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CN108619868A - Air dehumidifier based on composite micro porous film and dehumidification device - Google Patents

Air dehumidifier based on composite micro porous film and dehumidification device Download PDF

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CN108619868A
CN108619868A CN201810832959.XA CN201810832959A CN108619868A CN 108619868 A CN108619868 A CN 108619868A CN 201810832959 A CN201810832959 A CN 201810832959A CN 108619868 A CN108619868 A CN 108619868A
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cold water
air
dehumidifier
water
temperature
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尚永红
王晶
陶东兴
吕剑锋
纪欣言
侯雅琴
袁卫星
方以锦
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Beijing Institute of Spacecraft Environment Engineering
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D53/00Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/26Drying gases or vapours
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D63/00Apparatus in general for separation processes using semi-permeable membranes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/46Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50Arrangements or adaptations of devices for control of environment or living conditions for temperature control

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Abstract

本发明公开了一种复合微孔膜除湿器,包括端头、法兰、纵长的中段管壳结构、支柱、接头、冷水出入口流道、空气出入口流道,两侧端头为固定膜丝的两端,分别通过接头和法兰与冷水出入口流道连通,使得低温冷水流入膜丝内部,管壳结构内容纳若干成簇的中空纤维复合微孔膜丝并与两侧端头密封连接,且其中心轴线上设置的支柱为支持结构,确保膜丝有足够的机械强度,低温冷水进入膜丝内部,并与管壳结构侧面上设置的空气出入口流道进出的高温高湿的空气换热后,送入密封舱内使用。本发明不仅同时降低湿空气的温度和湿度,而且在膜层微孔内的毛细力和水蒸汽分压差的共同主导下,实现水蒸汽向冷水的传输过程,可直接全部回收航天器舱内宝贵的水蒸汽。

The invention discloses a composite microporous membrane dehumidifier, which comprises a terminal head, a flange, a longitudinal middle section shell structure, a pillar, a joint, a cold water inlet and outlet flow channel, and an air inlet and outlet flow channel, and the ends on both sides are fixed membrane wires The two ends of the tube are respectively connected with the cold water inlet and outlet channels through the joints and flanges, so that the low-temperature cold water flows into the inside of the membrane, and the shell structure contains a number of clustered hollow fiber composite microporous membranes and is sealed with the ends on both sides. And the pillars set on the central axis are supporting structures to ensure that the membrane filaments have sufficient mechanical strength, low-temperature cold water enters the interior of the membrane filaments, and exchanges heat with the high-temperature and high-humidity air that enters and exits the air inlet and outlet channels set on the side of the shell structure After that, it is sent into the airtight cabin for use. The invention not only reduces the temperature and humidity of the humid air at the same time, but also realizes the transmission process of water vapor to the cold water under the joint leadership of the capillary force in the micropores of the film layer and the water vapor partial pressure difference, and can directly recycle all the water vapor in the spacecraft cabin precious water vapor.

Description

基于复合微孔膜的空气除湿器及除湿装置Air dehumidifier and dehumidification device based on composite microporous membrane

技术领域technical field

本发明属于航天器环境控制领域,具体涉及一种航天器基于复合微孔膜的空气除湿部件与相应系统,解决航天器舱内空气的湿度进行精确控制问题,降低空气除湿的功耗、提高可靠性。The invention belongs to the field of spacecraft environment control, and specifically relates to an air dehumidification component and a corresponding system based on a composite microporous membrane of a spacecraft, which solves the problem of precise control of the humidity of the air in the spacecraft cabin, reduces power consumption of air dehumidification, and improves reliability. sex.

背景技术Background technique

湿度控制技术是载人航天器环控生保技术的重要方面,其基本任务是为航天员提供舒适的湿度环境。航天员舒适环境相对湿度要求为28%-65%,当相对湿度低于25%或高于80%时,航天员在轨工作时间不能超过12h。除此以外,由于载人航天器舱内空间狭小,电子设备众多,航天员因工作和生理呼吸等活动不断产生水蒸汽,当相对湿度偏高时,可能在舱内设备的低温表面出现水蒸汽冷凝,产生结露,可能会造成电子设备短路,电化学腐蚀等后果,甚至危及航天器的安全;偏高的相对湿度,可能加速微生物的生长和繁殖,增大航天员感染疾病的几率。而相对湿度偏低又可能引起静电现象。因此对航天器舱内空气的湿度进行精确控制,并尽量降低空气除湿的功耗、提高可靠性,已成为航天器环境控制领域一项重要的技术。Humidity control technology is an important aspect of manned spacecraft environmental control and life protection technology, and its basic task is to provide astronauts with a comfortable humidity environment. The relative humidity requirement for astronauts' comfortable environment is 28%-65%. When the relative humidity is lower than 25% or higher than 80%, the working time of astronauts in orbit cannot exceed 12 hours. In addition, due to the small space in the cabin of the manned spacecraft and the large number of electronic equipment, the astronauts continue to produce water vapor due to work and physiological breathing activities. When the relative humidity is high, water vapor may appear on the low-temperature surface of the equipment in the cabin. Condensation and condensation may cause short circuit of electronic equipment, electrochemical corrosion and other consequences, and even endanger the safety of spacecraft; high relative humidity may accelerate the growth and reproduction of microorganisms, increasing the probability of astronauts being infected with diseases. The low relative humidity may cause static electricity. Therefore, it has become an important technology in the field of spacecraft environmental control to accurately control the humidity of the air in the spacecraft cabin, reduce the power consumption of air dehumidification and improve the reliability as much as possible.

航天器湿度控制技术从最早的干燥剂、吸湿剂和吸湿材料,发展到现已广泛用于载人飞船、航天飞机和空间站的冷凝干燥器。根据活动量不同,航天员产湿量在50-155g/h,平均日产湿量1800g。干燥剂、吸湿剂和吸湿材料等被动湿度控制方法已不能满足载人航天器的发展需要。以冷凝干燥器为代表的主动湿度控制技术发展较多,在各国载人航天器上得到广泛应用,技术成熟,但在微重力下的空气除湿方法,均是将湿空气的冷凝和气水分离过程分开进行,需要消耗较多的电功、且有运动机械,冷凝水无法回收利用。Spacecraft humidity control technology has developed from the earliest desiccants, hygroscopic agents and hygroscopic materials to condensation dryers that are widely used in manned spacecraft, space shuttles and space stations. Depending on the amount of activity, the moisture production of astronauts is 50-155g/h, and the average daily moisture production is 1800g. Passive humidity control methods such as desiccants, hygroscopic agents, and hygroscopic materials can no longer meet the development needs of manned spacecraft. The active humidity control technology represented by condensing dryers has developed a lot and has been widely used in manned spacecraft in various countries. The technology is mature, but the air dehumidification method under microgravity is the process of condensation of humid air and separation of gas and water. Separately, it needs to consume more electric power, and there are moving machines, and the condensed water cannot be recycled.

膜法除湿主要利用膜的选择透过性进行气体除湿,具有除湿过程连续进行、无腐蚀问题、无需阀门切换、无运动部件、系统可靠性高、分离效率高、易维护、压降小、能耗小等优点,近年来,利用膜的选择性和透过性,对空气进行除湿的技术有了重大发展。Membrane dehumidification mainly uses the selective permeability of the membrane for gas dehumidification. It has the advantages of continuous dehumidification process, no corrosion problems, no need for valve switching, no moving parts, high system reliability, high separation efficiency, easy maintenance, small pressure drop, and energy efficiency. In recent years, the technology of using the selectivity and permeability of the membrane to dehumidify the air has made great progress.

中国专利《三流体膜除湿装置和方法》(ZLCN201610170275.9)提出了一种同轴三流体膜除湿装置,该装置主要由膜管、金属套管及外壳三部分组成,由内而外依次是冷水、湿空气、热水,冷水在最内层的膜管内流动,湿空气在膜管与套管之间的环形通道内流动,热水在套管和外壳之间的环形通道内流动。冷水提供较低的水分压,与高水分压的湿空气之间形成水蒸气分压力差,水蒸气会在膜两侧水蒸气分压力差的作用下通过膜孔进入冷水,从而达到除湿的目的。该方法需同时提供冷源和热源,系统结构复杂,设备较多。The Chinese patent "Three-fluid membrane dehumidification device and method" (ZLCN201610170275.9) proposes a coaxial three-fluid membrane dehumidification device. The device is mainly composed of three parts: a membrane tube, a metal casing and a casing. Cold water, humid air, hot water, cold water flows in the innermost membrane tube, moist air flows in the annular channel between the membrane tube and the sleeve, and hot water flows in the annular channel between the sleeve and the casing. The cold water provides a lower water pressure, forming a water vapor partial pressure difference with the humid air with a high water pressure, and the water vapor will enter the cold water through the membrane holes under the action of the water vapor partial pressure difference on both sides of the membrane, so as to achieve the purpose of dehumidification . This method needs to provide cold source and heat source at the same time, the system structure is complicated, and there are many equipments.

采用膜材料的新型空气除湿装置和技术,非常适合在航天器的环境控制系统中应用,具有较好的应用前景。此方法不仅同时降低湿空气的温度和湿度,而且在膜层微孔内的毛细力和水蒸汽分压差的共同主导下,实现水蒸汽向冷水的传输过程,不仅巧妙克服微重力下气液分离的难题,还可直接全部回收航天器舱内宝贵的水蒸汽。由此可见,膜除湿技术在航天领域的应用具有广阔前景,具有积极的现实意义。The new air dehumidification device and technology using membrane materials are very suitable for application in the environmental control system of spacecraft and have good application prospects. This method not only reduces the temperature and humidity of the humid air at the same time, but also realizes the transmission process of water vapor to cold water under the joint leadership of the capillary force in the micropores of the film layer and the partial pressure difference of water vapor, which not only cleverly overcomes the problem of gas-liquid under microgravity. It can also directly recover all the valuable water vapor in the spacecraft cabin. It can be seen that the application of membrane dehumidification technology in the aerospace field has broad prospects and positive practical significance.

发明内容Contents of the invention

本发明要解决的技术问题是提供一种可用于航天微重力环境的空气除湿方法和设备,能同时完成湿空气减焓除湿、气液分离和水蒸汽冷凝回收三种任务,满足航天器的应用需求。The technical problem to be solved by the present invention is to provide an air dehumidification method and equipment that can be used in aerospace microgravity environment, which can simultaneously complete three tasks of humid air enthalpy reduction and dehumidification, gas-liquid separation and water vapor condensation recovery, and satisfy the application of spacecraft need.

为解决上述问题,本发明采用的技术方案如下:In order to solve the above problems, the technical scheme adopted in the present invention is as follows:

本发明复合微孔膜的除湿器,是基于“气-液型”疏水复合微孔膜的除湿过程:其中,复合微孔膜将湿空气和低温冷水分隔开,低温冷水在复合膜的内侧管道内流过,热湿空气在膜管外表面流过,水蒸汽在低温的膜表面冷凝成微液层,微液层只能吸收水蒸汽,有效阻止干空气进入膜层;微液层中的水在表面张力作用下迅速进入膜层内的微孔,微孔内的液态水在表面张力、内外压力差共同作用下向膜层渗流,之后经液-汽相变过程,以水蒸汽的形式进入膜层微孔,再在水蒸汽压力梯度和重力等的共同作用下向冷水侧扩散,并最终在冷水表面冷凝后被冷水吸收带走,从而对热湿空气减焓除湿和气液分离。The dehumidifier of the composite microporous membrane of the present invention is based on the dehumidification process of the "gas-liquid type" hydrophobic composite microporous membrane: wherein, the composite microporous membrane separates the humid air from the low-temperature cold water, and the low-temperature cold water is on the inner side of the composite membrane Flowing through the pipe, hot and humid air flows through the outer surface of the membrane tube, and water vapor condenses on the low-temperature membrane surface to form a micro-liquid layer. The micro-liquid layer can only absorb water vapor, effectively preventing dry air from entering the film layer; in the micro-liquid layer Under the action of surface tension, the water quickly enters the micropores in the membrane layer, and the liquid water in the micropores seeps into the membrane layer under the joint action of surface tension and internal and external pressure difference, and then undergoes a liquid-vapor phase transition process, and is transformed into water vapor. The form enters the micropores of the film layer, and then diffuses to the cold water side under the combined action of the water vapor pressure gradient and gravity, and finally condenses on the surface of the cold water and is taken away by the cold water, thereby reducing enthalpy and dehumidification of the hot and humid air and separating gas and liquid.

复合微孔膜除湿器,包括两侧的端头、法兰、纵长的中段管壳结构、支柱、接头、密封圈、冷水入口流道、冷水出口流道、空气入口流道和空气出口流道构成,两侧端头为固定复合微孔膜丝的两端,分别通过接头和法兰与冷水入口流道和冷水出口流道连通,并确保每根膜丝的入口和出口处通畅,使得低温冷水顺利流入膜丝内部,纵长的中段管壳结构容纳紧密封装在两侧端头的若干纵长的中空纤维复合微孔膜丝并且与两侧端头密封连接,纵长中段结构中心轴线上设置的支柱为支持结构,确保若干中空纤维复合微孔膜丝有足够的机械强度,低温冷水从冷水入口流道进入,流经端头进入膜丝内部,从冷却入口流道流出,进入冷水循环系统,纵长的中段管壳结构侧面上分别靠近两侧端头的位置设置有空气入口流道和空气出口流道,高温高湿的空气从空气入口流道进入,与中空纤维膜丝传热传质后,降低了温度和湿度的空气从空气出口流道流出,送入密封舱内使用。Composite microporous membrane dehumidifier, including ends on both sides, flanges, longitudinal mid-section shell structure, struts, joints, seals, cold water inlet flow, cold water outlet flow, air inlet flow, and air outlet flow The ends on both sides are the two ends of the fixed composite microporous membrane, which are respectively connected with the cold water inlet flow channel and the cold water outlet flow channel through joints and flanges, and ensure that the entrance and exit of each membrane wire are unobstructed, so that Low-temperature cold water smoothly flows into the inside of the membrane filaments, and the longitudinal middle shell structure accommodates a number of longitudinal hollow fiber composite microporous membrane filaments that are tightly packaged at the ends on both sides and is sealed and connected to the ends on both sides. The central axis of the longitudinal middle section structure The pillars set on the top are supporting structures to ensure that several hollow fiber composite microporous membranes have sufficient mechanical strength. Circulation system, the side of the long and middle section shell structure is provided with an air inlet flow channel and an air outlet flow channel at the positions close to the ends of both sides respectively. After heat and mass transfer, the air with reduced temperature and humidity flows out from the air outlet channel and is sent into the sealed cabin for use.

其中,中空纤维膜丝通过疏水性的复合微孔膜支撑,膜管内壁是疏水层,管中的冷水在正常或较低压力下不能向管外侧渗透,保证水蒸汽在表面冷凝后进入膜内,膜管外壁向内壁的传递具有单向性。Among them, the hollow fiber membrane is supported by a hydrophobic composite microporous membrane. The inner wall of the membrane tube is a hydrophobic layer. The cold water in the tube cannot penetrate to the outside of the tube under normal or low pressure, ensuring that water vapor enters the membrane after condensing on the surface. , the transmission from the outer wall to the inner wall of the membrane tube is unidirectional.

其中,中空纤维膜丝以成簇组合形式固定在中段管壳结构的壳内,两端紧密固定在两侧的端头中。Wherein, the hollow fiber membrane filaments are fixed in the shell of the middle tube shell structure in the form of clustering and combination, and the two ends are tightly fixed in the ends on both sides.

其中,中空纤维膜丝为直径在1.1mm-1.9mm的空心结构,膜厚在100μm-200μm可变。Among them, the hollow fiber membrane is a hollow structure with a diameter of 1.1mm-1.9mm, and the membrane thickness is variable between 100μm-200μm.

其中,中空纤维膜丝的微孔膜的孔隙率为50%-80%。Wherein, the porosity of the microporous membrane of the hollow fiber membrane is 50%-80%.

其中,法兰与接头连接处设置有密封圈。Wherein, a sealing ring is arranged at the joint between the flange and the joint.

复合微孔膜除湿装置,包括复合微孔膜除湿器、风机、水泵、辐射散热器、单向阀和集水器,风机将热湿空气送入复合微孔膜除湿器中,热湿空气在除湿器内流经复合微孔膜的管束外侧,水蒸汽完成减焓减湿的除湿过程,变为冷干空气后重新进入舱内环境;随着湿空气焓热的不断加入,膜管内的冷水温度升高,升温后的水在水泵泵送下流经航天器的辐射散热器后降低温度,从而再次成为低温冷水进入除湿器的冷水入口流道,冷却水冷凝出的水通过单向阀被集水器收集。Composite microporous membrane dehumidifier, including composite microporous membrane dehumidifier, fan, water pump, radiation radiator, one-way valve and water collector. The fan sends hot and humid air into the composite microporous membrane dehumidifier. The dehumidifier flows through the outside of the tube bundle of the composite microporous membrane, and the water vapor completes the dehumidification process of reducing enthalpy and dehumidification, becomes cold and dry air, and then re-enters the cabin environment; with the continuous addition of humid air enthalpy, the cold water in the membrane tube As the temperature rises, the heated water flows through the radiation radiator of the spacecraft under the water pump and then lowers its temperature, so that it becomes low-temperature cold water again and enters the cold water inlet channel of the dehumidifier. The water condensed from the cooling water is collected by the one-way valve. Decanter collection.

其中,运行时,低温冷水和高湿空气以逆流形式工作,低温冷水在中空纤维膜丝的管内流动,高湿空气在壳侧以横掠管壳截面积流动,空气侧端头直接连至风道的预留法兰接口,水侧端头留出可接水路的螺纹口,通过软管连接至循环水路。Among them, during operation, the low-temperature cold water and high-humidity air work in a countercurrent manner, the low-temperature cold water flows in the tube of the hollow fiber membrane, and the high-humidity air flows on the shell side by sweeping the cross-sectional area of the shell, and the end of the air side is directly connected to the wind turbine. The reserved flange interface of the channel, the water side end has a threaded port that can be connected to the water circuit, and is connected to the circulating water circuit through a hose.

本发明的装置不仅同时降低湿空气的温度和湿度,而且在膜层微孔内的毛细力和水蒸汽分压差的共同主导下,实现水蒸汽向冷水的传输过程,不仅巧妙克服微重力下气液分离的难题,还可直接全部回收航天器舱内宝贵的水蒸汽。可为航天器的舱内空气湿度控制新技术提供很好的实践基础和试验基础。The device of the present invention not only reduces the temperature and humidity of humid air at the same time, but also realizes the transmission process of water vapor to cold water under the joint leadership of the capillary force in the micropores of the film layer and the partial pressure difference of water vapor, not only ingeniously overcomes the problem of microgravity. The difficult problem of gas-liquid separation can also directly recover all the valuable water vapor in the spacecraft cabin. It can provide a good practice basis and test basis for the new technology of air humidity control in the spacecraft cabin.

附图说明Description of drawings

图1是本发明的复合微孔膜的空气除湿方法中水蒸气透过中空纤维膜丝的示意图,水蒸气传质过程包括湿空气侧的对流传质、膜内扩散以及冷水侧的对流传质。Fig. 1 is the schematic diagram of water vapor passing through the hollow fiber membrane in the air dehumidification method of the composite microporous membrane of the present invention. .

图2是本发明的复合微孔膜除湿器的结构示意图,如图中所示除湿器采用一种管壳式结构,中空纤维膜丝以成簇组合形式固定在除湿器中段纵长管壳结构的壳内,其中,1、端头,2、法兰,3、中段管壳结构,4、支柱,5、接头,6、密封圈,7、冷水入口流道,8、冷水出口流道,10、空气入口流道,9、空气出口流道,中空纤维膜丝未标示。Fig. 2 is a schematic structural view of the composite microporous membrane dehumidifier of the present invention. As shown in the figure, the dehumidifier adopts a shell-and-tube structure, and the hollow fiber membranes are fixed in the middle section of the dehumidifier in the form of a clustered combination. In the shell, among them, 1. end, 2. flange, 3. shell structure in the middle section, 4. pillar, 5. joint, 6. sealing ring, 7. cold water inlet flow channel, 8. cold water outlet flow channel, 10. Air inlet channel, 9. Air outlet channel, hollow fiber membranes are not marked.

图3是本发明的复合微孔膜除湿器装置的结构示意图,图中,包括复合微孔膜除湿器、风机、水泵、辐射散热器、单向阀和集水器组成。Fig. 3 is a structural schematic diagram of the composite microporous membrane dehumidifier device of the present invention, in which, the composite microporous membrane dehumidifier, fan, water pump, radiation radiator, one-way valve and water collector are composed.

具体实施方式Detailed ways

以下参照附图对本发明的复合微孔膜除湿方法和装置进行详细说明,但该描述仅仅示例性的,并不旨在对本发明的保护范围进行任何限制。The composite microporous membrane dehumidification method and device of the present invention will be described in detail below with reference to the accompanying drawings, but the description is only exemplary and not intended to limit the protection scope of the present invention.

参见图1,图1显示了本发明的复合微孔膜的空气除湿方法中水蒸气透过中空纤维膜丝的示意图,水蒸气传质过程包括湿空气侧的对流传质、膜内扩散以及冷水侧的对流传质。其中,复合膜将湿空气和低温冷水分隔开,低温冷水在复合膜的渗透侧流过,热湿空气在膜管外原料侧流过,水蒸汽在低温的膜表面冷凝成微液层,微液层只能吸收水蒸汽,有效阻止干空气进入膜层;水蒸气在微液层中的水在表面张力作用下迅速进入膜层内的微孔,微孔内的液态水在表面张力、内外压力差等共同作用下向渗透侧膜层渗流;在原料侧以水蒸汽的形式进入疏水性膜层微孔,在水蒸汽压力梯度的作用下向渗透侧扩散,并最终在冷水表面冷凝后被冷水吸收带走,从而达到对热湿空气减焓除湿和气液分离的双重目的。Referring to Fig. 1, Fig. 1 has shown the schematic diagram that water vapor passes through hollow fiber membrane silk in the air dehumidification method of composite microporous membrane of the present invention, and water vapor mass transfer process comprises the convective mass transfer of moist air side, diffusion and cold water side convective mass transfer. Among them, the composite membrane separates the humid air from the low-temperature cold water, the low-temperature cold water flows through the permeation side of the composite membrane, the hot and humid air flows through the raw material side outside the membrane tube, and the water vapor condenses into a micro-liquid layer on the low-temperature membrane surface. The micro-liquid layer can only absorb water vapor, which effectively prevents dry air from entering the film layer; the water vapor in the micro-liquid layer quickly enters the micropores in the film layer under the action of surface tension, and the liquid water in the micropores is under surface tension, Under the joint action of internal and external pressure difference, it seeps to the permeate side membrane layer; on the raw material side, water vapor enters the micropores of the hydrophobic membrane layer, diffuses to the permeate side under the action of the water vapor pressure gradient, and finally condenses on the cold water surface It is absorbed and taken away by cold water, so as to achieve the dual purposes of reducing enthalpy and dehumidification of hot and humid air and separating gas and liquid.

图2是本发明的复合微孔膜除湿器的剖面图,复合微孔膜除湿器采用一种管壳式结构,低温冷水和高湿空气以逆流形式工作,其中,复合微孔膜除湿器包括两侧的端头1、法兰2、纵长的中段管壳结构3、支柱4、接头5、密封圈6、冷水入口流道7、冷水出口流道8、空气入口流道10和空气出口流道9构成,两侧端头1为固定复合微孔膜丝的两端,分别通过接头5和法兰2与冷水入口流道7和冷水出口流道8连通,并确保每根膜丝的入口和出口处通畅,使得低温冷水顺利流入膜丝内部,纵长的中段管壳结构3容纳紧密封装在两侧端头1的若干纵长的中空纤维复合微孔膜丝并且与两侧端头1密封连接,纵长中段管壳结构3中心轴线上设置的支柱4为支持结构,确保膜丝有足够的机械强度,支柱4起到支撑两个端头间的距离的作用,因为膜丝为软性的无支撑,无强度的中空纤维膜丝,直径在1.1mm-1.9mm的空心结构,膜厚在100μm-200μm可变。其中,用于制造中空纤维膜丝的微孔膜为市面上或厂家市购的成熟产品,例如购自中科院大连物化所、山东东旭蓝天环保科技有限公司、康泽源(天津)科技发展有限公司的产品,其区别在于对膜材料、膜管尺寸、膜面孔隙等性能的要求,中空纤维膜丝的制造方法也可以通过已知的溶液纺丝法制备方法加以制造。其中低温冷水从冷水入口流道7进入,流经端头进入膜丝内部,从冷水出口流道8流出,进入冷水循环系统,纵长的中段管壳结构3侧面上分别靠近两侧端头的位置设置有空气入口流道10和空气出口流道9,高温高湿的空气从空气入口流道10进入,与中空纤维膜丝传热传质后,降低了温度和湿度的空气从空气出口流9流出,送入密封舱内使用。Fig. 2 is a sectional view of the composite microporous membrane dehumidifier of the present invention, the composite microporous membrane dehumidifier adopts a shell-and-tube structure, and low-temperature cold water and high-humidity air work in countercurrent form, wherein the composite microporous membrane dehumidifier includes The ends on both sides 1, the flange 2, the longitudinal middle shell structure 3, the pillar 4, the joint 5, the sealing ring 6, the cold water inlet flow channel 7, the cold water outlet flow channel 8, the air inlet flow channel 10 and the air outlet The flow channel 9 is formed, and the ends 1 on both sides are the two ends of the fixed composite microporous membrane, which are respectively connected with the cold water inlet flow channel 7 and the cold water outlet flow channel 8 through the joint 5 and the flange 2, and ensure the The entrance and exit are unobstructed, so that low-temperature cold water flows smoothly into the interior of the membrane filaments, and the longitudinal middle section shell structure 3 accommodates several longitudinal hollow fiber composite microporous membrane filaments tightly packaged at the ends 1 on both sides and is connected to the ends on both sides. 1 Sealed connection, the longitudinal middle section shell structure 3 The pillar 4 set on the central axis is a supporting structure to ensure that the membrane filament has sufficient mechanical strength, and the pillar 4 plays the role of supporting the distance between the two ends, because the membrane filament is Soft unsupported, non-strength hollow fiber membrane, hollow structure with a diameter of 1.1mm-1.9mm, and a variable membrane thickness of 100μm-200μm. Among them, the microporous membranes used to manufacture hollow fiber membranes are mature products on the market or purchased by manufacturers, such as those purchased from Dalian Institute of Physics and Chemistry, Chinese Academy of Sciences, Shandong Dongxu Lantian Environmental Protection Technology Co., Ltd., and Kang Zeyuan (Tianjin) Technology Development Co., Ltd. Products, the difference lies in the performance requirements of the membrane material, membrane tube size, membrane surface pores, etc. The manufacturing method of the hollow fiber membrane can also be manufactured by the known solution spinning method. Among them, the low-temperature cold water enters from the cold water inlet flow channel 7, flows through the end into the inside of the membrane filament, flows out from the cold water outlet flow channel 8, and enters the cold water circulation system. The position is provided with an air inlet flow channel 10 and an air outlet flow channel 9. The air with high temperature and high humidity enters from the air inlet flow channel 10, and after heat and mass transfer with the hollow fiber membrane, the air with reduced temperature and humidity flows from the air outlet. 9 flows out and is sent into the airtight cabin for use.

图3是本发明的复合微孔膜除湿器装置的结构示意图,包含除湿器、风机、水泵、辐射散热器、单向阀和集水器。除湿器的冷水接口与冷水循环系统相连,利用水泵实现冷水的循环流动,从高温高湿空气中吸收的热量由辐射器将热量带走以保持冷水温度,从高温高湿空气中吸收的水量经由单向阀送入集水器中收集。除湿器的空气接口与高温高湿空气管路系统相连,通过风机实现高温高湿空气经由除湿器的单向流动。Fig. 3 is a schematic structural view of the composite microporous membrane dehumidifier device of the present invention, including a dehumidifier, fan, water pump, radiation radiator, one-way valve and water collector. The cold water interface of the dehumidifier is connected to the cold water circulation system, and the water pump is used to realize the circulation of cold water. The heat absorbed from the high-temperature and high-humidity air is taken away by the radiator to maintain the temperature of the cold water. The water absorbed from the high-temperature and high-humidity air passes through The one-way valve is sent into the water collector for collection. The air interface of the dehumidifier is connected to the high-temperature and high-humidity air pipeline system, and the one-way flow of high-temperature and high-humidity air through the dehumidifier is realized through the fan.

在完成设计的基础上,开展了相应的试验研究。在高温高湿空气温度在23度时,空气相对湿度在30%-70%间变化,空气入口表压为9kPa,空气流量为76L/min;冷水入口温度稳定在9℃,液体流量为455mL/min。由于采用的是逆流换热形式,因此空气的温度由入口时的23℃左右降至15℃,空气出口的温度17℃较为稳定,冷水的温度由入口时的9℃升至出口时的13℃,冷水的出口温度由11℃升至13℃。气体入口的含湿量为14g/kg,而出口的含湿量稳定在8g/kg。在采用由100根膜管,表面积为0.1m2时,入口相对湿度为70%时除湿量为14.16g/h。On the basis of completing the design, the corresponding experimental research was carried out. When the high-temperature and high-humidity air temperature is 23 degrees, the relative humidity of the air varies between 30% and 70%, the air inlet gauge pressure is 9kPa, and the air flow rate is 76L/min; the cold water inlet temperature is stable at 9°C, and the liquid flow rate is 455mL/min min. Due to the use of countercurrent heat exchange, the temperature of the air drops from about 23°C at the inlet to 15°C, the temperature at the air outlet is relatively stable at 17°C, and the temperature of the cold water rises from 9°C at the inlet to 13°C at the outlet , the outlet temperature of the cold water rose from 11°C to 13°C. The moisture content of the gas inlet was 14 g/kg, while the moisture content of the outlet was stable at 8 g/kg. When using 100 membrane tubes with a surface area of 0.1m 2 , the dehumidification capacity is 14.16g/h when the inlet relative humidity is 70%.

尽管上文对本发明的具体实施方式给予了详细描述和说明,但是应该指明的是,我们可以依据本发明的构想对上述实施方式进行各种等效改变和修改,其所产生的功能作用仍未超出说明书及附图所涵盖的精神时,均应在本发明的保护范围之内。Although the specific embodiments of the present invention have been described and illustrated in detail above, it should be pointed out that we can make various equivalent changes and modifications to the above-mentioned embodiments according to the concept of the present invention, and the functional effects produced by it are still the same. Anything beyond the spirit contained in the specification and drawings shall fall within the protection scope of the present invention.

Claims (10)

1. composite micro porous film dehumidifier, including the end of both sides, flange, the stage casing shell structure of lengthwise, pillar, connector, sealing Circle, cold water inlet runner, cooling water outlet runner, air intake runner and air outlet slit runner are constituted, and both sides end is fixed multiple The both ends for closing micropore film wire, are connected to by connector and flange with cold water inlet runner and cooling water outlet runner respectively, and are ensured every It is unobstructed at the entrance and exit of root film wire so that low-temperature cold water smoothly flows into inside film wire, and the stage casing shell structure of lengthwise accommodates Compact package several lengthwises of both sides end the composite microporous film wire of doughnut and with both sides end be tightly connected, lengthwise The pillar being arranged on middle section structure central axis is support structure, it is ensured that several composite microporous film wires of doughnut have enough machines Tool intensity, low-temperature cold water enter from cold water inlet runner, flow through end and enter inside film wire, are flowed out from cooling entrance channel, into Enter cold water circulating system, the position on the stage casing shell structure side of lengthwise respectively close to both sides end is provided with air intake stream The air of road and air outlet slit runner, high temperature and humidity enters from air intake runner, after hollow fiber film thread heat and mass, drop The air of low temperature and humidity is flowed out from air outlet slit runner, is sent into sealed compartment and is used.
2. dehumidifier as described in claim 1, wherein hollow fiber film thread is supported by hydrophobic composite micro porous film, film Inside pipe wall is hydrophobic layer, and the cold water in pipe cannot ensure water vapour on surface under normal or lower pressure to permeating on the outside of pipe Enter in film after condensation, the transmission of membrane tube outer wall inward wall has one-way.
3. dehumidifier as claimed in claim 1 or 2, wherein hollow fiber film thread is fixed on stage casing with cluster combining form and manages In the shell of shell structure, both ends are tightly fixed in the end of both sides.
4. dehumidifier as claimed in claim 3, wherein hollow fiber film thread is hollow-core construction of the diameter in 1.1mm-1.9mm, Film thickness can be changed at 100 μm -200 μm.
5. dehumidifier as claimed in claim 3, wherein the porosity of the microporous barrier of hollow fiber film thread is 50%-80%.
6. dehumidifier as described in claim 1, wherein flange is provided with sealing ring with joint.
7. composite microporous membrane dehumidifier, including claim 1-6 any one of them composite micro porous films dehumidifier, wind turbine, water Hot wet air heating is sent into composite micro porous film dehumidifier by pump, radiator, check valve and water collector, wind turbine, and Hot wet air heating exists On the outside of the tube bank for flowing through composite micro porous film in dehumidifier, water vapour is completed to subtract the dehumidification process of enthalpy dehumidification, after becoming cold dry air Reenter indoor environment;With being continuously added for humid air property heat, the cold water temperature in membrane tube increases, and the water after heating is in water Temperature is reduced after flowing through the radiator of spacecraft under pump pumping, to become the cold water that low-temperature cold water enters dehumidifier again Entrance channel, the water that cooling water condensation goes out are collected by check valve by water collector.
8. composite microporous membrane dehumidifier as claimed in claim 7, wherein when operation, low-temperature cold water and highly humid air are with inverse Manifold formula works, and for low-temperature cold water in the Bottomhole pressure of hollow fiber film thread, highly humid air plunders shell sectional area stream in shell-side with horizontal Dynamic, air side end is directly connected to the reserved flange-interface in air duct, water side head reserve can water receiving road screw thread mouth, pass through hose It is connected to circulation waterway.
9. composite microporous membrane dehumidifier as claimed in claim 7, wherein hollow fiber film thread is completely filled with stage casing shell knot Structure.
10. composite microporous membrane dehumidifier as claimed in claim 7, wherein also set in cold water inlet runner and membrane tube Temperature measuring equipment is equipped with to monitor water temperature.
CN201810832959.XA 2018-07-26 2018-07-26 Air dehumidifier based on composite micro porous film and dehumidification device Pending CN108619868A (en)

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CN111720943A (en) * 2019-03-22 2020-09-29 卢定伟 Efficient full heat exchange fresh air recovery module
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CN102814104A (en) * 2011-06-08 2012-12-12 北京航空航天大学 Novel dehumidifying apparatus on basis of hydrophilic/hydrophobic composite microporous membranes under microgravity
WO2018063849A1 (en) * 2016-09-28 2018-04-05 Dow Corning Corporation Radiant heat transfer device and membrane or liquid contactor for dehumidification or humidification of air

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CN111111358A (en) * 2018-10-31 2020-05-08 南京圣卡孚科技有限公司 Method and device for separating condensable component liquid drops in gas-phase medium
CN111111358B (en) * 2018-10-31 2022-02-18 南京圣卡孚科技有限公司 Method and device for separating condensable component liquid drops in gas-phase medium
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