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37results about How to "Extended thermal path" patented technology

Thermally enhanced wiring board with built-in heat sink and build-up circuitry

A thermally enhanced wiring board includes a heat sink, a stiffener and a build-up circuitry. The heat sink extends into an aperture of the stiffener and is thermally connected to the build-up circuitry. The build-up circuitry covers the heat sink and the stiffener and provides signal routing for the stiffener. The stiffener provides signal routing and mechanical support for the build-up circuitry.
Owner:BRIDGE SEMICON

Liquefied natural gas cylinder for vehicle and heavy-duty truck using liquefied natural gas cylinder for vehicle

The invention provides a liquefied natural gas cylinder for vehicle and a heavy-duty truck using the liquefied natural gas cylinder for vehicle. A cryopump is connected to a hydraulic control system, a split type inside sleeve comprises a flange, a thin walled tube and a pedestal, and a thermal insulation layer is provided on the outer wall of the thin walled tube as well as between the flange and the pedestal; an overlay welding is carried out for an outside sleeve and the inside sleeve after positioning through a corresponding through hole and a corresponding tapped hole, grooves are respectively formed at bottom parts of the inside sleeve and the outside sleeve, an inverted V-shaped part is combined after connection, and a welding is carried out; a valve seat in a front end supporting device is provided with multifunctional holes, a liquid inlet tube, a liquid outlet tube, a blow-down tube, a liquidometer tube or a safety valve tube are installed in the holes, an over-filling preventing head and an over-filling preventing cylindrical shell are equipped, and the bottom of the over-filling preventing head is provided with a small hole; a rear end supporting device is provided with a small hole on a supporting head, so that the internal space of the supporting head is communicated with the space of the cylinder; a rear end supporting shaft sleeve is made of epoxy glass fiber reinforced plastic; front and back heads of an inner container are provided with molecular sieves; a head of a housing is provided with palladium oxide. The cryopump can be stably installed on the liquefied natural gas cylinder, and heat leakage is effectively reduced.
Owner:SHAANXI AUTOMOBILE GROUP +1

Rapid vulcanization die for building lamination shock insulation rubber bearing

InactiveCN103786282AAvoid heat transfer barriersAchieving direct heat conductionVulcanizationEngineering
The invention discloses a rapid vulcanization die for a building lamination shock insulation rubber bearing. The rapid vulcanization die comprises an inner heating die with a heat conduction strip, an outer heating die with a heat conduction strip, an excessive glue groove, heat conduction strips, an upper heating template, a lower heating template, a positioning shaft, a positioning hole and a positioning shaft mounting groove, wherein the lower heating template is mounted on a support, the outer heating die with the heat conduction strip is arranged on the upper surface of the lower heating template, the inner heating die with the heat conduction strip is arranged in the center of the outer heating die with the heat conduction strip, the height of the outer heating die with the heat conduction strip is equal to that of the inner heating die with the heat conduction strip, and the upper heating template is arranged at the tops of the outer heating die with the heat conduction strip and the inner heating die with the heat conduction strip. The rapid vulcanization die fully utilizes the structural principle of vulcanization equipment and a vulcanization target to realize rapid and uniform vulcanization and efficient mounting, is applicable to vulcanization processing of various rubber bearings, such as a standard rubber bearing, a pencil lead rubber bearing, a high damping rubber bearing and a stacked rubber bearing, and is high in vulcanization efficiency and rapid and convenient to mount and maintain.
Owner:彭勃

Phase-change energy storage device

ActiveCN110274503ARealize the heat dissipation functionRealize heat preservation and energy storage functionHeat storage plantsHeat transfer modificationEngineeringPhase change
The invention discloses a phase-change energy storage device. The phase-change energy storage device comprises a heat conduction piston cavity, a phase-change unit, a heat conduction piston, a limiting ring, a first spring, a heat conduction cap and a heat sink; the piston cavity and the heat sink are oppositely arranged on the front surface and the rear surface, the heat sink is arranged in front of the piston cavity, the front end of the piston cavity is open, and the rear end of the piston cavity is sealed; the piston is in sliding fit in the piston cavity, and the piston is in dynamic sealing with the inner wall of the piston cavity; the phase-change unit is filled in a cavity defined by the end part of the rear end of the piston and the piston cavity, the limiting ring is fixedly connected with the inner wall of the front end of the piston cavity, and the first spring is arranged between the limiting ring and the piston; and the two ends of the first spring are respectively abutted against the limiting ring and the piston, the heat conduction cap is connected with the front end of the piston, the front end of the heat conduction cap penetrates out of the piston cavity, and the heat sink is arranged in front of the heat conduction cap. The phase-change energy storage device can dissipate heat generated by high-power equipment on the basis of keeping a small size, the problem of thermal control of the high-power equipment on a satellite is solved, and normal operation of the equipment is guaranteed.
Owner:BEIJING INST OF RADIO MEASUREMENT

Vacuum Break Mechanism in Superconducting Feeder System

The invention discloses a vacuum separation mechanism in a superconducting feeder line system, which comprises a vacuum separation body, various superconducting buses, low-temperature pipeline ports, a corrugated pipe, a protection device of the corrugated pipe and a cold screen connection hot stopper, wherein the vacuum separation body consists a peripheral U-shaped neck pipe and a center separation plate which realize the vacuum environment, the superconducting buses and the low-temperature pipeline ports pass through the center separation plate, the vacuum separation body realizes the vacuum separation at both sides, the superconducting buses and the low-temperature pipeline ports are combined with the corrugated pipe and the protection device of the corrugated pipe for realizing the vacuum sealing, then, the superconducting buses and the low-temperature pipelines can freely and axially extend and contract in the designed range, and the displacement requirement of the system in the work is met. A corrugated pipe protection sleeve protects the corrugated pipe so that the corrugated pipe can normally work under the condition of twisting and bending caused through electromagnetic force. In the aspect of heat insulation performance, the heat conducting path from the room temperature to the low temperature is lengthened through the U-shaped neck pipe, the temperature gradient on the vacuum separation is optimized through the hot stopper, and the heat load of 4.2K low-temperature components in the center position of the separation is possibly reduced.
Owner:HEFEI CAS ION MEDICAL & TECHNICAL DEVICES CO LTD

Enhancement heat conduction structure for high-power CCD of space optical remote sensor

The invention provides an enhancement heat conduction structure for a high-power CCD of a space optical remote sensor, and belongs to the technical field of space optical remoter sensors. The structure aims to solve the problems that in the prior art, heat conduction paths of a CCD are limited, the contact area between a fixing component at the back of the CCD and an installation substrate is small, thermal contact resistance is large and heat conduction efficiency is low. The enhancement heat conduction structure for the high-power CCD of the space optical remote sensor is an integral component composed of a device pressing plate, fixing ends and an enhancement heat conduction end. The fixing ends are located at the two ends of the device pressing plate, multiple narrow grooves are evenly machined between the enhancement heat conduction end and the device pressing plate, and the narrow grooves correspond to device pins at the back of the CCD in a one-to-one mode. On the basis that the CCD is fixed, the enhancement heat conduction end is designed, the heat conduction paths of the back of the device are effectively increased, the contact area between the CCD and the installation substrate is increased, heat conduction efficiency is improved, and the heat conduction requirement of the high-power CCD is met.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

High-power device heat dissipation device and method

The invention relates to a high-power device heat dissipation device and method, belongs to the technical field of aerospace, and particularly relates to the technical field of heat dissipation of high-power devices on aerospace vehicles. The device and the method are matched with the layout of a printed board, a graphite heat diffusion plate is processed, and a boss is arranged in a position, corresponding to a high-power device on the printed board, on the heat diffusion plate; the printed board on which the components are welded is fixed on the frame; the distance between the top surface ofthe high-power device and the mounting surface of the heat diffusion plate is measured, the height of a heat dissipation boss of the graphite heat diffusion plate is machined according to the measured distance, when the heat conduction pad is mounted, heat conduction grease is additionally coated according to the distribution condition of the heat conduction grease on the high-power device, and heat conduction paths are increased for a heat dissipation device with a bonding pad at the belly.
Owner:BEIJING RES INST OF TELEMETRY +1

Vacuum thermal insulating plate and refrigerator

The invention provides a vacuum thermal insulating plate and a refrigerator. The vacuum thermal insulating plate comprises a core material and a blocking membrane bag. A groove is formed in the side face of the core material. The core material is sealed in the blocking membrane bag. The blocking membrane bag is attached to the outer surface of the core material. The blocking membrane bag is attached to the inner wall face of the groove. By forming the groove in the side face of the vacuum thermal insulating plate, on one hand, the heat conduction route of the blocking membrane bag is lengthened, the heat conduction heat resistance of the blocking membrane bag is increased, and therefore the heat bridge effect in the vacuum thermal insulating plate is reduced, and the thermal insulating effect of the vacuum thermal insulating plate is improved; on the other hand, the contact area between the side face of the vacuum thermal insulating plate and a foamed layer is enlarged, the side face of the vacuum thermal insulating plate and the foamed layer are clamped, the adhesive force between the side face of the vacuum thermal insulating plate and the foamed layer is increased, the foamed layer and the vacuum thermal insulating plate are more firmly combined, and the disengagement phenomenon between the vacuum thermal insulating plate and the foamed layer is effectively avoided.
Owner:HEFEI HUALING CO LTD +1

Cooling Structure of Ultra-Precision Linear Motors

ActiveCN102882314BDo not change the ambient temperatureIncrease thrustCooling/ventillation arrangementSurface mountingCopper coil
The invention relates to a cooling structure for an ultraprecise linear motor and belongs to the technical field of linear motors. The cooling structure solves the problem of proneness to heat exchange with environment caused by high side temperature of two-side surface-mounted cooling structures of existing linear motors. The cooling structure comprises a winding supporting portion, a winding and a heat conductive portion, wherein the winding is fixed on the surface of the winding supporting portion, the heat conductive portion is arranged on the surface on the outer side and fixedly connected with the winding supporting portion, the heat conductive portion is a copper foil ring which fits the outer profile of the winding and is sleeved and fixed on the surface on the outer side of the winding, or the heat conductive portion is a copper foil heat conductive ring formed by arraying multiple copper foil sections in a dispersed manner, the copper coil heat conductive ring fits the outer profile of the winding, and each copper coil section is fixed on the surface on the outer side of the winding. The cooling structure for the ultraprecise linear motor is suitable for cooling of linear motors.
Owner:HARBIN INST OF TECH

Low-temperature thermal-isolation gas cylinder

The invention relates to a low-temperature thermal-insulation gas cylinder. The low-temperature thermal-insulation gas cylinder comprises a liner component, an upper bearing of a thermal bridge, a housing component, an upper flange component and a radial soft bearing (5). The low-temperature thermal-insulation gas cylinder disclosed by the invention is large in storage volume, good in thermal insulation performance and reliable in bearing.
Owner:JIANGSU SERLNG NEW ENERGY TECH COMPANY

High temperature pipeline heat insulation wall-penetrating structure and folding sleeve thereof

The invention discloses a high temperature pipeline heat insulation wall-penetrating structure and a folding sleeve thereof. The high temperature pipeline heat insulation wall-penetrating structure comprises the folding sleeve, a high temperature pipeline and a wall body; the folding sleeve is provided with a channel corresponding to the high temperature pipeline, and the extension direction of the channel is parallel to the axis direction of the folding sleeve; the side wall of the folding sleeve is formed by back-folding along the axis direction of the folding sleeve through a folding plate;the tail end, away from one side of the channel, of the folding plate extends outside in the radical direction of the folding sleeve and forms a connecting part used for connecting with the wall body; an installing hole is formed in the wall body corresponding to the folding sleeve, and the folding sleeve is arranged in the installing hole in a penetrating mode; and the high temperature pipelineis arranged in the channel in a penetrating mode, and thus the side wall of the folding sleeve is clamped between the high temperature pipeline and the wall body. According to the high temperature pipeline heat insulation wall-penetrating structure and the folding sleeve thereof, temperature of the wall body in connection with the pipeline is efficiently lowered, damage and thermal stress deformation caused by high temperature of the wall body is avoided, and high temperature damage on the other parts of the wall body is avoided. The folding sleeve has the displacement compensation ability dueto the back-folding structure, and vibration and sliding moving of the high temperature pipeline are efficiently prevented.
Owner:SHANGHAI MICROPOWERS

Anti-freeze starter electromagnetic switch with double-layer stationary contact

The present invention relates to an anti-freeze starter electromagnetic switch with a double-layer stationary contact, and the electromagnetic switch is characterized in that the central part of a movable contact piece is provided with a through hole; the lower end of a movable contact rod passes through the through hole of the movable contact piece, and a clamp spring is employed for limiting, so as to prevent the movable contact piece from being separated from the movable contact rod; the movable contact rod between an annular stopper boss and the movable contact piece is provided with a compression spring in a sleeved manner; The stationary contact consists of a screw rod and a double-layer stationary contact piece structure disposed at the top of the screw rod; the double-layer stationary contact piece structure consists of a lower stationary contact piece, an upper stationary contact piece and a spring piece between the lower stationary contact piece and the upper stationary contact piece; the spring piece is made of a bimetallic sheet which is deformed with temperature. The electromagnetic switch solves a problem of contact freezing fundamentally, is simple in structure, is low in cost, is small in size, is long in service life, is reliable for use, and is wide in application range.
Owner:JINZHOU HALLA ELECTRICAL EQUIP

CPT-atomic-magnetometer-based space glass air chamber heat insulation device

The invention discloses a CPT-atomic-magnetometer-based space glass air chamber thermal insulation device, which comprises a main body structure and glass air chamber thermal insulation sleeves clamped at two ends of a glass air chamber. The glass air chamber thermal insulation sleeves are assembled in the main body structure. According to the glass air chamber heat insulation device, the glass air chamber thermal insulation sleeves are made of polyimide materials with a small heat conduction coefficient and the outer spline, the inner fence and the S-shaped section are adopted and a e glass air chamber thermal insulation device is provided, so that when the glass air chamber is used in space, the temperature does not fluctuate greatly along with periodic changes of a track.
Owner:BEIJING INST OF AEROSPACE CONTROL DEVICES

A vacuum isolation device for ultra-low temperature fluid transmission pipeline

The invention discloses a vacuum isolation device for ultralow-temperature fluid transmission pipelines. The vacuum isolation device comprises a vacuum isolation flange connected with low-temperature pipelines in an ultralow-temperature area, a first low-temperature area and a second low-temperature area; each temperature area comprises a sleeve and a low-temperature pipeline extending out of the sleeve; the ultralow-temperature area is positioned at the center of the vacuum isolation flange, and the second low-temperature area is distributed on the outer periphery of the first low-temperature area which is distributed on the outer periphery of the ultralow-temperature area; the low-temperature pipeline in the ultralow-temperature area, the low-temperature pipeline in the first low-temperature area and the low-temperature pipeline in the second low-temperature area respectively penetrate the vacuum isolation flange, and one end of the sleeve of each temperature area is hermetically connected with the vacuum isolation flange; each sleeve is connected with the low-temperature pipeline in the last temperature area through a thermal stopper which is identical to the low-temperature pipeline in the last temperature area in temperature. The vacuum isolation device has the advantages that temperature gradient of vacuum isolation sleeves is optimized, and fluid consumption of the low-temperature areas is reduced.
Owner:INST OF HIGH ENERGY PHYSICS CHINESE ACAD OF SCI

Thermal bridge blocking structure for aircraft and preparation method thereof

The invention provides a thermal bridge blocking structure for an aircraft and a preparation method thereof. The thermal bridge blocking structure is located between a high-temperature structure and acold bearing structure of the aircraft. The thermal bridge blocking structure comprises a plurality of thermal insulation units. The multiple thermal insulation units are arranged in a stacked mode in the direction from the high-temperature structure to the cold bearing structure. Each thermal insulation unit comprises a first thermal insulation part and a plurality of second thermal insulation parts; the multiple second thermal insulation parts are arranged on one end face, in the stacking direction, of the first thermal insulation part at intervals and distributed in the circumferential direction of the end face, and projections of the multiple second thermal insulation parts of any two adjacent thermal insulation units in the stacking direction are arranged in a staggered mode so as toprolong the thermal conduction path between the high-temperature structure and the cold bearing structure. By means of the technical scheme, the technical problem that in the prior art, a thermal bridge blocking structure is poor in thermal insulation effect in a narrow space, and consequently the thermal insulation requirement of a high-speed aircraft cannot be met can be solved.
Owner:BEIJING AEROSPACE TECH INST

Low-temperature vacuum pipe connector

The invention relates to a low-temperature vacuum pipe connector comprising a liquid access pipe (4), an inner casing (7), a middle casing (6), and an outer casing (1). The head of the liquid access pipe (4) is connected with the bottom of a vacuum pipeline inner pipe (11) through a liquid access pipe connecting joint (9). The head of the outer casing (1) is connected with a vacuum pipeline outer pipe (12). A fiberglass insulating hoop (2) and a retainer ring (3) are connected to the bottom of the outer casing (1). The fiberglass insulating hoop (2) and the retainer ring (3) below the same are sequentially sleeved outside the liquid access pipe (4). The low-temperature vacuum pipe connector is effective in thermal insulation, the liquid access pipe is protected from external impact and distortion, cracks at a weld are avoided, and reliable quality is ensured; in addition, a connecting ring I, the middling casing, the inner casing and a connecting ring III are assembled and welded to form a thermal bridge component, a heat conducting path is added, heat conduction is effectively reduced, and delivery of low-temperature liquid can be insusceptible to external ambient temperature.
Owner:JIANGSU SERLNG NEW ENERGY TECH COMPANY

Contact type liquid nitrogen cryotherapy device

PendingCN110301972AAvoid doctor-patient fightsWon't hurtSurgical instruments for coolingTherapeutic DevicesNitrogen
The invention discloses a contact type liquid nitrogen cryotherapy device. The contact type liquid nitrogen cryotherapy device comprises an outer layer mechanism, an implementing mechanism and an inner layer mechanism. The outer layer mechanism is arranged on the outer side of the inner layer mechanism, and the implementing mechanism is connected with the inner layer mechanism; according to the size of an area need to be treated, cryoprobes of different sizes are selected and unnecessary damages to skin in a non-treatment area cannot be caused; one end of the cryoprobe is in contact with the skin and the other end of the cryoprobe is always in contact with liquid nitrogen so that the liquid nitrogen temperature is directly transmitted to the skin; and a temperature sensor with a patch is arranged on the cryoprobe to monitor the temperature of the cryoprobe in real time in the freezing process, so that it is ensured that the temperature of the cryoprobe is low enough and stable; in thefreezing process, the temperature is not judged by relying on the sense of a patient; nitrogen vaporized from liquid nitrogen or nitrogen which is not directly sprayed to the skin is collected by a pipeline and discharged separately, and the freezing safety is high; and the freezing temperature can be recorded in a storage of the device or even printed out by a printer provided with the device andsigned by both doctors and patients to avoid doctor-patient fights afterwards.
Owner:海尔生物医疗科技(成都)有限公司

A thermal insulation device for space glass air chamber based on cpt atomic magnetometer

The invention discloses a glass air chamber heat preservation device for space based on a CPT atomic magnetometer. The heat preservation device includes a main structure and a glass air chamber heat preservation sleeve, and the glass air chamber heat preservation sleeve is clamped at both ends of the glass air chamber. The glass air chamber insulation sleeve is assembled in the main structure. The present invention provides a glass air chamber insulation device for space by using polyimide material with a small thermal conductivity to make the glass air chamber insulation sleeve, and adopting the outer spline, inner "fence" and "S" section design at the same time. To ensure that when the glass air chamber is used in space, the temperature does not fluctuate greatly with the change of the orbital period.
Owner:BEIJING INST OF AEROSPACE CONTROL DEVICES

cryogenic storage device

The invention discloses a low-temperature storage device. The low-temperature storage device comprises an outer tank, shaft assemblies, an inner container and a driving assembly, wherein the inner container is arranged in the outer tank, and the driving assembly is arranged outside the outer tank. The inn container is connected and fixed with the outer tank. The center of the top of the outer tankand the center of the top of the inner container are provided with shaft holes for the shaft assemblies to penetrate. The shaft hole in the top of the outer tank is connected with the shaft hole in the top of the inner container through a corrugated pipe. First heat insulation assemblies for blocking airflow convection are arranged between the corrugated pipe and the shaft assemblies. The shaft assembly located inside the inner container is provided with an inner rotator for placing biological samples in different zones, and the shaft assembly located outside the outer tank is connected withthe driving assembly. Corresponding eccentric positions of the top of the outer tank and the top of the inner container are provided with object taking holes serving as biological sample taking and placing channels, and an openable heat preservation cover is arranged between the two object taking holes. The low-temperature storage device effectively reduces the loss of liquid nitrogen and has a better effect of storing the biological samples.
Owner:郭福军

A high-power device heat dissipation device and method

The invention relates to a heat dissipation device and method for high-power devices, belonging to the technical field of aerospace, in particular to the technical field of heat dissipation for high-power devices on aerospace vehicles. The present invention cooperates with the layout of the printed board, processes the graphite heat expansion plate, and makes a boss on the heat expansion plate corresponding to the position of the high-power device on the printed board; fixes the printed board with the welded components on the frame, and measures the high power The distance between the top surface of the device and the installation surface of the heat expansion plate is based on the measured distance, and the height of the heat dissipation boss of the graphite heat expansion plate is matched. Grease, for heat dissipation devices with pads on the abdomen, increase the heat conduction path.
Owner:BEIJING RES INST OF TELEMETRY +1

Thermal bridge blocking structure for aircraft and preparation method thereof

The invention provides a thermal bridge blocking structure for an aircraft and a preparation method thereof. The thermal bridge blocking structure is located between the high temperature structure and the cold load bearing structure of the aircraft. The thermal bridge blocking structure includes a plurality of heat insulation units, A plurality of heat insulation units are stacked along the direction from the high temperature structure to the cold bearing structure, any heat insulation unit includes a first heat insulation part and a plurality of second heat insulation parts, and a plurality of second heat insulation parts are arranged at intervals on the first The heat insulation parts are distributed along one end face of the stacking direction and along the circumferential direction of the end face, and the projections of multiple second heat insulation parts of any two adjacent heat insulation units on the stacking direction are staggered to extend the high temperature structure and the cold load-bearing structure heat conduction path between. Applying the technical solution of the present invention can solve the technical problem in the prior art that the thermal bridge blocking structure has a poor heat insulation effect in a narrow space and thus cannot meet the heat insulation requirements of high-speed aircraft.
Owner:BEIJING AEROSPACE TECH INST

Vehicle liquefied natural gas cylinders and the heavy truck

The invention provides a liquefied natural gas cylinder for vehicle and a heavy-duty truck using the liquefied natural gas cylinder for vehicle. A cryopump is connected to a hydraulic control system, a split type inside sleeve comprises a flange, a thin walled tube and a pedestal, and a thermal insulation layer is provided on the outer wall of the thin walled tube as well as between the flange and the pedestal; an overlay welding is carried out for an outside sleeve and the inside sleeve after positioning through a corresponding through hole and a corresponding tapped hole, grooves are respectively formed at bottom parts of the inside sleeve and the outside sleeve, an inverted V-shaped part is combined after connection, and a welding is carried out; a valve seat in a front end supporting device is provided with multifunctional holes, a liquid inlet tube, a liquid outlet tube, a blow-down tube, a liquidometer tube or a safety valve tube are installed in the holes, an over-filling preventing head and an over-filling preventing cylindrical shell are equipped, and the bottom of the over-filling preventing head is provided with a small hole; a rear end supporting device is provided with a small hole on a supporting head, so that the internal space of the supporting head is communicated with the space of the cylinder; a rear end supporting shaft sleeve is made of epoxy glass fiber reinforced plastic; front and back heads of an inner container are provided with molecular sieves; a head of a housing is provided with palladium oxide. The cryopump can be stably installed on the liquefied natural gas cylinder, and heat leakage is effectively reduced.
Owner:SHAANXI AUTOMOBILE GROUP +1

Components for service tower, service tower body and service tower

The present application discloses components for a service tower, a service tower body and a service tower. Components of the service tower include connection bases, connection pipes, return pipes, and cold head containers. The cold head secondary cylinder container is placed in the cold head container. The connecting seat has a through channel passing through the connecting seat, and at least one section of the connecting pipe is a flexible connecting pipe. The connecting pipe communicates with the through channel of the connecting seat and the return pipe communicates with the through channel of the connecting seat and the cold head secondary cylinder container in the cold head container, thus, the connecting seat, the The connecting pipe, the return pipe and the cold head container are integrated into one, so that the integrated service tower assembly can be connected to the cryogenic container through a connection port arranged on the top plate of the cryogenic container, thereby forming an overhead Compared with the way that the integrated service tower is often placed on the side of the superconducting magnet, the maximum liquid filling volume will be increased, the cooling effect will be improved, the structure is simple and the installation is also convenient.
Owner:NEUSOFT MEDICAL SYST CO LTD

Conical concentric-square-shaped labyrinth structure supporting structure

The invention provides a conical concentric-square-shaped labyrinth structure supporting structure which comprises an outer tank body of a cryogenic liquefaction container, an inner tank body of the cryogenic liquefaction container, conical concentric-square-shaped labyrinth supporting seat structures and heat insulation pads, and the conical concentric-square-shaped labyrinth supporting seat structures are embedded in the two ends of the outer tank body of the cryogenic liquefaction container and the two ends of the inner tank body of the cryogenic liquefaction container; the conical concentric-square-shaped labyrinth supporting seat structure further comprises a left conical concentric-square-shaped labyrinth connecting seat, a right conical concentric-square-shaped labyrinth connecting seat and threaded holes. The interiors of a left-side conical concentric-square-shaped labyrinth connecting base and a right-side conical concentric-square-shaped labyrinth connecting base are each of a double-vortex-line cavity structure. According to the structure, the heat exchange area is increased while the structural mechanical strength is guaranteed, the gas-solid heat exchange performance is far better than that of a hollow cavity, a low-temperature chamber is additionally arranged in the middle of the support, heat sink is added to the support, the temperature gradient of the support is reduced, the heat insulation performance of the support is improved through low-temperature gas precooling, and cold leakage is further reduced.
Owner:中太(苏州)氢能源科技有限公司

High-efficiency heat-insulation storage device and structure for space station

The invention discloses high-efficiency heat-insulation storage device and structure for a space station. The high-efficiency heat-insulation storage device for the space station is provided with at least one storage chamber, wherein a first side wall of the storage chamber comprises an inner wall layer, a support piece, a heat-insulation core layer and an outer wall layer arranged sequentially from the storage chamber to the outside environment; the inner wall layer and the outer wall layer form a sealed space; gas with a low heat conductivity coefficient is filled in the sealed space; and the support piece is of a horn-shaped structure and comprises a large-diameter end connected with the inner wall layer and a small-diameter end penetrating through the heat-insulation core layer so as to be abutted against the small-diameter end of the outer wall layer. The high-efficiency heat-insulation storage device for the space station provided by the invention has the excellent effects of small structure heat conduction, small gas heat conduction, small side wall dimension, large storage chamber utilization space and high heat insulation efficiency, and meets the low-temperature storage demand of the space station.
Owner:SHANGHAI MICROPOWERS

Heat dissipation system

A heat dissipation system is suitable for being thermally coupled to a heat source. The heat dissipation system comprises a centrifugal fan, a heat pipe, a radiator and a heat conduction frame set. The centrifugal fan comprises a shell and a fan blade. The shell is provided with a containing space, an air inlet and an air outlet, wherein the air inlet and the air outlet are communicated with the containing space. The fan blades are located in the containing space. The heat pipe is thermally coupled to the heat source. The radiator is located at the air outlet and thermally coupled to the heatpipe. The heat conduction frame set comprises a heat absorption frame and a heat dissipation frame. The heat absorption frame is used for assembling a heat source and thermally coupled with the heat source. The heat dissipation frame is arranged on a shell of the centrifugal fan and is partially located in the containing space. The heat dissipation frame is thermally coupled to the heat absorptionframe.
Owner:INVENTEC PUDONG TECH CORPOARTION +1

A phase change energy storage device

ActiveCN110274503BRealize the heat dissipation functionRealize heat preservation and energy storage functionHeat storage plantsHeat transfer modificationPower equipmentHeat sink
The invention discloses a phase-change energy storage device. The phase-change energy storage device comprises a heat conduction piston cavity, a phase-change unit, a heat conduction piston, a limiting ring, a first spring, a heat conduction cap and a heat sink; the piston cavity and the heat sink are oppositely arranged on the front surface and the rear surface, the heat sink is arranged in front of the piston cavity, the front end of the piston cavity is open, and the rear end of the piston cavity is sealed; the piston is in sliding fit in the piston cavity, and the piston is in dynamic sealing with the inner wall of the piston cavity; the phase-change unit is filled in a cavity defined by the end part of the rear end of the piston and the piston cavity, the limiting ring is fixedly connected with the inner wall of the front end of the piston cavity, and the first spring is arranged between the limiting ring and the piston; and the two ends of the first spring are respectively abutted against the limiting ring and the piston, the heat conduction cap is connected with the front end of the piston, the front end of the heat conduction cap penetrates out of the piston cavity, and the heat sink is arranged in front of the heat conduction cap. The phase-change energy storage device can dissipate heat generated by high-power equipment on the basis of keeping a small size, the problem of thermal control of the high-power equipment on a satellite is solved, and normal operation of the equipment is guaranteed.
Owner:BEIJING INST OF RADIO MEASUREMENT

Anti-icing starter solenoid switch with double-layer static contacts

The present invention relates to an anti-freeze starter electromagnetic switch with a double-layer stationary contact, and the electromagnetic switch is characterized in that the central part of a movable contact piece is provided with a through hole; the lower end of a movable contact rod passes through the through hole of the movable contact piece, and a clamp spring is employed for limiting, so as to prevent the movable contact piece from being separated from the movable contact rod; the movable contact rod between an annular stopper boss and the movable contact piece is provided with a compression spring in a sleeved manner; The stationary contact consists of a screw rod and a double-layer stationary contact piece structure disposed at the top of the screw rod; the double-layer stationary contact piece structure consists of a lower stationary contact piece, an upper stationary contact piece and a spring piece between the lower stationary contact piece and the upper stationary contact piece; the spring piece is made of a bimetallic sheet which is deformed with temperature. The electromagnetic switch solves a problem of contact freezing fundamentally, is simple in structure, is low in cost, is small in size, is long in service life, is reliable for use, and is wide in application range.
Owner:JINZHOU HALLA ELECTRICAL EQUIP

Vacuum insulation panels and refrigerators

The invention provides a vacuum thermal insulating plate and a refrigerator. The vacuum thermal insulating plate comprises a core material and a blocking membrane bag. A groove is formed in the side face of the core material. The core material is sealed in the blocking membrane bag. The blocking membrane bag is attached to the outer surface of the core material. The blocking membrane bag is attached to the inner wall face of the groove. By forming the groove in the side face of the vacuum thermal insulating plate, on one hand, the heat conduction route of the blocking membrane bag is lengthened, the heat conduction heat resistance of the blocking membrane bag is increased, and therefore the heat bridge effect in the vacuum thermal insulating plate is reduced, and the thermal insulating effect of the vacuum thermal insulating plate is improved; on the other hand, the contact area between the side face of the vacuum thermal insulating plate and a foamed layer is enlarged, the side face of the vacuum thermal insulating plate and the foamed layer are clamped, the adhesive force between the side face of the vacuum thermal insulating plate and the foamed layer is increased, the foamed layer and the vacuum thermal insulating plate are more firmly combined, and the disengagement phenomenon between the vacuum thermal insulating plate and the foamed layer is effectively avoided.
Owner:HEFEI HUALING CO LTD +1
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