公开(公告)号：US10358214B2

公开(公告)日：2019-07-23

申请号：US16024446

申请日：2018-06-29

Applicant: Hangzhou Zero Zero Technology Co., Ltd

Inventor： Tong Zhang ,  Mengqiu Wang ,  Zhaozhe Wang ,  Xuyang Zhang ,  Guanqun Zhang ,  Shuang Gong ,  Yalin Zhang ,  Jinglong Wang ,  Lixin Liu

IPC: B64C39/02 ,  B64C27/08

Abstract: An aerial vehicle, preferably including: a rotary wing and a protection housing enclosing the rotary wing. An aerial vehicle, preferably including: a first rotary wing module including a first rotary wing and a second rotary wing module including a second rotary wing, wherein the first rotary wing module and the second rotary wing module are preferably operable between a folded configuration and an unfolded configuration. A method of aerial vehicle operation.

公开(公告)号：US20180319496A1

公开(公告)日：2018-11-08

申请号：US16024446

申请日：2018-06-29

Applicant: Hangzhou Zero Zero Technology Co., Ltd

Inventor： Tong Zhang ,  Mengqui Wang ,  Zhaozhe Wang ,  Xuyang Zhang ,  Guanqun Zhang ,  Shuang Gong ,  Yalin Zhang ,  Jinglong Wang ,  Lixin Liu

IPC: B64C39/02 ,  B64C27/08

CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/162 ,  B64C2201/20 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2211/00

Abstract: An aerial vehicle, preferably including: a rotary wing and a protection housing enclosing the rotary wing. An aerial vehicle, preferably including: a first rotary wing module including a first rotary wing and a second rotary wing module including a second rotary wing, wherein the first rotary wing module and the second rotary wing module are preferably operable between a folded configuration and an unfolded configuration. A method of aerial vehicle operation.

公开(公告)号：US20180188730A1

公开(公告)日：2018-07-05

申请号：US15907532

申请日：2018-02-28

Applicant: Hangzhou Zero Zero Technology Co., Ltd

Inventor： Mengqiu Wang ,  Lixin Liu ,  Pengxiang Jin ,  Jia Lu ,  Tong Zhang

IPC: G05D1/00 ,  G05D1/04 ,  G05D1/06 ,  G05D1/08 ,  B64C39/02

Abstract: A method for controlling an aerial system with a rotor enclosed by a housing, including: operating the rotor in a flight mode, detecting a grab event indicative of the aerial system being grabbed, and automatically operating the rotor in a standby mode. A method for controlling an aerial system including a central axis extending normal to a lateral plane of the aerial system, including: generating a first aerodynamic force with a set of rotors enclosed by a housing, detecting that an acute angle between the central axis and a gravity vector is greater than a threshold angle, and operating each rotor of the set of rotors to cooperatively generate a second aerodynamic force less than the first aerodynamic force with the set of rotors.