Sz Dji Osmo Technology Co., Ltd.

Sz Dji Technology Co., Ltd.

Chengyu Yin

Peng Wang

Peng Bin

Zihan Chen

Yongze Qi

A stabilizing device for stabilizing a payload includes a handle assembly, a payload stabilization assembly, and a constant force assembly. The handle assembly includes one or more grips. The payload stabilization assembly is configured to support a payload and permit the payload to rotate about at least one axis of rotation. The constant force assembly is operably connected to the handle assembly, is configured to support the payload stabilization assembly, and includes a parallelogram linkage. The parallelogram linkage includes four pivots and a resilient member obliquely arranged within the parallelogram linkage. The constant force assembly is configured to provide a force that equipoises a gravity force of the payload stabilization assembly with the payload in a vertical direction such that a net force of the payload stabilization assembly with the payload in the vertical direction is substantially zero.

Systems and methods for payload stabilization

A stabilizing device for stabilizing a payload includes a handle assembly, a payload stabilization assembly, and a constant force assembly. The handle assembly includes one or more grips configured to permit a user to support the entirety of the stabilizing device using the one or more grips. The payload stabilization assembly is configured to support the payload and permit the payload to rotate about at least one axis of rotation. The constant force assembly is operably connected to the handle assembly and supports the payload stabilization assembly. The constant force assembly is configured to provide a force that equipoises a gravity force of the payload stabilization assembly with the payload in a vertical direction such that a net force of the payload stabilization assembly with the payload in the vertical direction is substantially zero.

A stabilizing platform for stabilizing a payload includes a frame assembly, a plurality of actuators, and a plurality of electronic speed control (ESC) units. The frame assembly includes a plurality of frame components movable relative to one another and is configured to support the payload. The plurality of actuators are configured to permit the plurality of frame components to move relative to one another. Each of the plurality of ESC units is electrically coupled to a corresponding actuator of the plurality of actuators and is configured to control actuation of the corresponding actuator. At least one of the plurality of frame components includes a cavity, one of the plurality of actuators allowing the at least one of the frame components that includes the cavity to move relative to the carrier. At least two of the plurality of ESC units are received and sealed in the cavity.

Stabilizing platform and camera

A photographing apparatus includes a stabilizing mechanism and an imaging device arranged at the stabilizing mechanism. The stabilizing mechanism is configured to be detachably mounted at a portable electronic apparatus. The imaging device is configured to communicate with the portable electronic apparatus to allow the portable electronic apparatus to control the imaging device and to transmit captured images to the portable electronic apparatus.

Photographing apparatus, photographing device, and electronic device

A gimbal includes a photographing device, a support assembly carrying the photographing device, a connection assembly connected to the support assembly, and a plurality of shock absorption balls mounted at the connection assembly and configured to connect the gimbal to a vehicle body of an unmanned aerial vehicle (UAV). A geometric plane where geometric centers of the plurality of shock absorption balls are located is oblique relative to a horizontal direction.

Gimbal and unmanned aerial vehicle provided with gimbal

A stabilizing platform for stabilizing a payload includes a frame assembly, a plurality of actuators, and a plurality of electronic speed control (ESC) units. The frame assembly includes a plurality of frame components movable relative to one another and is configured to support the payload. The plurality of actuators are configured to permit the plurality of frame components to move relative to one another. The plurality of actuators include a first actuator that is configured to control movement of the payload about a first axis and a second actuator that is configured to control movement of the payload about a second axis. Each of the plurality of ESC units is electrically coupled to a corresponding actuator of the plurality of actuators and is configured to control actuation of the corresponding actuator. At least one of the plurality of ESC units is received in the payload.

Growing community of inventors

Shenzhen, China

Chengyu Yin