公开(公告)号：US20180105271A1

公开(公告)日：2018-04-19

申请号：US15656295

申请日：2017-07-21

Applicant: Dynetics, Inc.

Inventor： Aaron Wypyszynski ,  Bill Martin ,  John Roy ,  Stephen R. Norris

IPC: B64D1/00 ,  B64C39/02

Abstract: The present disclosure primarily relates to interceptor unmanned aerial systems and methods for countering Unmanned Aerial Systems (UAS), although the inventions disclosed herein are useful for capture of any aerial object. The system utilizes a rigid effector frame, an effector attached directly to the frame, and at least two propulsion elements connected to the effector frame, and is configured to intercept and disable threat UAS. The disclosed systems can be oriented to any virtually any angle to maximize the chances of intercept.

公开(公告)号：US20200331605A1

公开(公告)日：2020-10-22

申请号：US16906405

申请日：2020-06-19

Applicant: Dynetics, Inc.

Inventor： Aaron Wypyszynski ,  Bill Martin ,  John Roy ,  Stephen R. Norris

IPC: B64C39/02 ,  F41H11/04

Abstract: The present disclosure primarily relates to interceptor unmanned aerial systems and methods for countering Unmanned Aerial Systems (UAS), although the inventions disclosed herein are useful for capture of any aerial object. The system utilizes a rigid effector frame, an effector attached directly to the frame, and at least two propulsion elements connected to the effector frame, and is configured to intercept and disable threat UAS. The disclosed systems can be oriented to any virtually any angle to maximize the chances of intercept.

公开(公告)号：US10689109B2

公开(公告)日：2020-06-23

申请号：US15656295

申请日：2017-07-21

Applicant: Dynetics, Inc.

Inventor： Aaron Wypyszynski ,  Bill Martin ,  John Roy ,  Stephen R. Norris

IPC: B64C39/02 ,  F41H11/04

Abstract: The present disclosure primarily relates to interceptor unmanned aerial systems and methods for countering Unmanned Aerial Systems (UAS), although the inventions disclosed herein are useful for capture of any aerial object. The system utilizes a rigid effector frame, an effector attached directly to the frame, and at least two propulsion elements connected to the effector frame, and is configured to intercept and disable threat UAS. The disclosed systems can be oriented to any virtually any angle to maximize the chances of intercept.