公开(公告)号：US11745874B2

公开(公告)日：2023-09-05

申请号：US17048414

申请日：2019-04-17

Applicant: AVSS-AERIAL VEHICLE SAFETY SOLUTIONS INC.

Inventor： Josh Ogden ,  Josh Boudreau ,  Robert D. Watters ,  Mike Sirois ,  Luc Boucher ,  Etienne Poisson

IPC: B64C9/02 ,  B64C39/02 ,  B64D17/70 ,  B64D17/80 ,  B64U70/83

CPC classification number: B64C39/024 ,  B64D17/70 ,  B64D17/80 ,  B64U70/83 ,  B64U2201/20

Abstract: An apparatus an unmanned aerial vehicle recovery system is provided. The apparatus includes a base to mount to an unmanned aerial vehicle. The apparatus further includes a housing to engage the base. In addition, the apparatus includes a parachute disposed within the housing. Also, the apparatus includes a deployment mechanism to deploy the parachute. The deployment mechanism is to eject the housing away from the base upon a triggering event.

公开(公告)号：US20210155343A1

公开(公告)日：2021-05-27

申请号：US17048414

申请日：2019-04-17

Applicant: AVSS - AERIAL VEHICLE SAFETY SOLUTIONS INC.

Inventor： Josh OGDEN ,  Josh BOUDREAU ,  Robert D. WATTERS ,  Mike SIROIS ,  Luc BOUCHER ,  Etienne POISSON

IPC: B64C39/02 ,  B64D17/70

Abstract: An apparatus an unmanned aerial vehicle recovery system is provided. The apparatus includes a base to mount to an unmanned aerial vehicle. The apparatus further includes a housing to engage the base. In addition, the apparatus includes a parachute disposed within the housing. Also, the apparatus includes a deployment mechanism to deploy the parachute. The deployment mechanism is to eject the housing away from the base upon a triggering event.

公开(公告)号：US20240166382A1

公开(公告)日：2024-05-23

申请号：US18282054

申请日：2022-03-14

Applicant: AVSS - AERIAL VEHICLE SAFETY SOLUTIONS INC.

Inventor： Joshua BOUDREAU ,  Ashim PANTA ,  Joshua OGDEN ,  Reay O'DARE ,  Ryan DES COTES ,  Robert D. WATTERS ,  Joseph Luc BOUCHER ,  Thomas MOORE ,  Michael SIROIS

IPC: B64U10/50 ,  B64D1/08 ,  B64D17/02 ,  B64D17/34 ,  B64D17/80 ,  B64U101/64

CPC classification number: B64U10/50 ,  B64D1/08 ,  B64D17/02 ,  B64D17/34 ,  B64D17/80 ,  B64U2101/64 ,  B64U2201/10

Abstract: A system for payload delivery and drone recovery, wherein the system functions with the use of a lightweight parachute and a directional control module. The system can include a drop system for payload delivery, wherein the drop system releases the parachute and payload upon reaching a target site. The system can also include a recovery system, wherein the recovery system deploys the parachute and steers the failed drone to a target site. A lightweight ram-air parachute is used to provide a lighter steerable parachute system.