开(公告)日：2021-09-09

申请号：US17149355

申请日：2021-01-14

Applicant: Wing Aviation LLC

Inventor： Giulia Pantalone ,  Adam Woodworth ,  André Prager

IPC: B64C27/46 ,  B64C27/467 ,  B64C27/08 ,  B64C39/02

Abstract: An aerial vehicle is provided including rotor units connected to the aerial vehicle, and a control system configured to operate at least one of the rotor units. The rotor unit includes rotor blades, wherein each rotor blade includes a surface area, and wherein an asymmetric parameter is defined, at least in part, by the relationship between the surface areas of the rotor blades. The value of the asymmetric parameter is selected such that the operation of the rotor unit: (i) moves the rotor blades such that each rotor blade produces a respective vortex and (ii) the respective vortices cause the rotor unit to produce a sound output having an energy distribution defined, at least in part, by a set of frequencies, wherein the set of frequencies includes a fundamental frequency, one or more harmonic frequencies, and one or more non-harmonic frequencies having a respective strength greater than a threshold strength.

公开(公告)号：US10604245B2

公开(公告)日：2020-03-31

申请号：US15396399

申请日：2016-12-30

Applicant: Wing Aviation LLC

Inventor： Giulia Pantalone ,  Adam Woodworth

IPC: B64C27/46 ,  B64C27/467 ,  B64C39/02 ,  B64C27/08 ,  B64C27/32

Abstract: An aerial vehicle is provided including rotor units connected to the aerial vehicle, and a control system configured to operate at least one of the rotor units. The rotor unit includes rotor blades, wherein each rotor blade includes a surface area, and wherein an asymmetric parameter is defined, at least in part, by the relationship between the surface areas of the rotor blades. The value of the asymmetric parameter is selected such that the operation of the rotor unit: (i) moves the rotor blades such that each rotor blade produces a respective vortex and (ii) the respective vortices cause the rotor unit to produce a sound output having an energy distribution defined, at least in part, by a set of frequencies, wherein the set of frequencies includes a fundamental frequency, one or more harmonic frequencies, and one or more non-harmonic frequencies having a respective strength greater than a threshold strength.