专利检索 ap:("Flirtey Holdings, Inc.") AND inv:"FOGGIA, John R." 第 1 页

1.

发明公开
AERIAL VEHICLE DETECTION SYSTEM 审中-公开

公开(公告)号：EP3682435A1

公开(公告)日：2020-07-22

申请号：EP18779953.1

申请日：2018-09-13

申请人： Flirtey Holdings, Inc.

发明人： SWEENY, Matthew , FOGGIA, John R. , MALLOY, Allison

IPC分类号： G08G5/00 , G08G5/04 , G01S13/93 , G01S13/91 , G01S13/87 , G01S13/72

2.

发明公开
UAV FACILITY 审中-公开

公开(公告)号：EP3681802A1

公开(公告)日：2020-07-22

申请号：EP18779954.9

申请日：2018-09-13

申请人： Flirtey Holdings, Inc.

发明人： SWEENY, Matthew , FOGGIA, John R. , HAYDEN, Jess , RINALDI, Joseph

IPC分类号： B64F1/22 , B64F1/00 , B64C39/02

3.

发明公开
UNMANNED AERIAL VEHICLE (UAV) POSITIONING MECHANISMS FOR MOVING A UAV ACROSS A SURFACE 审中-公开

公开(公告)号：EP3681803A1

公开(公告)日：2020-07-22

申请号：EP18800350.3

申请日：2018-09-13

申请人： Flirtey Holdings, Inc.

发明人： SWEENY, Matthew , FOGGIA, John R. , HAYDEN, Jess , RINALDI, Joseph

IPC分类号： B64F1/22 , B64F1/00 , B64C39/02 , B64F1/12

4.

发明公开
UNMANNED AERIAL VEHICLE AND PAYLOAD DELIVERY SYSTEM 审中-公开

公开(公告)号：EP3681798A1

公开(公告)日：2020-07-22

申请号：EP18780281.4

申请日：2018-09-13

申请人： Flirtey Holdings, Inc.

发明人： SWEENY, Matthew , KILGORE, Andrianah Jade , FOGGIA, John R.

IPC分类号： B64C39/02 , B64D1/08 , B64D1/12

5.

发明公开
PARACHUTE CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE 审中-公开

公开(公告)号：EP3362360A1

公开(公告)日：2018-08-22

申请号：EP16856334.4

申请日：2016-10-14

申请人： Flirtey Holdings, Inc.

发明人： FATHALLAH, Michel , SWEENEY, Matthew , BASS, Tom , BADDAM, Kranthi , FOGGIA, John R.

IPC分类号： B64D17/80 , B64C9/32 , B64C25/56 , B64C27/08 , B64D17/00

CPC分类号： B64D17/80 , B64C25/58 , B64C39/024 , B64C2201/108 , B64C2201/146 , B64C2201/185 , B64D17/70 , B64D45/00 , G05D1/0038 , G05D1/105

摘要： Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automatically, e.g., in response to a variety of failures such as a free fall, or manually from a base unit operated by a remote user. For example, the PDS can determine the failure of the drone based on data obtained from an accelerometer, a gyroscope, a magnetometer and a barometer of the drone and automatically deploy the parachute if any failure is determined. In another example, the remote user can “kill” the drone, that is, cut off the power supply to the drone and deploy the parachute by activating an onboard “kill” switch from the base unit.