Abstract: 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.

Abstract: 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.

Abstract: Charging connector and charging apparatus are provided. The charging connector includes a partition plate including at least one charging interface provided on each side surface of two opposite side surfaces of the partition plate. The at least one charging interface is electrically coupled to a charging interface of a battery to charge the battery. Two lateral plates are respectively pivotally connected to the two opposite side surfaces of the partition plate and respectively rotatable with respect to the partition plate. Outer edges of the two lateral plates, which are away from a pivot joint portion, are configured to move away from or close to the partition plate to expose or cover the two opposite side surfaces of the partition plate to enable the charging connector to be in an open state or a folded state correspondingly.

Abstract: An inertia measure unit (IMU) includes a housing assembly, a weight block assembly, a circuit board, and a signal line. The housing assembly includes a cavity and a first opening in communication with the cavity. The weight block assembly is arranged in the cavity of the housing assembly. The weight block assembly includes a weight block forming an inner chamber and a second opening in communication with the inner chamber. An opening direction of the second opening is opposite to an opening direction of the first opening. The circuit board is disposed in the inner chamber. The signal line is coupled to an edge of the circuit board and sequentially extends out from the second opening and the first opening.

Abstract: 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.

Abstract: A remote control mobile apparatus includes a fuselage, a mounting bracket disposed at the fuselage. The mounting bracket is substantially polyhedron-shape and includes a receiving space. The remote control mobile apparatus further includes a power supply device received in the receiving space, and at least two functional circuits arranged separately on different outer surfaces of the mounting bracket. The at least two functional circuits are electrically coupled to each other and to the power supply device.

Abstract: 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.

Abstract: The present disclosure provides an integrated vision module component. The integrated vision module includes a bracket, a first vision module, and a second vision module. The first vision module and the second vision module are mounted on the bracket. The first vision module includes a first flexible circuit board, and a first image sensor and a second image sensor mounted on the first flexible circuit board. The second vision module includes a second flexible circuit board, and a third image sensor and a fourth image sensor mounted on the second flexible circuit board. The first image sensor and the third image sensor form a first binocular vision sensor. The second image sensor and the fourth image sensor form a second binocular vision sensor.

Abstract: An electrical connector is provided for both power and data transmission. The electrical connector comprises an electrical plug (100) having a plurality of pins (131˜138) and an electrical socket (200) having a plurality of passageways (220) which are arranged corresponding to the plurality of pins (131˜138). The pins (131˜138) of the plug comprise at least one signal pin (131, 136), two or more positive power pins (133, 134) and two or more negative power pins (132, 135). The pins (131˜138) of the plug can be disposed such that the positive power pins (133, 134) and the at least one signal pin (131, 136) are positioned on opposite sides of the negative power pins (132, 135).

Abstract: A sealed quick release structure includes a main enclosure provided with an accommodation member and a mounting surface, the mounting surface including an opening in communication with the accommodation member; a sealing cover accommodated in an accommodation groove and slidable in the accommodation groove to cover and seal the opening; and a fixing cover detachably disposed at the mounting surface and including the accommodation groove, the fixing cover being configured to slide relative to the mounting surface and the sealing cover between a lock position, at which the fixing cover is connected with the main enclosure and is pressed against the sealing cover; and an unlock position, at which the fixing cover is separated from the main enclosure to allow the sealing cover to be separated from the opening.

Abstract: An unmanned aerial vehicle includes a fuselage and a power supply assembly arranged at the fuselage. The power supply assembly includes a polyhedron mounting bracket arranged at the fuselage, a power supply device arranged at the fuselage, and at least two functional circuits arranged separately on different outer surfaces of the mounting bracket and electrically coupled to each other and to the power supply device.

Abstract: The present disclosure provides an unmanned aerial vehicle (UAV). The UAV includes a main body; an inertial measurement unit (IMU) disposed in the main body; a mounting bracket for fixing the IMU; and a circuit board fixedly disposed at the main body and integrated with a plurality of functional modules. The IMU is fixed on the circuit board through the mounting bracket.

Abstract: A connection structure includes an elastic member and a knob. The elastic member includes a bottom portion and an elastic piece extending from the bottom portion and including a free end not contacting the bottom portion. The free end includes a first protrusion extending outward along a radial direction of the elastic member and a second protrusion extending inward along the radial direction of the elastic member. The knob is configured to engage with the elastic member and includes a fitting slot formed at an inner wall of the knob. The fitting slot includes a first portion and a second portion in a circumferential direction of the knob for engaging with the first protrusion of the elastic piece. A depth of the first portion is smaller than a depth of the second portion.

Abstract: The present disclosure provides an integrated vision module component. The integrated vision module includes a bracket, a first vision module, and a second vision module. The first vision module and the second vision module are mounted on the bracket. The first vision module includes a first flexible circuit board, and a first image sensor and a second image sensor mounted on the first flexible circuit board. The second vision module includes a second flexible circuit board, and a third image sensor and a fourth image sensor mounted on the second flexible circuit board. The first image sensor and the third image sensor form a first binocular vision sensor. The second image sensor and the fourth image sensor form a second binocular vision sensor.

Abstract: The present disclosure provides an Unmanned Ariel Vehicle (UAV). The UAV includes a fuselage including a housing, a core control board disposed in the housing, and a battery, the housing including a battery compartment, and the battery being disposed in the battery compartment; an arm disposed on the fuselage; and a power assembly disposed on the arm. The core control board is disposed above the battery, a payload receiving cavity is disposed at a front lower end of the housing, a rear-bottom view component is disposed at a rear end of the housing and electrically connected to the core control board, and the battery compartment is disposed at a middle position under the housing.

Abstract: 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.

Abstract: 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.

Abstract: An unmanned aerial vehicle (UAV) includes a casing including a first end portion and a second end portion away from the first end portion. An accommodation chamber is formed at the second end portion. The UAV further includes a support plate arranged in the casing. The accommodation chamber is recessed relative to the support plate. The UAV also includes a circuit board assembly housed in the casing and a load provided at the first end portion of the casing. The circuit board assembly includes a circuit board connected to the support plate and an inertial measurement assembly provided at the circuit board and accommodated in the accommodation chamber.

Abstract: The present disclosure provides a motion sensor assembly applied to an unmanned vehicle. The motion sensor assembly includes a mounting bracket, a sensor assembly body, and a shock absorption mechanism disposed between the mounting bracket and the sensor assembly body. The sensor assembly body includes a protective casing and a sensor module disposed in the protective casing. The shock absorption mechanism including a plurality of elastic members, which are disposed between the mounting bracket and the protective casing for absorbing the shock of the sensor module in the protective casing.

Abstract: Protective cover for a gimbal camera of an unmanned aerial vehicle (UAV) and UAV are provided. The protective cover includes a stopper slidingly connected to the UAV and a locking member rotatably connected to the stopper. The locking member is configured to be locked to the UAV such that the stopper and the locking member are fixed to the UAV. The locking member is closed with the stopper to at least partially cover the gimbal camera.