Sz Dji Technology Co., Ltd.

Di Ou

Liang Sun

Tao Peng

Xiaokai Guo

Zhongqian You

Fangming Ye

Bing Xue

Wentao Wang

Bin Jiang

Canlong Lin

Dayang Zheng

Feihu Yang

Hao Luo

Tao Deng

Hongshan Li

Wenlong Liang

Chaobing Chen

An aerial imaging system for transferring pictures captured from two or more imaging devices includes an aerial node and a ground node. The aerial node has two or more channels, each for acquiring at least one picture from a corresponding imaging device. The aerial node is configured to transfer the acquired pictures. The ground node is configured to present the acquired pictures from the two or more imaging devices.

Imaging system and method for unmanned vehicles

A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.

Rotor-wing assembly and unmanned aerial vehicle

A motor includes a bottom and a top opposite to the bottom. The bottom is a mounting side of the motor and the bottom is inclined relative to a rotation axis of the motor.

Motor and unmanned aerial vehicle

A battery mounting apparatus includes a mounting plate configured to hold a battery, a locking structure configured to detachably attach the battery to the mounting plate, and an ejection structure configured to eject the battery when the locking structure releases the battery, such that at least a portion of the battery is separated from the mounting plate.

Battery mounting apparatus, battery and unmanned aerial vehicle

An unmanned aerial vehicle (UAV) includes a central part, a frame assembly, and a propulsion assembly mounted to the frame assembly. The UAV also includes a servo mounted to the central part. The servo includes a driving apparatus, a control apparatus operably coupled with the driving apparatus, and a sensor configured to obtain operating parameters of the driving apparatus. The operating parameters include operating positions of the driving apparatus. The control apparatus is configured to control the driving apparatus to rotate to a predetermined position and stay at the predetermined position based on the operating positions of the driving apparatus obtained by the sensor.

Servo, control method, and unmanned aerial vehicle

An aerial imaging system for transferring pictures captured from a plurality of imaging devices includes an aerial node. The aerial node has a plurality of channels for acquiring the pictures from the imaging devices and is configured to transfer the pictures.

A signal line protection assembly of an aerial vehicle includes a foot stand and a protection sleeve. The foot stand includes a foot stand sleeve and a lower cover including an antenna compartment configured to receive an antenna of the aerial vehicle. The protection sleeve is configured to receive a signal line. At least a portion of the protection sleeve is received in the foot stand sleeve. The signal line includes a data line for the antenna.

Aerial vehicle and a signal line protection assembly thereof

The present disclosure discloses a battery housing apparatus. The apparatus includes a housing body and a battery locking mechanism. The housing body is configured with at least one battery compartment for housing a battery. The battery locking mechanism is disposed on the housing body and configured to indicate whether the battery is mounted in place during a process of mounting the battery in the battery compartment and to lock the battery in the battery compartment after the battery is mounted in place.

Battery housing apparatus and unmanned aerial vehicle

A propulsion system assembly includes a propeller and a motor configured to drive the propeller to rotate. The propeller includes one of a first body and a second body. The motor comprises the other one of the first body and the second body. The propulsion system assembly also includes a locking mechanism configured to detachably connecting the first body and the second body. The locking mechanism includes a locking member and a position limiting lock catch. The locking member is configured to lock the first body and the second body. The locking member includes locking parts located at at least two sides of the locking member. When the locking parts of the locking member rotate to a locking position, the position limiting lock catch is mounted to a side of the locking parts, to restrain the locking member from rotating relative to the first body.

Locking mechanism, propeller, motor, propulsion system assembly, and aircraft

An unmanned aerial vehicle (UAV) includes a fuselage, an electrical component, and an adapter arranged at the fuselage. The fuselage includes a battery compartment for accommodating a battery. The battery compartment includes an electrical connector for electrically coupling to the battery. The adapter is electrically coupled to the electrical connector and includes an access unit electrically coupled to the electrical connector and an adapting unit detachably coupled to the access unit. The adapting unit is configured to be electrically connected to the access unit when the adapting unit is coupled to the access unit. The adapting unit is electrically coupled to the electrical component through an adapting conductive wire to conduct power from the battery to the electrical component.

Unmanned aerial vehicle

A signal line protection assembly connecting to a propulsion system of an aerial vehicle includes a foot stand and a protection sleeve. The foot stand includes a foot stand sleeve including a bearing member and a receiving portion. The bearing member has a first side and a second side that is opposite to the first side. The first side is configured to bear the propulsion system, and the receiving portion is arranged at the second side. The protection sleeve is configured to receive a signal line. At least a portion of the protection sleeve is received in the receiving portion.

A transformable aerial vehicle includes a fuselage and a body frame. The fuselage includes a transmission mechanism including a leadscrew, at least two nuts threadedly connected to the leadscrew and connected to each other, and a nut adapter sleeved on one of the at least two nuts. The body frame includes a main support arm connected to the nut adapter, a crossbar connected to the main support arm, and a rotary power mechanism mounted on the crossbar.

Transformable aerial vehicle

A signal line protection assembly connecting to a propulsion system of an aerial vehicle includes a foot stand and a protection sleeve. The foot stand includes a foot stand sleeve including an electronic speed controller compartment arranged below a motor of the propulsion system and forming a closed space to receive an electronic speed controller of the aerial vehicle. The protection sleeve is configured to receive a power line for the electronic speed controller. At least a portion of the protection sleeve is received in the electronic speed controller compartment.

A signal line protection assembly for an aerial vehicle includes a foot stand and a protection sleeve configured to receive a signal line. The foot stand includes a foot stand sleeve. At least a portion of the protection sleeve is received in the foot stand sleeve.

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Shenzhen, China

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