Abstract: An electrical connector includes an insulative housing defining a top surface and a bottom surface opposite to each other and a plurality of electrical contacts received in the insulative housing. Each electrical contact is formed by stamping a metal plate and includes a contacting portion exposed to the top surface, a mounting portion extending out of the bottom surface and an elastic portion disposed between the contacting portion and the mounting portion and in the insulative housing, wherein the elastic portion includes a first elastic portion and a second elastic portion disposed on two opposite sides of the contacting portion.

Abstract: A composition including: (a) a silane derivative of the formula (I) in which R1, R2, R3 and R4, which may be the same or different, are selected from alkyl, acyl, alkyleneacyl, cycloalkyl, aryl and alkylenearyl, and/or a hydrolysis and/or condensation product of the silane derivative of the formula (I); (b) a silane derivative of the formula (II) R6R73?nSi(OR5)n??(II) in which R5 is an alkyl, acyl, alkyleneacyl, cycloalkyl, aryl or alkylenearyl group, R6 is an organic radical containing an epoxide group, R7 is an unsubstituted or substituted alkyl, cycloalkyl, aryl or alkylenearyl group, n is 2 or 3, and/or a hydrolysis and/or condensation product of the silane derivative of the formula (II); (c) a colloidal inorganic oxide, fluoride or oxyfluoride; (d) an epoxide compound having at least two epoxide groups, and (e) a catalyst system.

Abstract: A liquid volume transfer system includes: a liquid infusion device, including a first communication module, a first controller and a first flow rate detecting module; a liquid container, including a second communication module; and an unmanned aerial vehicle, including a third communication module, a third controller and a second flow rate detecting module.

Abstract: The present invention relates to pharmaceutical products comprising a combination of (i) a MET inhibitor and (ii) an EGFR inhibitor, or a pharmaceutically acceptable salt thereof, respectively, or a prodrug thereof, which are jointly active in the treatment of proliferative diseases, corresponding pharmaceutical formulations, uses, methods, processes, commercial packages and related invention embodiments.

Abstract: The embodiments of the disclosure discloses an aircraft spraying control device, a method thereof, and a spraying system, relating to the technical field of agricultural plant protection. The aircraft spraying control device comprises a micro-controller, a pump motor, and a nozzle motor; the micro-controller acquires the flight information of the aircraft and the preset pesticide spraying information of the aircraft, and acquires the target rotational speed n of the pump motor according to the flight information of the aircraft, the preset pesticide spraying information of the aircraft, and the pesticide discharging amount K per rotation of the pump motor so as to control the pump motor to rotate at the target rotational speed n of the pump motor so that the pump supplies pesticide to a nozzle. The micro-controller also controls the nozzle to spray.

Abstract: An electrical connector includes: an insulative housing defining a mating cavity upwardly communicating with an exterior through a top mating face thereof along an up-to-down direction, the mating cavity including a pair of side walls facing each other in a lengthwise direction perpendicular to the up-to-down direction; and a pair of flat power terminals retained in the two side walls of the mating cavity, respectively; wherein each flat power terminal includes a pair of elastic arms extending on two opposite sides thereof in the up-to-down direction, the pair of elastic arms of each flat power terminal are staggered in a transverse direction perpendicular to the up-to-down direction and the lengthwise direction.

Abstract: An unmanned aerial vehicle is provided and includes: an unmanned aerial vehicle body, including an airframe and an articles storing device; an arm, including at least two front arms symmetrically arranged with respect to a central axis of the airframe along a front-rear direction and at least two rear arms symmetrically arranged with respect to the central axis of the airframe; and a rotor-wing electric motor, including a front electric motor and a rear electric motor. A first end of the front arm is connected with a front end of the airframe, and a second end of the front arm is provided with the front electric motor to drive the unmanned aerial vehicle. A first end of the rear arm is connected with a rear end of the airframe, and a second end of the rear arm is provided with the rear electric motor to drive the unmanned aerial vehicle.

Abstract: An optical element has a substrate body made from transparent plastic and a coating having multiple layers. The coating includes a hard lacquer layer adjoining the substrate. The coating has a diffusivity ensuring the absorption of water molecules passing through the coating in the substrate and the release of water molecules from the substrate through the coating from an air atmosphere on that side of the coating facing away from the substrate with a flow density which, proceeding from the equilibrium state of the quantity of water molecules absorbed in the substrate in an air atmosphere at 23° C. and 50% relative humidity, brings the setting of the equilibrium state of the quantity of water molecules absorbed in the substrate in an air atmosphere at 40° C. and 95% relative humidity within an interval not more than 10 h longer than for setting this equilibrium under corresponding conditions with an identical uncoated substrate.

Abstract: An electrical connector includes an insulative housing defining a top surface and a bottom surface opposite to each other and a plurality of electrical contacts received in the insulative housing. Each electrical contact is formed by stamping a metal plate and includes a contacting portion exposed to the top surface, a mounting portion extending out of the bottom surface and an elastic portion disposed between the contacting portion and the mounting portion and in the insulative housing, wherein the elastic portion includes a first elastic portion and a second elastic portion disposed on two opposite sides of the contacting portion.

Abstract: A rotorcraft together with a heat dissipation structure for a motor are provided. The motor includes a body and a revolving shaft driven by the body, and the heat dissipation structure for the motor includes: a casing being a hollow structure having a top opening and an air inlet in a bottom portion, in which the body is disposed inside of the casing, and an air channel is formed between a circumferential edge of the body and an inner wall of the casing; a head cover connected to the revolving shaft of the motor synchronously and provided with a plurality of air flow picks on the lower surface thereof; and a mounting stand fixed to an upper surface of the head cover.

Abstract: A rotorcraft and an assembly and disassembly structure for a foot stand and an airframe of a rotorcraft are provided. The foot stand is disposed to a bottom of the airframe, the airframe has an accommodating groove, a top wall of the accommodating groove is provided with a hole, and a side wall of the accommodating groove is provided with a clamping slot, and the assembly and disassembly structure includes a fixing stand fixedly connected to the foot stand and accommodated in the accommodating groove; a plug pin movably mounted into the fixing stand, in which a portion of the plug pin passes through an upper surface of the fixing stand and forms an insertion end, and the insertion end matches the hole and is inserted into the hole; and an elastic component mounted in the fixing stand and connected to the plug pin.

Abstract: A rotorcraft and a connecting structure for an arm and an airframe of a rotorcraft are provided. The connecting structure includes: a fixed sleeve pipe configured to extend out from a circumferential edge of the airframe; an insertion head configured to be disposed to the first end of the arm and configured to be inserted into the fixed sleeve pipe; a lock sleeve configured to be fitted over the arm and having an insertion portion configured to be embedded into the insertion groove; and a lock nut configured to be fitted over the arm and configured for being in threaded connection with the fixed sleeve pipe.

Abstract: A rotorcraft and an automatic landing system and method thereof are provided in the present disclosure. The automatic landing system of the rotorcraft includes a controller, a laser emitter, a camera, an electronic governor and a motor configured to drive a propeller of the rotorcraft to rotate. The laser emitter and the camera are both locate in a bottom portion of an airframe of the rotorcraft. The laser emitter has two emission heads, laser beams emitted from the two emission heads respectively are symmetrical about a central axis, the central axis is perpendicular to a horizontal plane of a ground, and an angle between each laser beam and the central axis is an acute angle. Simply with an operation of the laser emitter, the camera and the controller, the flight speed and displacement of the rotorcraft can be controlled to realize automatic landing in the present disclosure.

Abstract: This invention provides compounds of Formula I: (Formula I should be inserted here) or a pharmaceutically acceptable salt thereof; pharmaceutical compositions comprising a compound of Formula I; and use of a compound of Formula I for treating specified cancers.

Abstract: This invention provides compounds of Formula (I) or a pharmaceutically acceptable salt thereof; pharmaceutical compositions comprising a compound of Formula (I); and use of a compound of Formula (I) for treating specified cancers.

Abstract: The present invention relates to pharmaceutical products comprising a combination of (i) a MET inhibitor and (ii) an EGFR inhibitor, or a pharmaceutically acceptable salt thereof, respectively, or a prodrug thereof, which are jointly active in the treatment of proliferative diseases, corresponding pharmaceutical formulations, uses, methods, processes commercial packages and related invention embodiments.

Abstract: This invention provides compounds of Formula I: (Formula I should be inserted here) or a pharmaceutically acceptable salt thereof; pharmaceutical compositions comprising a compound of Formula I; and use of a compound of Formula I for treating specified cancers.

Abstract: This invention provides compounds of Formula (I) or a pharmaceutically acceptable salt thereof; pharmaceutical compositions comprising a compound of Formula (I); and use of a compound of Formula (I) for treating specified cancers.

Abstract: An optical element has a substrate body made from transparent plastic and a coating having multiple layers. The coating includes a hard lacquer layer adjoining the substrate. The coating has a diffusivity ensuring the absorption of water molecules passing through the coating in the substrate and the release of water molecules from the substrate through the coating from an air atmosphere on that side of the coating facing away from the substrate with a flow density which, proceeding from the equilibrium state of the quantity of water molecules absorbed in the substrate in an air atmosphere at 23° C. and 50% relative humidity, brings the setting of the equilibrium state of the quantity of water molecules absorbed in the substrate in an air atmosphere at 40° C. and 95% relative humidity within an interval not more than 10 h longer than for setting this equilibrium under corresponding conditions with an identical uncoated substrate.

Abstract: An electrical connector assembly includes a receptacle connector and a plug connector. The receptacle connector includes a housing unit defining a mating cavity communicating with an exterior via an insertion opening at a front end thereof. A plurality of contact grooves are defined within the housing unit and extend along a front-to-rear direction. A plurality of contacts are arranged in the contact grooves in a side-by-side manner. A pair of elastic locking devices are disposed at opposite sides of the mating cavity and each has a pair of locking arms projecting into the mating cavity. The locking arms are formed within a common plane which is perpendicular to the front-to-rear direction. The plug connector is inserted into the mating cavity and clipped by the locking arms so as to realize a better retaining effect.