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228 results about "Decompression chamber" patented technology

Degasifier

InactiveUS20070240569A1Prevents deterioration in sealing propertySemi-permeable membranesDispersed particle filtrationDecompression chamberEngineering
A degasifier is provided in which the deterioration in sealing property (deterioration in airtightness) is prevented while sealing members to be placed between a container and covers that compose a decompression chamber can be omitted. A degasifier includes a decompression chamber provided with a container and covers, and a gas-permeable tube. The container is a tubular body extending along the central axis. The covers seal the openings of the ends of the tubular body. The gas-permeable tube is contained in the decompression chamber in such a manner that a liquid to be degassed that has entered from the outside of the decompression chamber flows therethrough and the liquid to be degassed that has flowed therethrough flows out of the decompression chamber. The inner circumference surfaces in the vicinities of the openings of the container each are provided with a first slope that is formed to be tilted at a predetermined angle θ with respect to the central axis and to extend away from the central axis toward the opening side of the container. A portion of each of the covers that is in contact with the container is provided with a second slope that is formed to be tilted at the angle θ with respect to the central axis and to extend to approach the central axis toward the inner side of the decompression chamber, with the openings being sealed. The openings are sealed with the container and the covers being joined to each other in the state where the first slopes and the second slopes are in contact with each other, respectively.
Owner:NITTO DENKO CORP

Electronic ceramic continuous sputtering coating equipment

The electronic ceramic continual sputter plating device comprises: a vacuum extraction device; and a body with five near vacuum chambers mutual connected insulating valves as the pre-pump chamber, front transition chamber, sputtering chamber with metal sputtering targets on mutual disposition, back transition chamber and the decompression chamber. Wherein, arranging a fitting friction piece transfer device and a piece frame can be convened to five chambers and outside by the transfer device; arranging a feeding table, an out-feeding table and a back mechanism all and said transfer device connected to a continual loop transfer line. This invention has large yield with low cost, strong bonding force and resistance to high temperature and corrosion.
Owner:ZHEJIANG UNIV

Damping type flow control forming process and die for aluminium-alloy rib-plate forging

The invention provides a damping type flow control forming process for an aluminium-alloy rib-plate forging. The process comprises two forming steps of pre-forging and finish-forging, a forming load is reduced through a decompression chamber during pre-forging, and the damping force is applied to a web portion of the forging during finish-forging, so that the web portion is prevented from plastic deformation, and deformation only occurs in rib portions. The invention also provides a die for implementing the method. A damper is arranged inside a concave die to apply the acting force to the web portion of the forging. According to the process and the die, metal flow is controlled through the damping force, so that metal distribution is adjusted reasonably during forming, and the forming load is reduced.
Owner:HUAZHONG UNIV OF SCI & TECH

Casting device, solution casting apparatus, and casting method

A casting drum is rotated around a shaft. A peripheral surface of the casting drum moves in an X direction. A dope is discharged through a casting die onto the peripheral surface such that a casting bead is formed so as to extend from a discharge port of the casting die to the peripheral surface. A decompression chamber decompresses an upstream side from the casting bead in a moving direction of the casting drum. The decompression chamber is provided with a sensor unit for detecting a width of the casting bead in a Y direction as width data. A control section shifts outer side seal plates in the Y direction based on the width data detected by the sensor unit such that the outer side seal plates are located in an upstream side from side ends of the casting bead in the X direction. Upon formation of a casting bead having a new width, the control section shifts the outer side seal plates in the Y direction based on the width data of the casting bead having the new width such that the outer side seal plates are located in the upstream side from the side ends of the casting bead having the new width in the X direction.
Owner:FUJIFILM CORP

Method and system for extracting and disposing of water vapor contained in the air of a space vehicle

A system for extracting including a cooled condenser apparatus in contact with the volume of pressurized air being dehumidified, the condensed water being transferred into collection areas by means of capillary attraction; an evaporation chamber in thermal contact with the condenser apparatus having an inlet connected to the collection areas by means of a first valve device and an outlet connected by means of a second valve device to a space wherein the pressure is lower than that of the volume of pressurized air; and a control device for controlling the valve devices in order to carry out a control cycle with a first phase for placing the evaporation chamber under negative pressure in relation to the volume of pressurized air, and a second phase for suctioning the condensed water in the collection areas towards the decompression chamber, until the pressure in the decompression chamber reaches a predefined threshold.
Owner:EUROPEAN SPACE AGENCY

Weight clump manufacturing method

The invention discloses a method for manufacturing a non-casting balancing weight, which comprises: firstly welding a plurality of metal plates into a shell, reserving a feeding port on the shell, filling core materials such as waste metal, gravel and waste residues into the shell, putting the balancing weight filled with the core materials into a decompression chamber for drying, pumping wet air in the decompression chamber by an extraction pump and simultaneously blowing dry air into the decompression chamber in the drying process, and sealing the feeding port after drying of the balancing weight to manufacture the balancing weight; or firstly sealing the feeding port before executing the drying step, and in the process of executing the drying step, utilizing the shell of the balancing weight to replace the decompression chamber, configuring an extract opening and an air inlet port on the shell, respectively connecting the extract opening and the air inlet port to the extraction pump and a dry air source, pumping the wet air in the shell of the balancing weight by the extraction pump while filling the dry air into the shell, and using less energy consumption to achieve better drying effect.
Owner:青岛地恩地材料科技有限公司

Aviation-simulated rapid decompression chamber

The invention belongs to the technical field of pressure chamber structures, and relates to a decompression chamber, in particular to an aviation-simulated rapid decompression chamber. The aviation-simulated rapid decompression chamber is characterized by comprising a main chamber, wherein the main chamber is connected with an auxiliary chamber by a quick-open chamber door, and is an environmental experiment chamber used for simulating and creating environments in different height and at different temperatures, and the auxiliary chamber is a rapid decompression chamber used for simulating and creating an environment in a cabin or a cockpit. The aviation-simulated rapid decompression chamber is provided with a one-chamber and two-room structure, so that the required pressure and temperature environments are achieved by adjusting pressure and temperature adjustment equipment in the chamber; when rapid decompression is required to be simulated, the quick-open door is controlled by controlling and operating an electric permanent magnet between the two chambers through an electric signal; a course of environment change when the cabin is damaged and a cockpit drops during a high-altitude flight of an airplane is simulated truly; and experimental researches such as various aeromedical researches, equipment experiment testing and the like are carried out during the course, so that the purposes of reducing or avoiding casualties and equipment damages are achieved.
Owner:烟台宏远氧业股份有限公司
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