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：US10168704B2

公开(公告)日：2019-01-01

申请号：US15658572

申请日：2017-07-25

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Tong Zhang ,  Mengqiu Wang

IPC: G05D1/10 ,  G05D1/00 ,  B64C39/02 ,  B64D47/08 ,  H04N5/232 ,  G06F3/01 ,  G06F3/16 ,  G06F3/0488 ,  H04N5/225

Abstract: System and method for controlling an aerial system to perform a selected operation using an easy-to-use release and auto-positioning process.

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：US10067504B1

公开(公告)日：2018-09-04

申请号：US15893991

申请日：2018-02-12

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Zheng Qu ,  Pengxiang Jin ,  Tong Zhang

IPC: G05D1/00 ,  G05D1/02 ,  G06F3/01 ,  B64C39/02 ,  G06F3/0488

Abstract: An aerial device includes a body, an optical system having gimbal supporting a camera, a lift mechanism coupled to the body, a haptic sensor coupled to the body and configured to generate haptic data, and a processing system disposed in the body and in data communication with the haptic sensor. The processing system is configured to process the haptic data to understand an intended position of the aerial device and/or an intended orientation of the gimbal and convert the intended position to a target position of the aerial device and/or the intended orientation to a target orientation of the gimbal utilizing said processed data irrespective of an initial position of said aerial device and an initial orientation of said gimbal. Also disclosed is a method for controlling the aerial device.

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.

公开(公告)号：US20170305542A1

公开(公告)日：2017-10-26

申请号：US15495615

申请日：2017-04-24

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Lei Zhang ,  Hanqing Guo ,  Zhaozhe Wang ,  Tong Zhang ,  Mengqiu Wang

IPC: B64C27/32 ,  B64C27/00 ,  B64C11/02 ,  B64C27/14 ,  B64C39/02 ,  B64C27/08

CPC classification number: B64C27/32 ,  B64C11/02 ,  B64C11/04 ,  B64C27/001 ,  B64C27/08 ,  B64C27/14 ,  B64C39/024 ,  B64C2027/003 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108

Abstract: An aerial vehicle including a housing, an outrunner motor including a stator mechanically coupled to the housing and a rotor rotationally coupled to the stator, and a propeller removably coupled to the rotor, the propeller including a hub and a plurality of propeller blades. A rotor, a propeller including a hub and a propeller blade, a radial alignment mechanism, a rotational retention mechanism, and an axial retention mechanism.

公开(公告)号：US11914370B2

公开(公告)日：2024-02-27

申请号：US17178337

申请日：2021-02-18

Applicant: HANGZHOU ZERO ZERO TECHNOLOGY CO., LTD.

Inventor： Tong Zhang ,  Mengqiu Wang

IPC: G05D1/00 ,  B64C39/02 ,  G06F3/01 ,  H04N23/62 ,  H04N23/69 ,  H04N23/63 ,  B64D47/08 ,  G06F3/16 ,  G06F3/0488 ,  H04N23/45 ,  H04N23/51

CPC classification number: G05D1/0088 ,  B64C39/024 ,  G05D1/0016 ,  G05D1/0094 ,  G05D1/0669 ,  G06F3/017 ,  H04N23/62 ,  H04N23/632 ,  H04N23/69 ,  B64D47/08 ,  B64U2201/20 ,  G06F3/0488 ,  G06F3/16 ,  G06F2203/04808 ,  H04N23/45 ,  H04N23/51

Abstract: The present disclosure provides an aerial system, comprising: a body; a lift mechanism coupled to the body; an optical system coupled to the body; and a computer system having at least one processor and at least one memory comprising first program instructions. When the first program instructions are executed by the at least one processor, the at least one processor may be configured to: receive a target operation, the target operation associated with a flight trajectory and a predefined action performed by the optical system and execute the target operation.

公开(公告)号：US11530025B2

公开(公告)日：2022-12-20

申请号：US16834452

申请日：2020-03-30

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Long Zhang ,  Zhaozhe Wang ,  Weiqi Liu ,  Xiaonan Cheng ,  Tong Zhang

IPC: B64C1/30 ,  B64C39/02

Abstract: An unmanned aerial vehicle includes a fuselage body, a foldable wing assembly and a gear assembly. The foldable wing assembly, including a pair of opposing wing members, is coupled to the fuselage body and positionable in a stowed position and a deployed position. The gear assembly positions the wing members in a stowed position and a deployed position and include a support bracket assembly and a pair of opposing hinge members. The support bracket assembly is coupled to the fuselage body and including first and second support brackets forming a cavity therebetween and a pair of opposing hinge members. The pair of opposing hinge members are pivotably coupled to the support bracket assembly and positioned within the cavity. Each hinge member is coupled to a corresponding wing member and includes a set of gear teeth extending outwardly from an arcuate radially outer surface and coupled in a meshed arrangement.

公开(公告)号：US11003181B2

公开(公告)日：2021-05-11

申请号：US16055540

申请日：2018-08-06

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Zheng Qu ,  Pengxiang Jin ,  Tong Zhang

IPC: G05D1/00 ,  G05D1/02 ,  G06F3/01 ,  B64C39/02 ,  G06F3/0488

Abstract: An aerial device includes a body, an optical system having gimbal supporting a camera, a lift mechanism coupled to the body, a haptic sensor coupled to the body and configured to generate haptic data, and a processing system disposed in the body and in data communication with the haptic sensor. The processing system is configured to process the haptic data to understand an intended position of the aerial device and/or an intended orientation of the gimbal and convert the intended position to a target position of the aerial device and/or the intended orientation to a target orientation of the gimbal utilizing said processed data irrespective of an initial position of said aerial device and an initial orientation of said gimbal. Also disclosed is a method for controlling the aerial device.

公开(公告)号：US10901437B2

公开(公告)日：2021-01-26

申请号：US16265707

申请日：2019-02-01

Applicant: Hangzhou Zero Zero Technology Co., Ltd.

Inventor： Tong Zhang ,  Lei Zhang ,  Zhaozhe Wang ,  Xi Zhang ,  Mengwen Tan

IPC: G05D1/10 ,  B64D47/08 ,  B64C39/02 ,  H04N5/225 ,  H04N13/204 ,  G06K9/00 ,  G06T7/50 ,  H04N5/247

Abstract: An unmanned aerial vehicle is described herein. The unmanned aerial vehicle includes a fuselage body, a lift mechanism coupled to the fuselage body, and a depth sensing and obstacle avoidance system coupled to the fuselage body. The depth sensing and obstacle avoidance system includes a platform assembly, a pair of stereovision cameras coupled to a platform assembly, and a motor assembly coupled to the fuselage body and to the platform assembly. The platform assembly includes a support member extending between a first end and an opposite second end along a longitudinal axis. The pair of stereovision cameras includes each stereovision camera positioned at an opposite end of the support member. The motor assembly is configured to rotate the platform assembly with respect to the fuselage body about a rotational axis perpendicular to the longitudinal axis of the platform assembly.