Sz Dji Technology Co., Ltd.

Sz Zuvi Technology Co., Ltd.

Sz Dji Osmo Technology Co., Ltd.

Zte Corporation

Yin Tang

Tao Zhao

Feihu Yang

Jiangang Feng

Tao Peng

Lei Deng

Hualiang Qiu

Guisheng Nong

Rongming Xiong

Lei Zhang

Wentao Wang

Yumian Deng

Shengjia Guo

Mingyu Wang

Cong Zhao

Guyue Zhou

Xifeng Zhao

Bo Yuan

Honghui Zhang

Yanxin Huang

Xiaokai Guo

Xingwang Xu

Zhenkai Wu

Xianwu Xiong

Guozhu Gui

Dexi Li

Shaojie Chen

Yun Yu

Yonggen Wang

Yun Zhao

Shaofu Peng

Ran Chen

Zhenhua Xu

Xing Huang

Hualiang Qui

A controlling method for an unmanned aerial vehicle (UAV) that includes an image device. The controlling method includes transmitting, by a remote controller when a dial of a dial structure of the remote controller is rotated, a first control signal for changing imaging device information of an imaging device of the UAV via a signal transmitting device of the remote controller. The imaging device information comprises at least one of an operating mode of the imaging device, a shutter speed of the imaging device, an aperture size of the imaging device, a light sensitivity of the imaging device, or a preview image of the imaging device. The controlling method further includes transmitting a second control signal for confirming imaging device information via the signal transmitting device by the controller when the dial is slid with a displacement.

Dial structure, remote controller employing the same, and controlling method

An unmanned aerial vehicle includes a central body, a plurality of arms extendable from the central body, and one or more joints. Each of the plurality of arms is configured to support one or more propulsion units, and is configured to transform between (1) a flight configuration in which the arm is extending away from the central body and (2) a compact configuration in which the arm is folded against the central body. Each joint is configured to couple one arm to the central body. At least one of the one or more joints includes an elastic element configured to cause at least one of the plurality of arms to automatically retract when the at least one of the plurality of arms is reversibly folded to a first predetermined state, and automatically extend when the at least one of the plurality of arms is reversibly extended to a second predetermined state.

Foldable multi-rotor aerial vehicle

Apparatuses and methods for drying objects are provided. The apparatus can comprise a housing configured to provide an airflow channel having an airflow inlet and an airflow outlet, an airflow generating element configured to effect an airflow through the airflow channel, and one or more radiation energy sources configured to generate infrared radiation and direct the infrared radiation toward an exterior of the housing. At least a portion of at least one of the one or more radiation energy sources does not contact the airflow channel or the airflow, thereby maintaining an operating temperature of the radiation energy source within a predetermined range.

Apparatuses and methods for drying an object

A movable object includes a body, one or more propulsion units carried by the body and configured to effect movement of the movable object, and an electrical plug for power and signal transmission. The electrical plug includes at least one signal pin configured to communicate signal, a plurality of power pins configured to transmit electrical power, and a plug substrate configured to support the at least one signal pin and the plurality of power pins. The plurality of power pins include at least one power pin having a first polarity and at least one power pin having a second polarity opposite to the first polarity. The one or more propulsion units are provided with electrical energy via the electrical plug. The plurality of power pins and the at least one signal pin include a first set of power pins and signal pins, and a second set of power pins and signal pins. The first set and the second set are disposed symmetrically opposite to each other on the plug substrate, and the second set is provided in a row with the first set.

Electrical connector

A gimbal photographing device includes a fuselage; a folding mechanism, connected to the fuselage; and a gimbal camera, connected to the folding mechanism. The gimbal camera is foldable and unfoldable relative to the fuselage via the folding mechanism. A power switch is disposed on the fuselage. The folding mechanism includes a base connected to the gimbal camera. When the gimbal camera is unfolded relative to the fuselage, the base is configured to abut against the power switch to turn on the gimbal photographing device.

Foldable gimbal photographing device

A gimbal handle includes an enclosure including an accommodation space, a main control board accommodated in the accommodation space, and an electrical contact member provided at the main control board and electrically connected to the main control board. The electrical contact member penetrates the enclosure to expose to an outside of the enclosure. The electrical contact member is configured to be electrically connected to an adapter.

Gimbal handle and gimbal having same

A hand-held gimbal includes a handle portion and a gimbal photographing device mounted on the handle portion. A display screen is disposed at the handle portion and configured to display at least one of content captured by the gimbal photographing device or a photographing parameter of the gimbal photographing device.

Hand-held gimbal and hand-held gimbal apparatus

An unmanned aerial vehicle includes a central body and a plurality of arms extendable from the central body. Each of the plurality of arms is configured to support one or more propulsion units. Each of the plurality of arms is configured to transform between (1) a flight configuration in which the arm is extending away from the central body and (2) a compact configuration in which the arm is folded against the central body. At least one of the plurality of arms is configured to rotate about a first rotational axis and at least a portion of the at least one of the plurality of arms is configured to rotate about a second rotational axis not parallel to the first rotational axis.

An unmanned aerial vehicle (UAV) includes a body and a gimbal camera. The body includes a housing including an inwardly recessed mounting groove with a notch on one side of the mounting groove, and a protective cover arranged at the housing and configured to open and cover the notch. The gimbal camera includes a mounting frame detachably connected to the housing via the mounting groove; a gimbal arranged at the mounting frame; and a camera arranged at the gimbal. In response to the gimbal camera and the housing being connected via the mounting frame, the gimbal camera is at least partially accommodated in the notch.

UAV and body thereof, and gimbal camera

An unmanned aerial vehicle (UAV) includes a vehicle body and a multi-ocular imaging assembly. The multi-ocular imaging assembly includes at least two imaging devices disposed in and fixed to the vehicle body.

Unmanned aerial vehicle and multi-ocular imaging system

A handle structure of a remote controller includes a left body including a left docking portion, a right body including a right docking portion configured to be docked with the left docking portion, and a connecting mechanism connecting the left docking portion and the right docking portion and configured to allow the left docking portion or the right docking portion to slide relatively to adjust an interval between an end of the left body and an end of the right body that are distal from each other. At least one controlling member is disposed at one of the left body or the right body.

Remote controller and handle structure thereof, and method for controlling a UAV

A dial assembly comprises a dial base, a rolling wheel, a dial handle, a reset elastic member, and a sensor. The dial base includes a first rotation channel and a second rotation channel. The rolling wheel is seated on the first rotation channel and rotatable along the first rotation channel. The dial handle is rotatably connected with the dial base and rotatable along the second rotation channel. The dial handle is connected with the rolling wheel and configured to rotate along with the rolling wheel. The reset elastic member is connected with the dial handle and configured to provide a restoring force to the dial handle. The sensor is connected with the dial handle and configured to obtain a rotation angle of the rolling wheel by sensing a rotation of the dial handle and convert the rotation angle into a control signal to transmit.

Dial assembly, remote control, and method for controlling an unmanned aerial vehicle

A flight control device includes a housing, a main control board provided in the housing, an inertial measurement unit provided in the housing and electrically connected to the main control board, and a power management unit provided at the housing and electrically connected to the main control board. The main control board, the inertial measurement unit, and the power management unit are fixedly connected to and integrated with the housing as a whole.

Flight control device and unmanned aerial vehicle having the same

An inertia measure unit (IMU) includes a main circuit board, and first and second weight blocks. A first surface of the first weight block contacts the main circuit board. The first weight block includes a recess formed on a second surface thereof opposite to the first surface, and an opening formed on a side surface thereof. The second weight block is coupled to the first weight block on the second surface to cover the recess. The first and second weight blocks jointly form an inner chamber in communication with the opening. The IMU further includes a circuit board disposed in the inner chamber, and a signal line coupled to an edge of the circuit board and extending out of the opening. The signal line bends over an outer surface of the first weight block or the second weight block to connect to the main circuit board.

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Shenzhen, China

Yin Tang