Patent application number | Description | Published |
20130320606 | WAVE SOLDERING CARRIER - A wave soldering carrier includes a base plate and a fixing member positioned on the base plate. The base plate defines a receiving recess and a number of through holes communicating with the receiving recess. The receiving recess receives a circuit board. The through holes are arranged and shaped corresponding to a number of electronic components on the circuit board. The fixing member includes a shaft including a fixing shaft fixed to the base plate and a restricting shaft extending from an end of the fixing shaft. A diameter of the restricting shaft is greater than that of the fixing shaft, thereby forming a step. The fixing member further includes a rotatable member rotatably connected to the fixing shaft and sandwiched between the shoulder and the base plate. The rotation member is rotatable to a preset position, where a distal end of the rotatable member firmly contacts the circuit board. | 12-05-2013 |
20140339235 | MATERIALS TRAY - A materials tray for holding materials for a production line includes a main body, a plurality of receiving grooves located on the main body, and a plurality of spacing portions. Each spacing portion is between two adjacent receiving grooves to separate materials respectively received in the two adjacent receiving grooves, and each spacing portion defines at least one gap creating intercommunication between the two adjacent receiving grooves to ease extraction of the materials by the user. | 11-20-2014 |
20140353895 | CARRYING APPARATUS - A carrying apparatus is fixed on a base for carrying a printed circuit board (PCB). The carrying apparatus comprises a carrying mechanism for receiving the PCB and a positioning mechanism mounted on the base. The carrying mechanism is received in the positioning mechanism and is capable of detaching from the positioning mechanism. | 12-04-2014 |
20140374541 | AIRCRAFT CONTROL APPARATUS, CONTROL SYSTEM AND CONTROL METHOD - An aircraft control apparatus, control system, and control method are disclosed. A control apparatus includes: a first control rod configured to have a movement in a first movement direction controlling a motion of an aircraft in a first motion direction, wherein after an external force on the first control rod in the first movement direction is removed, the first control rod automatically returns to a preset position in the first movement direction; wherein the preset position which the first control rod automatically returns to corresponds to the aircraft in the first motion direction maintaining a state of flight; wherein the maintaining state of flight depends on control signals received by the aircraft generated resulting from changes in the external force applied to the control rod in the first movement direction and state signals measured by state measurement sensors carried by the aircraft. | 12-25-2014 |
Patent application number | Description | Published |
20140131510 | UNMANNED AERIAL VEHICLE AND OPERATIONS THEREOF - The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors. | 05-15-2014 |
20140263823 | TRANSFORMABLE AERIAL VEHICLE - Systems, devices, and methods for a transformable aerial vehicle are provided. In one aspect, a transformable aerial vehicle includes: a central body and at least two transformable frames assemblies respectively disposed on the central body, each of the at least two transformable frame assemblies having a proximal portion pivotally coupled to the central body and a distal portion; an actuation assembly mounted on the central body and configured to pivot the at least two frame assemblies to a plurality of different vertical angles relative to the central body; and a plurality of propulsion units mounted on the at least two transformable frame assemblies and operable to move the transformable aerial vehicle. | 09-18-2014 |
20140356174 | SELF-TIGHTENING ROTOR - Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force. | 12-04-2014 |
20150060606 | UNMANNED AERIAL VEHICLE AND OPERATIONS THEREOF - The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors. | 03-05-2015 |
20150069174 | UNMANNED AERIAL VEHICLE AND OPERATIONS THEREOF - The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors. | 03-12-2015 |