Patents
Literature
Hiro is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Hiro

70results about How to "Suppress eddy current" patented technology

In-pile flow distribution device of reactor of nuclear power station

The invention discloses an in-pile flow distribution device of a reactor of a nuclear power station. The device is used for distributing flow of a reactor core coolant; the flow distribution device comprises a lower reactor core support plate, a surrounding basket-shaped structure and vertical columns, wherein the surrounding basket-shaped structure is fixed below the lower reactor core support plate and comprises a porous surrounding basket and an eddy-current confinement plate positioned at the bottom of the porous surrounding basket; a plurality of flowing holes are respectively formed in the porous surrounding basket and the eddy-current confinement plate; the vertical plates are vertically arranged between the eddy-current confinement plate and the lower reactor core support plate. The in-pile flow distribution device of the reactor of the nuclear power station is relatively simple in structure, and by stirring and mixing the coolant through the eddy-current confinement plate and the vertical columns, eddy-current of a lower chamber is effectively inhibited, and the structure of the lower chamber is prevented from vortex shedding. The coolant is subjected to twice flow distribution through the surrounding basket-shaped structure and the lower reactor core support plate, so that the distribution effect is better, and the flow distribution uniformity in a reactor core fuel component is better.
Owner:中广核工程有限公司 +1

Suspended spraying type metal organic chemical vapor deposition (MOCVD) reactor

The invention relates to a suspended spraying type metal organic chemical vapor deposition (MOCVD) reactor, which can be used for the epitaxial growth of light emitting diodes (LEDs) on a large scale. The suspended spraying type MOCVD reactor comprises a nozzle, a base, a cover plate, flow diversion holes and a reaction zone, wherein the nozzle is arranged in the center of the base and comprises an upper nozzle and a lower nozzle; the lower nozzle is positioned on the lower part of the upper nozzle; the upper nozzle and the lower nozzle are provided with two radial channels respectively; the base comprise a large graphite disk; small graphite disks are arranged in the large graphite disk along the circumferential direction; wafer substrates are arranged in each small graphite disk along the circumferential direction; the bottom of the large graphite disk is provided with a revolution driving mechanism; the bottom of each small graphite disk is provided with an autorotation drive mechanism; and the flow diversion holes are formed on the inner wall of the cavity of the reaction zone along the circumferential direction. The suspended spraying type MOCVD reactor can improve the deposition uniformity of thin films and the utilization rate of source materials, prolong the service life of the graphite disks of the base, improve the introduction of source gas and the distribution of carrier gas, optimize the designs of the size of the reactor and the curve surface of the cover plate and prevent the generation of eddy current.
Owner:48TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP

Gas spraying head and deposition device

The invention discloses a gas spraying head and a deposition device. The gas spraying head comprises a cooling plate with an upper surface and a lower surface opposite to each other; the cooling plate includes a center area and a peripheral area; the peripheral area includes multiple cooling pipe areas; each cooling pipe area has a set of cooling pipes; one set of cooling pipes includes multiple arc pipe sections arranged from the center to the edge of the cooling plate in parallel; all the arc pipe sections are positioned on concentric circles with different radius; multiple connecting parts are arranged between the multiple arc pipe sections and the adjacent arc pipe sections; multiple ventilation grooves are formed among the connecting parts; the ventilation grooves penetrate through the cooling plate along the side walls of the adjacent arc pipe sections, and are positioned on the concentric circles with different radius; in one cooling pipe area, one set of ventilation grooves formed by the multiple ventilation grooves on the concentric circles with the same radius are communicated to a first gas output port and a second gas output port along with radius increment; and the center area includes multiple intake ports penetrating through the cooling plate. The gas spraying head can improve the film forming quality.
Owner:ADVANCED MICRO FAB EQUIP INC CHINA

Wing structure for wig vehicle

The present invention relates to a wing structure for a WIG vehicle. More specifically, the wing structure of a WIG vehicle comprises left and right side main wings, left and right downward wings, and a rudder unit. The left and right main wings protrude out from the central portions of left and right sides of the WIG vehicle. The panel of the main wing is flat and tapers successively toward the lateral edge, whereof the cross-section is airfoil-shaped and has the shape of a tadpole. The panel shaped left and right downward wings are connected with both ends of the left and right main wings without a joint and are formed heading downward to suppress vortex and guidance drag generated in both ends of the main wings. The rudder units are mounted on the rear surface of the left and right downward panels with a slight gap in order to compensate asymmetry between left and right lateral ends caused by movement under control of the fuselage driving unit of the WIG vehicle and to turn the fuselage left or right. Therefore, the wing structure of the WIG vehicle is capable of minimizing vortex and guidance drag generated in both ends of the left and right main wings by maximizing ground effect. Additionally, the wing structure has advantages for absorbing impact from the fuselage when taking off and landing and stabilizing horizontal disturbance of the fuselage because the left and right downward wings occupy much more volume than a winglet.
Owner:WING SHIP TECH CO LTD

Structure for suppressing flow vibration of instrumentation guide tube

A structure for suppressing flow vibration of an instrumentation guide tube, the structure being constructed such that an upper hole (37A) and a lower hole (37B) are formed at two upper and lower positions in a side face of the guide tube (27) and that a thimble tube (22) is pressed against the inner peripheral surface of the guide tube (27) by a difference between pressures of a cooling material in the inside and outside of the upper and lower hole (37A, 37B). Further, the structure desirably has an upper pressure regulation hole and lower pressure regulation hole formed at two upper and lower positions in a side face of an upper reactor core support column (21). The upper and lower pressure regulation holes allow a cooling material, having flown from the upper end of the guide tube into the guide tube, to flow from the inside to the outside of the guide tube through a gap between the thimble tube and the upper hole, flow from the inside to the outside of the upper reactor core support column through the upper pressure regulating hole, flow from the lower end of the guide tube into the guide tube, flow from the inside to the outside of the guide tube through a gap between the thimble tube and the lower hole, and then flow from the inside to the outside of the upper core reactor support column through the lower pressure regulating hole.
Owner:MITSUBISHI HEAVY IND LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products