Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: An unmanned aerial vehicle (UAV) includes a housing body and a battery locking mechanism disposed on the housing body. The housing body includes a battery compartment configured to receive a battery. The battery locking mechanism is configured to lock the battery in the battery compartment after the battery is mounted in place. The battery locking mechanism includes a locking assembly configured to be dislocated by the battery in a process of mounting the battery in the battery compartment and to be restored to lock the battery in the battery compartment after the battery is mounted in place, and an indicator assembly disposed on the housing body and configured to indicate whether the battery is mounted in place. The locking assembly includes a locking slider configured to tightly contact with the battery to lock the battery in a direction of a battery insertion.

Abstract: 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.

Abstract: A propulsion system assembly includes a propeller, a motor configured to drive the propeller to rotate, and a locking mechanism configured to detachably lock the propeller to the motor. The propeller includes one of a first body and a second body. The motor includes another one of the first body and the second body. The locking mechanism includes a coupling member including a femoral position groove, a fastener configured to fix the coupling member to the second body, and a locking member configured to lock the first body to the coupling member and the second body. A bottom portion of the first body that contacts the coupling member includes a protruding rib configured to fit with the femoral position groove to restrain the first body from rotating relative to the coupling member.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.

Abstract: 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.