CN205117838U - Pneumatics drive formula liquid suction device - Google Patents
Pneumatics drive formula liquid suction device Download PDFInfo
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- CN205117838U CN205117838U CN201520926478.7U CN201520926478U CN205117838U CN 205117838 U CN205117838 U CN 205117838U CN 201520926478 U CN201520926478 U CN 201520926478U CN 205117838 U CN205117838 U CN 205117838U
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Abstract
一种空压驱动式液体吸排装置,包括壳体、气嘴、第一阀门及第二阀门,壳体中心孔为三级阶梯孔结构,气嘴外筒壁为三级阶梯台结构,壳体与气嘴之间通过螺纹相连,两者之间通过密封圈密封,在气嘴上设有内凹的圆锥孔结构,在壳体内设有圆锥台结构件,圆锥孔结构与圆锥台结构件对应配合,两者之间留有环锥形缝隙,两者锥角范围在45°~75°;在壳体上设有压缩空气进气口,第一阀门连通在压缩空气进气口上,第二阀门连通在气嘴中心孔上;在壳体中心孔下孔口加装有满容防外泄组件。本实用新型实现了一种全新的液体吸排方式,仅采用压缩空气作为液体转运的动力源,提高了危险类液体的转运安全性,对污浊液体的转运无颗粒度要求,适用的液体种类范围更广。
An air pressure-driven liquid suction and discharge device, including a housing, an air nozzle, a first valve and a second valve, the central hole of the housing has a three-stage stepped hole structure, the outer cylinder wall of the air nozzle has a three-stage stepped platform structure, and the housing It is connected with the air nozzle through threads, and the two are sealed by a sealing ring. There is a concave conical hole structure on the air nozzle, and a conical truncated structure is provided in the shell. The conical hole structure corresponds to the conical truncated structure. Cooperate, there is a ring-shaped conical gap between the two, and the cone angle ranges from 45° to 75°; there is a compressed air inlet on the shell, the first valve is connected to the compressed air inlet, and the second valve is connected to the compressed air inlet. The valve is connected to the center hole of the gas nozzle; a full-capacity anti-leakage component is installed at the lower hole of the shell center hole. The utility model realizes a brand-new liquid suction and discharge method, only uses compressed air as the power source of liquid transfer, improves the transfer safety of dangerous liquids, has no particle size requirements for the transfer of dirty liquids, and has a wider range of applicable liquid types wide.
Description
技术领域technical field
本实用新型属于液体类物质运输技术领域,特别是涉及一种空压驱动式液体吸排装置。The utility model belongs to the technical field of liquid material transportation, in particular to an air pressure-driven liquid suction and discharge device.
背景技术Background technique
在工业生产中,对于液体类物质的运输,无外乎两种途径,一种是通过液体泵对液体类物质进行转运,另一种是通过人工方式转运。通过液体泵转运液体类物质是工业生产中比较常用且高效的转运方式,而人工转运方式只适用于少量液体类物质的转运,因其转运效率比较低。In industrial production, there are no more than two ways to transport liquid substances, one is to transport liquid substances through liquid pumps, and the other is to transport them manually. The transfer of liquid substances through liquid pumps is a common and efficient transfer method in industrial production, while the manual transfer method is only suitable for the transfer of a small amount of liquid substances because of its relatively low transfer efficiency.
对于一些易燃性及腐蚀性比较高的液体,在其转运过程中都具有一定的危险性,而这些危险类液体对泵本身的安全性影响也非常高,因此,有必要找到一种能够提高危险类液体转运安全性的新型转运方式。For some highly flammable and corrosive liquids, there is a certain degree of danger during their transfer, and these dangerous liquids also have a very high impact on the safety of the pump itself. Therefore, it is necessary to find a method that can improve A new transport method for the safety of hazardous liquid transport.
对于一些混有大量颗粒物的污浊液体,如果采用液体泵进行转运,对泵体伤害是非常大的,一旦污浊液体中的颗粒物粒度过大,液体泵将不再适用,最终只能被迫采用人工方式转运,因此,有必要找到以一种无颗粒度要求的污浊液体新型转运方式。For some dirty liquid mixed with a large amount of particles, if the liquid pump is used for transport, the damage to the pump body will be very large. Once the particle size in the dirty liquid is too large, the liquid pump will no longer be suitable, and finally can only be forced to use artificial Therefore, it is necessary to find a new transport method for dirty liquids without particle size requirements.
实用新型内容Utility model content
针对现有技术存在的问题,本实用新型提供一种空压驱动式液体吸排装置,能够提高危险类液体的转运安全性,对污浊液体的转运无颗粒度要求。Aiming at the problems existing in the prior art, the utility model provides an air pressure-driven liquid suction and discharge device, which can improve the safety of the transfer of dangerous liquids and has no granularity requirements for the transfer of dirty liquids.
为了实现上述目的,本实用新型采用如下技术方案:一种空压驱动式液体吸排装置,包括壳体、气嘴、第一阀门及第二阀门,所述壳体采用两端为开口的圆柱筒形结构,壳体的中心孔采用三级阶梯孔结构,中心孔的孔径由大到小依次为大孔段、中孔段及小孔段,在大孔段的壳体内壁上设有内螺纹,在中孔段的壳体内壁上开设有压缩空气进气口,所述第一阀门连通在压缩空气进气口上;所述气嘴采用两端为开口的圆柱筒形结构,气嘴的外筒壁采用三级阶梯台结构,外筒壁的外径由大到小依次为大径段、中径段及小径段,在大径段的气嘴外壁上设有外螺纹,气嘴与壳体通过内、外螺纹配合连接;所述第二阀门连通在大径段的气嘴中心孔孔口上;在所述中径段的气嘴外壁上安装有第一密封圈,第一密封圈与中孔段的壳体内壁相配合;所述小径段的气嘴外壁与中孔段的壳体内壁相对应,且二者之间留有环向间隙,小径段的气嘴中心孔孔口设置为内凹的圆锥孔结构,所述壳体中心孔的中孔段与小孔段过渡梯台面上设置有圆锥台结构件,所述气嘴的圆锥孔结构与壳体的圆锥台结构件相对应,在圆锥孔结构与圆锥台结构件之间留有环锥形缝隙;在所述小孔段的壳体外壁上安装有第二密封圈。In order to achieve the above purpose, the utility model adopts the following technical scheme: a pneumatically driven liquid suction and discharge device, including a shell, an air nozzle, a first valve and a second valve, the shell adopts a cylindrical tube with openings at both ends Shaped structure, the central hole of the shell adopts a three-stage stepped hole structure. The apertures of the central hole from large to small are the large hole section, the middle hole section and the small hole section. Internal threads are provided on the inner wall of the shell of the large hole section. , a compressed air inlet is opened on the inner wall of the shell of the middle hole section, and the first valve is connected to the compressed air inlet; the air nozzle adopts a cylindrical structure with openings at both ends, and the outer surface of the air nozzle The cylinder wall adopts a three-stage stepped structure. The outer diameter of the outer cylinder wall from large to small is the large diameter section, the middle diameter section and the small diameter section. There are external threads on the outer wall of the gas nozzle in the large diameter section. The gas nozzle and the shell The body is connected through internal and external threads; the second valve is connected to the center hole of the gas nozzle in the large-diameter section; a first sealing ring is installed on the outer wall of the gas nozzle in the middle-diameter section, and the first sealing ring and The inner wall of the shell of the middle hole section matches; the outer wall of the gas nozzle of the small diameter section corresponds to the inner wall of the shell of the middle hole section, and there is a circumferential gap between the two, and the center hole of the air nozzle of the small diameter section is set It is a concave conical hole structure. A truncated conical structure is arranged on the transitional ladder platform between the middle hole section and the small hole section of the central hole of the housing. Correspondingly, there is an annular conical gap between the conical hole structure and the truncated conical structure; a second sealing ring is installed on the outer wall of the shell of the small hole section.
所述圆锥孔结构与圆锥台结构件的锥角相同,其锥角范围在45°~75°。The cone angle of the conical hole structure is the same as that of the truncated cone structure, and the cone angle ranges from 45° to 75°.
作为优选,所述圆锥孔结构与圆锥台结构件的锥角均为60°。Preferably, the taper angles of the conical hole structure and the truncated conical structure are both 60°.
在所述壳体中心孔的小孔段孔口处加装有满容防外泄组件,所述满容防外泄组件包括透液套管及浮力塞,所述透液套管表面加工有若干透液孔,透液套管上端管口与壳体中心孔的小孔段孔口相连通,透液套管下端管口为封闭端,所述浮力塞位于透液套管内,浮力塞与壳体中心孔的小孔段孔口相对应。A full-capacity anti-leakage assembly is installed at the orifice of the small hole section of the central hole of the shell. The full-capacity anti-leakage assembly includes a liquid-permeable sleeve and a buoyancy plug. The surface of the liquid-permeable sleeve is processed with Several liquid-permeable holes, the nozzle at the upper end of the liquid-permeable casing communicates with the small-hole section of the central hole of the shell, the nozzle at the lower end of the liquid-permeable casing is a closed end, the buoyancy plug is located in the liquid-permeable casing, and the buoyancy plug and The small hole section orifice of the housing central hole is corresponding.
所述满容防外泄组件与壳体之间采用可拆卸式连接方式。A detachable connection is adopted between the full-capacity anti-leakage assembly and the housing.
本实用新型的有益效果:The beneficial effects of the utility model:
本实用新型与现有技术相比,实现了一种全新的液体吸排方式,仅采用压缩空气作为液体转运的动力源,克服了传统采用液体泵转运液体过程中的弊端,不但有效提高了危险类液体的转运安全性,且对污浊液体的转运无颗粒度要求,所适用的液体种类范围更广。Compared with the prior art, the utility model realizes a brand-new liquid suction and discharge method, only uses compressed air as the power source of liquid transfer, overcomes the disadvantages of the traditional liquid pump transfer process, and not only effectively improves the level of danger. The transfer of liquids is safe, and there is no particle size requirement for the transfer of dirty liquids, and the range of applicable liquids is wider.
附图说明Description of drawings
图1为本实用新型的一种空压驱动式液体吸排装置结构示意图;Fig. 1 is a schematic structural diagram of an air pressure-driven liquid suction and discharge device of the present invention;
图2为本实用新型的壳体结构示意图;Fig. 2 is a schematic diagram of the housing structure of the present utility model;
图3为本实用新型的气嘴结构示意图;Fig. 3 is the structural representation of the gas nozzle of the utility model;
图中,1—壳体,2—气嘴,3—第一阀门,4—第二阀门,5—大孔段,6—中孔段,7—小孔段,8—压缩空气进气口,9—大径段,10—中径段,11—小径段,12—第一密封圈,13—环向间隙,14—圆锥孔结构,15—圆锥台结构件,16—环锥形缝隙,17—第二密封圈,18—透液套管,19—浮力塞,20—透液孔。In the figure, 1—shell, 2—gas nozzle, 3—first valve, 4—second valve, 5—large hole section, 6—medium hole section, 7—small hole section, 8—compressed air inlet . , 17—the second sealing ring, 18—the liquid-permeable casing, 19—the buoyancy plug, 20—the liquid-permeable hole.
具体实施方式detailed description
下面结合附图和具体实施例对本实用新型做进一步的详细说明。Below in conjunction with accompanying drawing and specific embodiment the utility model is described in further detail.
如图1、2、3所示,一种空压驱动式液体吸排装置,包括壳体1、气嘴2、第一阀门3及第二阀门4,所述壳体1采用两端为开口的圆柱筒形结构,壳体1的中心孔采用三级阶梯孔结构,中心孔的孔径由大到小依次为大孔段5、中孔段6及小孔段7,在大孔段5的壳体1内壁上设有内螺纹,在中孔段6的壳体1内壁上开设有压缩空气进气口8,所述第一阀门3连通在压缩空气进气口8上;所述气嘴2采用两端为开口的圆柱筒形结构,气嘴2的外筒壁采用三级阶梯台结构,外筒壁的外径由大到小依次为大径段9、中径段10及小径段11,在大径段9的气嘴2外壁上设有外螺纹,气嘴2与壳体1通过内、外螺纹配合连接;所述第二阀门4连通在大径段9的气嘴2中心孔孔口上;在所述中径段10的气嘴2外壁上安装有第一密封圈12,第一密封圈12与中孔段6的壳体1内壁相配合;所述小径段11的气嘴2外壁与中孔段6的壳体1内壁相对应,且二者之间留有环向间隙13,小径段11的气嘴2中心孔孔口设置为内凹的圆锥孔结构14,所述壳体1中心孔的中孔段6与小孔段7过渡梯台面上设置有圆锥台结构件15,所述气嘴2的圆锥孔结构14与壳体1的圆锥台结构件15相对应,在圆锥孔结构14与圆锥台结构件15之间留有环锥形缝隙16;在所述小孔段7的壳体1外壁上安装有第二密封圈17。As shown in Figures 1, 2, and 3, an air pressure-driven liquid suction and discharge device includes a housing 1, an air nozzle 2, a first valve 3 and a second valve 4. Cylindrical structure, the central hole of the shell 1 adopts a three-stage stepped hole structure, and the diameter of the central hole from large to small is the large hole section 5, the middle hole section 6 and the small hole section 7, and the shell of the large hole section 5 Internal threads are provided on the inner wall of the body 1, and a compressed air inlet 8 is opened on the inner wall of the shell 1 of the middle hole section 6, and the first valve 3 is connected to the compressed air inlet 8; the air nozzle 2 A cylindrical structure with openings at both ends is adopted, and the outer cylinder wall of the gas nozzle 2 adopts a three-stage stepped structure. The outer diameter of the outer cylinder wall from large to small is the large diameter section 9, the middle diameter section 10 and the small diameter section 11. , the outer wall of the gas nozzle 2 of the large-diameter section 9 is provided with external threads, and the gas nozzle 2 is connected with the housing 1 through internal and external threads; the second valve 4 is connected to the center hole of the gas nozzle 2 of the large-diameter section 9 On the orifice; the first sealing ring 12 is installed on the outer wall of the gas nozzle 2 of the middle diameter section 10, and the first sealing ring 12 is matched with the inner wall of the housing 1 of the middle hole section 6; the gas nozzle of the small diameter section 11 2 The outer wall corresponds to the inner wall of the shell 1 of the middle hole section 6, and there is an annular gap 13 between them, and the center hole of the gas nozzle 2 of the small diameter section 11 is set as a concave conical hole structure 14, the The middle hole section 6 and the small hole section 7 of the center hole of the housing 1 are provided with a truncated conical structure 15 on the transitional ladder platform, and the conical hole structure 14 of the gas nozzle 2 corresponds to the truncated cone structure 15 of the housing 1. An annular conical gap 16 is left between the conical hole structure 14 and the truncated conical structure member 15 ; a second sealing ring 17 is installed on the outer wall of the housing 1 of the small hole section 7 .
所述圆锥孔结构14与圆锥台结构件15的锥角相同,其锥角范围在45°~75°。The cone angle of the conical hole structure 14 is the same as that of the truncated cone structure 15 , and the cone angle ranges from 45° to 75°.
作为优选,所述圆锥孔结构14与圆锥台结构件15的锥角均为60°,经过实际测试,当锥角为60°时,可以形成最佳的真空度,保证最大吸力。As a preference, the cone angles of the conical hole structure 14 and the truncated cone structure 15 are both 60°. According to actual tests, when the cone angle is 60°, the best vacuum degree can be formed to ensure the maximum suction force.
为了防止储液容器在满容时出现液体过吸外泄的情况,在所述壳体1中心孔的小孔段7孔口处加装有满容防外泄组件,所述满容防外泄组件包括透液套管18及浮力塞19,所述透液套管18表面加工有若干透液孔20,透液套管18上端管口与壳体1中心孔的小孔段7孔口相连通,透液套管18下端管口为封闭端,所述浮力塞19位于透液套管18内,浮力塞19与壳体1中心孔的小孔段7孔口相对应。In order to prevent the liquid storage container from over-absorbing and leaking when it is full, a full-capacity anti-leakage component is installed at the orifice of the small hole section 7 in the center hole of the housing 1. The discharge assembly includes a liquid-permeable sleeve 18 and a buoyancy plug 19. The surface of the liquid-permeable sleeve 18 is processed with a number of liquid-permeable holes 20. Connected to each other, the nozzle at the lower end of the liquid-permeable casing 18 is a closed end, and the buoyancy plug 19 is located in the liquid-permeable casing 18, and the buoyancy plug 19 corresponds to the aperture of the small hole section 7 of the central hole of the shell 1.
所述满容防外泄组件与壳体1之间采用可拆卸式连接方式。The full-capacity anti-leakage assembly is connected to the housing 1 in a detachable manner.
下面结合附图说明本实用新型的一次使用过程:Below in conjunction with accompanying drawing, the one-time use process of the present utility model is illustrated:
实施例一Embodiment one
利用本实用新型的吸排装置进行吸液操作,本实施例中,液体为航空煤油,容器为承装航空煤油的专用油桶,压缩空气的压力为6MPa。Use the suction and discharge device of the utility model to carry out the liquid suction operation. In the present embodiment, the liquid is aviation kerosene, the container is a special oil barrel for bearing aviation kerosene, and the pressure of the compressed air is 6MPa.
首先,将本实用新型安装到油桶的一个桶口内,准备一根软油管,软油管一端与油桶的另一个桶口密封连通,软油管另一端插入在外部油源中,然后将第一阀门3与现场的压缩空气源相连通。First, the utility model is installed in a bung mouth of the oil barrel, and a soft oil pipe is prepared, one end of the soft oil pipe is sealed and communicated with the other bung mouth of the oil barrel, and the other end of the soft oil pipe is inserted into an external oil source, and then the first Valve 3 communicates with the compressed air source on site.
进行吸液作业前,将第二阀门4调整到开启位置,第一阀门3处于关闭位置;开始吸液作业,首先启动压缩空气源,然后打开第一阀门3,压缩空气依次经过环向间隙13及环锥形缝隙16,并沿着环锥形缝隙16喷向第二阀门4,最后由第二阀门4排出,在此过程中,通过环锥形缝隙16连续不断的喷射压缩空气,就会在喷射流后方形成一定范围的真空负压区,随着真空负压区的形成,油桶内的空气会被不断的吸出,从而使油桶内形成负压环境,此时,通过软油管就可以把外部的航空煤油不断的吸入到油桶内。Before the liquid suction operation, adjust the second valve 4 to the open position, and the first valve 3 is in the closed position; start the liquid suction operation, first start the compressed air source, then open the first valve 3, and the compressed air passes through the annular gap 13 in sequence and the ring-shaped tapered gap 16, and spray along the ring-shaped tapered gap 16 to the second valve 4, and finally be discharged by the second valve 4. During this process, the compressed air will be injected continuously through the ring-shaped tapered gap 16. A certain range of vacuum negative pressure area is formed behind the jet flow. With the formation of the vacuum negative pressure area, the air in the oil barrel will be continuously sucked out, so that a negative pressure environment is formed in the oil barrel. The external aviation kerosene can be continuously sucked into the oil drum.
随着航空煤油不断的被吸入油桶,油桶内的液面也会不断升高,当航空煤油快达到满容时,满容防外泄组件内的浮力塞19也会随着液面一同上升,当航空煤油接近满容时,上升的浮力塞19会对封堵住壳体1中心孔,此时通过浮力塞19将真空负压区与油桶内腔隔离开,油桶内的压力恢复正常,吸油过程结束,有效防止了航空煤油因满容而外泄的情况发生。As the aviation kerosene is continuously sucked into the oil barrel, the liquid level in the oil barrel will also continue to rise. When the aviation kerosene is about to reach full capacity, the buoyancy plug 19 in the full capacity anti-leakage assembly will also increase with the liquid level. When the aviation kerosene is nearly full, the rising buoyancy plug 19 will block the center hole of the shell 1. At this time, the buoyancy plug 19 will isolate the vacuum negative pressure area from the inner cavity of the oil drum, and the pressure in the oil drum will Return to normal, the oil absorption process is over, effectively preventing the leakage of aviation kerosene due to full capacity.
实施例二Embodiment two
利用本实用新型的吸排装置进行排液操作,本实施例中,液体为航空煤油,容器为承装航空煤油的专用油桶,且油桶内满载有航空煤油,压缩空气的压力为6MPa。Utilize the suction and discharge device of the utility model to carry out the liquid discharge operation. In this embodiment, the liquid is aviation kerosene, the container is a special oil barrel for carrying aviation kerosene, and the oil barrel is fully loaded with aviation kerosene, and the pressure of the compressed air is 6MPa.
由于进行排油作业,可将满容防外泄组件卸下,然后将本实用新型安装到油桶的一个桶口内,在油桶的另一个桶口内插入一个导管,使导管下端贴近油桶的桶底,导管上端位于桶口上方,导管与桶口进行密封处理。Due to the oil discharge operation, the full-capacity anti-leakage assembly can be removed, and then the utility model is installed in one mouth of the oil barrel, and a conduit is inserted into the other mouth of the oil barrel, so that the lower end of the conduit is close to the bottom of the oil barrel At the bottom of the barrel, the upper end of the conduit is located above the mouth of the barrel, and the conduit and the mouth of the barrel are sealed.
进行排液作业前,将第二阀门4调整到关闭位置,第一阀门3处于关闭位置;开始排液作业,首先启动压缩空气源,然后打开第一阀门3,压缩空气依次经过环向间隙13及环锥形缝隙16,并沿着环锥形缝隙16喷向第二阀门4,但是,由于第二阀门4处于关闭状态,压缩空气会被迫排入油桶内,从而使油桶内形成正压环境,随着压缩空气的不断排入,油桶内的航空煤油会在高压作用下通过导管不断的被挤出油桶,从而实现了持续排油的目的。Before the liquid discharge operation, adjust the second valve 4 to the closed position, and the first valve 3 is in the closed position; start the liquid discharge operation, first start the compressed air source, then open the first valve 3, and the compressed air passes through the annular gap 13 in turn And the ring tapered gap 16, and spray to the second valve 4 along the ring tapered gap 16, but, because the second valve 4 is in the closed state, the compressed air will be forced into the oil drum, so that the oil drum will form In a positive pressure environment, with the continuous discharge of compressed air, the aviation kerosene in the oil barrel will be continuously squeezed out of the oil barrel through the conduit under high pressure, thus realizing the purpose of continuous oil discharge.
实施例中的方案并非用以限制本实用新型的专利保护范围,凡未脱离本实用新型所为的等效实施或变更,均包含于本案的专利范围中。The schemes in the embodiments are not intended to limit the patent protection scope of the present utility model, and all equivalent implementations or changes that do not deviate from the utility model are included in the patent scope of the present case.
Claims (5)
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| CN201520926478.7U CN205117838U (en) | 2015-11-18 | 2015-11-18 | Pneumatics drive formula liquid suction device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN114593095A (en) * | 2022-03-29 | 2022-06-07 | 青岛景天艾尔科技有限公司 | A reversible aerodynamic pump |
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| CN114593095A (en) * | 2022-03-29 | 2022-06-07 | 青岛景天艾尔科技有限公司 | A reversible aerodynamic pump |
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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: AECC SHENYANG LIMING AERO-ENGINE Co.,Ltd. Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Aecc Shenyang Liming Aero Engine Co., Ltd. |
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