Patent application number | Description | Published |
20140095638 | METHOD OF SUPPORTING THIRD-PARTY APPLICATIONS IN AN INSTANT MESSAGING SYSTEM AND A SYSTEM USING THE SAME - A mobile terminal system for providing instant messaging to a third-party application includes a mobile terminal having one or more processors and memory for storing one or more programs, wherein the one or more programs, when executed by the one or more processors, cause the mobile terminal to perform the instructions of acquiring an application ID (appid) and a software development kit (SDK) from an instant messaging open platform by the third-party application; registering the third-party application at the instant messaging open platform using the acquired appid and SDK when the third-party application initiates; providing an open application programming interface (API) to the third-party application via the instant messaging open platform; and transmitting information between the instant messaging open platform and the third-party application via the open API. | 04-03-2014 |
20140117149 | Tetra-Propeller Aircraft - Described herein is a vertical take-off and landing aircraft comprising: an upper enclosure comprising a first upper arm and a second upper arm; a lower enclosure comprising a first lower arm and a second lower arm; wherein the first upper arm and the first lower arm comprise a first upper buckle and a first lower buckle, respectively; wherein the second upper arm and the second lower arm comprise a second upper buckle and a second lower buckle, respectively; wherein the first upper buckle engages the first lower buckle and the second upper buckle engages the second lower buckle, thereby securing the upper enclosure to the lower enclosure. | 05-01-2014 |
20150108862 | Aircraft Vehicle and a Fixing Sleeve - This disclosure provides an aircraft vehicle, which comprises a circuit board, and at least one power component mounted on said circuit board. The at least one power component comprises a rotor, a drive unit and a fixing sleeve. Said drive unit is electrically connected to said circuit board and drives the rotor to rotate. Said fixing sleeve comprises a receiving space with an opening at a top. Said fixing sleeve comprises at least one first stopping piece and at least one second stopping piece projected on an outer surface of the fixing sleeve. Said drive unit is accommodated in the receiving space and is secured in the fixing sleeve. Said circuit board comprises at least one positioning hole corresponding to the power component. The fixing sleeve is configured to pass through the positioning hole so that the circuit board is retained between the first stopping piece and the second stopping piece. This disclosure also provides a fixing sleeve. Thus, when the aircraft vehicle falls or collides with another object, the fixing sleeve ensures that the drive unit does not separate from the circuit board, therefore enhancing the performance of the aircraft vehicle. | 04-23-2015 |