A leakage prevention system including a cold plate is proposed in the current application. In one embodiment, a cold plate comprises an inlet port to receive cooling fluid from an external cooling source; an outlet port to return the cooling fluid back to the external cooling source; a sealing notch integrated with a sealing pad included in an outside layer of the cold plate; a nanoparticle channel disposed inside the outside layer; the nanoparticle channel is filled with a plurality of nanoparticles; a cooling area disposed inside the nanoparticle channel; the cooling area is to receive the cooling fluid from the inlet port, to exchange heat generated by an electronic device attached to the cold plate and carried by the fluid, and to return the cooling fluid via the outlet port; the plurality of nanoparticles in cooling fluid is used to detect a leakage of the cooling fluid.

A leakage prevention system including a cold plate is proposed in the current application. In one embodiment, a cold plate comprises an inlet port to receive cooling fluid from an external cooling source; an outlet port to return the cooling fluid back to the external cooling source; a sealing notch integrated with a sealing pad included in an outside layer of the cold plate; a nanoparticle channel disposed inside the outside layer; the nanoparticle channel is filled with a plurality of nanoparticles; a cooling area disposed inside the nanoparticle channel; the cooling area is to receive the cooling fluid from the inlet port, to exchange heat generated by an electronic device attached to the cold plate and carried by the fluid, and to return the cooling fluid via the outlet port; the plurality of nanoparticles in cooling fluid is used to detect a leakage of the cooling fluid.

A detection device for a turbine blade of an aircraft engine includes a machine table, a fixing frame, a dip coating mechanism, and a detection mechanism. A sliding cavity is formed in an upper end of the machine table, a support plate is slidably arranged in the sliding cavity, a side end of the support plate is rotatably connected to a chuck, the fixing frame is in an inverted “U” shape and is fixed on the upper end of the machine table, and a mounting barrel is rotatably arranged on the fixing frame. The dip coating mechanism and the detection mechanism are arranged on the machine table, such that wall-hanging sediments in an air film hole and a cooling channel will be exposed to a first photosensitive camera and a second photosensitive camera through fluorescent liquid, thus completing wall hanging and blockage detection of the blade synchronously.

A detection device for a turbine blade of an aircraft engine includes a machine table, a fixing frame, a dip coating mechanism, and a detection mechanism. A sliding cavity is formed in an upper end of the machine table, a support plate is slidably arranged in the sliding cavity, a side end of the support plate is rotatably connected to a chuck, the fixing frame is in an inverted “U” shape and is fixed on the upper end of the machine table, and a mounting barrel is rotatably arranged on the fixing frame. The dip coating mechanism and the detection mechanism are arranged on the machine table, such that wall-hanging sediments in an air film hole and a cooling channel will be exposed to a first photosensitive camera and a second photosensitive camera through fluorescent liquid, thus completing wall hanging and blockage detection of the blade synchronously.

A gas detection probe includes a shell and a detection element. The detection element includes a first element and a second element. The shell includes a first shell portion, a second shell portion, and a third shell portion. The second shell portion and the third shell portion are mated and formed on an outer periphery of the first shell portion. The shell has a first cavity and a second cavity. The first shell portion is in sealing engagement with the third shell portion. The second shell portion is provided with a guide hole portion communicated with the second cavity. The first element is accommodated in the first cavity. The second element is accommodated in the second cavity. The gas detection probe of the present disclosure is more beneficial to realize miniaturization. A manufacturing method of the gas detection probe is also disclosed.

A leak detection cart at least includes a cart body and a fixing clip arranged on the cart body. The cart body is configured to place a component to be leak-detected, and the fixing clip is configured to fix the cart body and the component to be leak-detected. The cart body is provided with a leak detection hole, and the leak detection hole is located in a projection region of the component to be leak-detected on the cart body, and is configured to implement a leak detection for the component to be leak-detected.

Systems, devices, and methods for an unmanned aerial vehicle (UAV); a trace gas sensor disposed on the UAV, where the gas sensor is configured to measure a gas point concentration; a wind sensor, where the wind sensor is configured to determine a discrete wind vector corresponding to the gas point concentration measurement; and where the discrete wind vector and gas point concentration measurement are acquired substantially concurrently and co-locally.

Embodiments of this application provide a detection label for an electronic device and an electronic device. The detection label includes a detection part and an adhesive layer, where the detection part is configured to detect whether liquid flows into an electronic device, and the adhesive layer is configured to connect the detection part to a housing of the electronic device. The detection part has a first surface, the first surface is a surface of a side facing towards the housing, the adhesive layer may be disposed on the first surface, and an area of the adhesive layer is less than an area of the first surface. In this way, a part of the first surface is not covered with the adhesive layer, and liquid can be in contact with the first surface, so that the detection part can perform detection in a plurality of directions simultaneously.

Embodiments of this application provide a detection label for an electronic device and an electronic device. The detection label includes a detection part and an adhesive layer, where the detection part is configured to detect whether liquid flows into an electronic device, and the adhesive layer is configured to connect the detection part to a housing of the electronic device. The detection part has a first surface, the first surface is a surface of a side facing towards the housing, the adhesive layer may be disposed on the first surface, and an area of the adhesive layer is less than an area of the first surface. In this way, a part of the first surface is not covered with the adhesive layer, and liquid can be in contact with the first surface, so that the detection part can perform detection in a plurality of directions simultaneously.

A seal inspection device includes: a first holder including a port surrounded by an inspection target, and a through hole connected to an outside-leak detection flow path; a second holder holding the inspection target between the first and second holders; an inspection-place sealing portion forming, into a closed space, a space where the inspection target is arranged, in cooperation with the first and second holders; a pressurization valve connecting the port to both a supply source of an inspection gas and an exhaust system; a detector for the inspection gas; a first measurement valve connecting the detector to the port; and a second measurement valve connecting the outside-leak detection flow path to the detector.