公开(公告)号：US20200079492A1

公开(公告)日：2020-03-12

申请号：US16128432

申请日：2018-09-11

Applicant: Swift Engineering, Inc.

Inventor： Christopher NOSKOWICZ

IPC: B64C3/56 ,  B64C39/02 ,  B64C9/00

Abstract: A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.

公开(公告)号：US20240116624A1

公开(公告)日：2024-04-11

申请号：US18484394

申请日：2023-10-10

Applicant: SWIFT ENGINEERING, INC.

Inventor： Christopher NOSKOWICZ

IPC: B64C3/56 ,  B64C9/00 ,  B64C39/02

CPC classification number: B64C3/56 ,  B64C9/00 ,  B64C39/024 ,  B64C2009/005 ,  B64U10/25

Abstract: A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.

公开(公告)号：US20210253219A1

公开(公告)日：2021-08-19

申请号：US17111259

申请日：2020-12-03

Applicant: SWIFT ENGINEERING, INC.

Inventor： Christopher NOSKOWICZ

IPC: B64C3/56 ,  B64C39/02 ,  B64C9/00

Abstract: A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.