Abstract: The invention provides novel FGFR inhibitors based on the pyridinylpyrimidine. The invention includes inhibitors with broad inhibitory activity against all FGFR isoforms, and inhibitors with selective inhibition against FGFR4. These novel pyridinylpyrimidine-based FGFR inhibitors, or their derivatives, have strong potential to be used to treat cancer.

Abstract: The invention provides a series of GMPS enzyme inhibitors. The invention includes potent GMPS inhibitors that specifically and covalently bind to GMPS, exhibit broad anti-cancer activity, block the infection efficiency of viruses, and have the potentials to suppress undesired immune responses. These novel inhibitors of GMPS, and their derivatives, have tremendous potentials to be used as therapeutic agents for the treatment of cancers, viral infection and immune disorders.

Abstract: The invention provides a series of GMPS enzyme inhibitors. The invention includes potent GMPS inhibitors that specifically and covalently bind to GMPS, exhibit broad anti-cancer activity, block the infection efficiency of viruses, and have the potentials to suppress undesired immune responses. These novel inhibitors of GMPS, and their derivatives, have tremendous potentials to be used as therapeutic agents for the treatment of cancers, viral infection and immune disorders.

Abstract: Various embodiments are directed to an indicia scanner. In an embodiment, a scanning operation is started in response to detecting an object within a field of view of indicia scanner. Starting the scanning operation comprises energizing an illumination source of the indicia scanner. The scanning operation is continued responsive to determining that the object is within a region of interest within the field of view. The scanning operation is stopped upon decoding of an indicia embodied by the object.

Abstract: An unmanned aerial vehicle includes a fuselage, a battery accommodation cavity, a battery pack, a battery circuit board, and a functional module. The battery accommodation cavity is disposed on the fuselage. The battery pack includes at least two battery blocks which are mounted inside the battery accommodation cavity. The battery circuit board is electrically connected to the battery blocks in the battery pack. The functional module is electrically connected to the battery circuit board, and the battery blocks in the battery pack supply power to the functional module via the battery circuit board at the same time.

Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

Abstract: The present invention relates to the field of air vehicle technologies and provides an unmanned aerial vehicle (UAV), including a vehicle body and arms connected to the vehicle body. The arm is hinged to the vehicle body by using a spherical hinge portion and may be folded or unfolded relative to the vehicle body. Through the forgoing manner, the arm is connected to the vehicle body of the UAV by using the spherical hinge. The arm can be folded and unfolded smoothly without interference, which conforms to known operation habits of users, so that after the entire UAV is folded, the structure becomes more compact and easier to carry. In addition, it can be effectively avoided that the UAV is damaged due to impact in the carrying process.

Abstract: Embodiments of the present invention relate to the technical field of aircrafts, and provide an undercarriage and an unmanned aerial vehicle (UAV) having the undercarriage. The undercarriage includes a power assembly and an undercarriage body. The power assembly includes a connecting member and a drive apparatus for driving the connecting member to reciprocate. The undercarriage body includes a plurality of hinged connecting rods, the plurality of hinged connecting rods constituting at least one parallelogram mechanism, and projections of at least two of the hinged connecting rods on a side face of the fuselage are staggered. The undercarriage body is connected to the connecting member, and when the connecting member reciprocates, the undercarriage body is driven to be folded or unfolded.

Abstract: The utility model relates to an unmanned aerial vehicle and an undercarriage thereof. The undercarriage includes: a power assembly disposed within a fuselage, the power assembly including a first connecting member and a drive apparatus configured to drive the first connecting member to perform a reciprocating linear motion; and an undercarriage body connected to the power assembly, the undercarriage body including a first connecting rod hinged on the first connecting member, and a second connecting rod of which one end is hinged on the power assembly and the other end is hinged on the first connecting rod. When the first connecting member performs the reciprocating linear motion, the undercarriage body is driven to be unfolded or folded into the fuselage. The utility model further relates to an unmanned aerial vehicle. For the foregoing unmanned aerial vehicle and the undercarriage thereof, the power assembly may be used to drive the undercarriage body to switch between an unfolded state and a folded state.

Abstract: The invention provides a series of GMPS enzyme inhibitors. The invention includes potent GMPS inhibitors that specifically and covalently bind to GMPS, exhibit broad anti-cancer activity, block the infection efficiency of viruses, and have the potentials to suppress undesired immune responses. These novel inhibitors of GMPS, and their derivatives, have tremendous potentials to be used as therapeutic agents for the treatment of cancers, viral infection and immune disorders.

Abstract: The invention provides novel FGFR inhibitors based on the pyridinylpyrimidine. The invention includes inhibitors with broad inhibitory activity against all FGFR isoforms, and inhibitors with selective inhibition against FGFR4. These novel pyridinylpyrimidine-based FGFR inhibitors, or their derivatives, have strong potential to be used to treat cancer.

Abstract: Embodiments of the present invention relate to the field of aircraft technologies, and provide an unmanned aerial vehicle including an unmanned aerial vehicle body and a landing gear. The landing gear is entirely accommodated in the unmanned aerial vehicle body when being in a folded state. When being folded, the landing gear in the present invention is entirely accommodated in the unmanned aerial vehicle body, and therefore neither causes unnecessary resistance in air nor blocks an aerial photographing field of view in an aerial photographing process of the unmanned aerial vehicle. In addition, when the unmanned aerial vehicle is not in use, the landing gear is accommodated in the unmanned aerial vehicle body, so that the unmanned aerial vehicle is very compact in structure and easy to accommodate and carry.

Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

Abstract: The present invention discloses an unmanned aerial vehicle, including: a fuselage; a battery accommodation cavity, disposed on the fuselage; a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity; a battery circuit board, electrically connected to the battery blocks in the battery pack; and a functional module, electrically connected to the battery circuit board, the battery blocks in the battery pack supplying power to the functional module via the battery circuit board at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

Abstract: The present invention relates to the field of aircrafts and provides a photographic assembly applied to an aircraft, where the aircraft includes a vehicle body. The photographic assembly includes: a vibration absorption member, a frame provided at the periphery of the vehicle body and connected to the vehicle body through a vibration absorption member, a gimbal connected to the frame and a camera connected to the gimbal. The frame of the photographic assembly in embodiments of the present invention can be mounted on unmanned aerial vehicle bodies of different specifications and the frame is sleeved over the vehicle body, so that the structure of the vehicle body can be designed compactly. The embodiments of the present invention further provide an unmanned aerial vehicle having the photographic assembly.

Abstract: The present invention relates to the technical field of aircrafts, and provides a gimbal, a photographing assembly and an unmanned aerial vehicle (UAV) that have the gimbal. The gimbal includes: a first rotating member and a second rotating member. The first rotating member includes a first drive apparatus, the first drive apparatus including a first rotating portion, and the second rotating member includes a second drive apparatus and a first connecting arm, the second drive apparatus including a second fixing portion and a second rotating portion that may rotate relative to the second fixing portion, the first connecting arm being fixedly connected between the first rotating portion and the second fixing portion, and the first connecting arm is integrally formed with the first rotating portion and the second fixing portion.

Abstract: The present invention relates to the field of air vehicle technologies and provides an arm, a power assembly and an unmanned aerial vehicle. The arm includes a principal arm and an auxiliary arm. The principal arm is mounted on the vehicle body and the principal arm can rotate relative to the vehicle body. One end of the auxiliary arm is connected to the principal arm. The auxiliary arm can rotate relative to the principal arm. In the foregoing manner, an unmanned aerial vehicle having the arm is compact in structure, small in volume and easy to carry after being folded.

Abstract: The present invention discloses an antenna and an unmanned aerial vehicle, where the antenna is applied to the unmanned aerial vehicle and the unmanned aerial vehicle includes a camera apparatus, the antenna including an antenna body and a bending part connected to the antenna body; and the bending part bends to a direction avoiding a field of view of the camera apparatus. Based on the foregoing technical solutions, in the embodiments of the present invention, it can be ensured that the antenna has a certain effective length to obtain a relatively strong radio signal, and avoids a shooting vision of the camera apparatus at the same time, so that images satisfying user demands are obtained.

Abstract: Embodiments of the present invention disclose an arm and an unmanned aerial vehicle (UAV). The arm is mounted on a movable object and is in contact with an outline of the movable object after being folded. The UAV includes a vehicle body, the arm connected to the vehicle body and a power device disposed on the arm. The arm is in contact with an outline of the vehicle body after being folded. According to the technical solutions, the arm provided in the embodiments of the present invention can be in contact with the outline of the movable object after being folded, so that the structure of the movable object to which the arm is applied is more compact.