32results about How to "Meet the working temperature requirements" patented technology

The invention discloses a circulation cooling device in the water jacket of a motor bearing, which comprises two parts, namely, a water jacket part and a flange part, wherein the water jacket part is composed of an outer water-jacket ring, an inner water-jacket ring, a water baffle, a water inlet pipe and a water outlet pipe; the inner wall of the outer water-jacket ring or the outer wall of the inner water-jacket ring is provided with a circular groove, the outer water-jacket ring and the inner water-jacket ring are hermetically connected and surrounded to form the water jacket, the water baffle is transversely arranged in the water jacket, and the water inlet pipe and the water outlet pipe are respectively arranged at the two sides of the water baffle and communicated with the water jacket; the flange part comprises a large flange and a small flange, the straight gate end of the small flange is the connecting end of an external device, the straight gate end of the large flange is the connecting end of a motor bedplate, the other ends of the small flange and the large flange are connected together, and the coaxial inner holes of the small flange and the large flange are connected with the outer ring of the water jacket. The device of the invention can replace an end cover of a traditional motor, and by using the device, cooling fans for cooling bearing can not be used; and a water jacket at the periphery of a bearing chamber is added so as to carry out circulation cooling, so that the bearing temperature is always kept below 95 DEG C, thereby meeting the temperature requirements for the normal operation of the bearing, and guaranteeing the normal operations of motor.

The invention relates to shipborne access layer switch equipment and a shipborne access layer switch equipment assembling and reinforcing method. The shipborne access layer switch equipment is mainly composed of an aviation socket board, a housing, a mounting base and a switch module. The housing is made of aluminum alloy and is manufactured through processes of sandblast, nickel plating and anticorrosive paint applying. A mounting base is fixed at the back of the housing. A vibration damping pad is added between the inner bottom of the housing and the switch module. Furthermore vibration damping rings are arranged at a portion between the front surface of the switch module and the housing, a portion between the back surface of the switch and the housing, a portion between the left surface of the switch module and the housing and a portion between the right surface of the switch module and the housing. The aviation socket board is connected with the switch module through a cable. Discrete elements of the circuit board in the switch module are fixed through 1345 glue. Each connecting slit of the housing is provided with conductive lining material. The shipborne access layer switch equipment and the shipborne access layer switch equipment assembling and reinforcing method can effectively satisfy requirements for heat radiation performance, vibration resistance, impact resistance, water resistance, moisture resistance, dust resistance and electromagnetic compatibility of commercial network equipment in a shipborne environment, and furthermore satisfy a requirement for the access layer network equipment by the shipborne electronic information system.

The invention provides a laser vision cooling device, belongs to the technical field of laser vision, and solves the problem that the existing laser vision system is poor in cooling effect. The laser vision cooling device comprises a rectangular shell, a left baffle and a right baffle, wherein the left baffle is arranged on the left side of the shell; the right baffle is arranged on the right side of the shell; a laser clamp and a camera are arranged in the shell; a laser is arranged on the laser clamp; a water pump with a water inlet I and a water outlet I is arranged on the top of the shell; a water cooling grate with a water inlet II and a water outlet II is arranged in the front of the shell; the water inlet II is communicated with the water outlet I; a metal plate I which is used for separating the laser from the camera and is internally provided with a cavity I is also arranged inside the shell; the metal plate I is attached to the camera and is provided with a water inlet III and a water outlet III which are respectively communicated with the cavity I; the water outlet II is communicated with the water inlet III; the water outlet III is communicated with the water inlet I. The laser vision cooling device has the advantages that the structure is compact, the cooling effect is good and the like.

The invention discloses a water-cooling heat dissipation module system of an engineering vehicle heating dissipation system, and belongs to the technical field of engineering vehicle heat dissipation. The water-cooling heat dissipation module system mainly comprises vehicle system heat sinks, a vehicle cooling liquid heat sink, a vehicle cooling liquid driving system and a cooling fan, wherein each vehicle system heat sink comprises an engine supercharged air heat sink, a vehicle hydraulic system hydraulic oil heat sink and a vehicle transmission system transmission oil heat sink, and vehicle cooling liquid sequentially flows through the vehicle system heat sinks; the water-cooling heat dissipation module system of the engineering vehicle also comprises an engine cooling liquid heat sink; the engine cooling liquid heat sink and the vehicle cooling liquid heat sink are arranged in a series connection manner; cooling air firstly flows through the vehicle cooling liquid heat sink and then flows through the engine cooling liquid heat sink so as to meet the working temperature requirements on supercharged air of an engine. The water-cooling heat dissipation module system has the advantages that the structural sizes of the vehicle system heat sinks are reduced, and the effective control on the temperature states of cold and hot fluids is easy to realize.

The invention discloses a high-temperature superconducting motor rotor low-temperature cooling system using liquid hydrogen, and relates to the field of low-temperature technology for superconducting applications. In the system, liquid hydrogen is stored in a liquid hydrogen storage tank to form a liquid section at the bottom and a gas section at the top. , the liquid hydrogen in the liquid section is transferred to the liquid hydrogen gasification chamber in the outer wall cavity of the high temperature superconducting motor rotor under the action of gravity through the liquid hydrogen delivery pipe for heat exchange to achieve cooling, and the hydrogen gas formed after the liquid hydrogen gasification passes through the hydrogen gas The gas section of the delivery pipeline that is transported back to the liquid hydrogen storage tank maintains the pressure in the liquid hydrogen storage tank, thus forming a closed cycle. The system uses liquid hydrogen as a low-temperature cooling medium, which can effectively maintain the temperature in the liquid hydrogen gasification chamber to meet the The working temperature of the superconducting magnet is required, and it is driven by gravity, so there is no need to use an additional circulation pump, which improves the reliability of the system.

The present invention relates to a high power non liquid cooling severe style constant temperature device, which consists of a thermal insulation unit, a semiconductor thermoelectric apparatus, a heat capacity block, a radiator, a temperature detector, a temperature control unit and a switching power. The thermal insulation unit consists of a thermal insulation box and thermal insulation filling materials, the thermal insulation filling materials is arranged in the thermal insulation box, the semiconductor thermoelectric apparatus, the heat capacity block and a temperature controlled optoelectronic device are arranged at the central part inside the thermal insulation box, and contacts with the thermal insulation filling materials; the temperature detector is directly pasted and covered on the outer surface of the optoelectronic device. The high power non liquid cooling severe style constant temperature device of the present invention has the advantages of novel concept, severe structure, large amount of refrigeration and heating, small size, convenient installation, no liquid refrigerator and compressor needed, no pollution, quick refrigeration speed, fine control performance, and easy industrialized batch production, etc; the present invention can be widely used for the temperature control of the apparatus needing constant temperature operation in the optoelectronic field, in particular to the site needing large amount of refrigeration and heating.