CN114962356B - Multi-stage energized jet pump - Google Patents
Multi-stage energized jet pump Download PDFInfo
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- CN114962356B CN114962356B CN202210783698.3A CN202210783698A CN114962356B CN 114962356 B CN114962356 B CN 114962356B CN 202210783698 A CN202210783698 A CN 202210783698A CN 114962356 B CN114962356 B CN 114962356B
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
- F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
- F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
- F04F5/46—Arrangements of nozzles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
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Abstract
Description
技术领域Technical field
本发明涉及射流泵技术领域,更具体的说是涉及一种多级加能的射流泵。The present invention relates to the technical field of jet pumps, and more specifically to a multi-stage energized jet pump.
背景技术Background technique
目前,射流泵由于没有运动的工作元件,结构简单,工作可靠,无泄漏,因此被广泛使用。At present, jet pumps are widely used because they have no moving working components, simple structure, reliable operation and no leakage.
但是,射流泵通常采用截面为线性渐缩型的喷嘴,没有加能的结构设置,导致其喷嘴流速低,且在进气口压力不够的时候会出现射流泵喷嘴流速小,使射流泵的工作效率降低的问题。However, jet pumps usually use nozzles with a linearly tapered cross section and no energy-adding structural settings, resulting in low flow rates in the nozzles. When the air inlet pressure is insufficient, the flow rate in the jet pump nozzles will be low, making the jet pump inoperable. The problem of reduced efficiency.
因此,如何提供一种对射流泵喷嘴流速提升的射流泵是本领域技术人员亟需解决的问题。Therefore, how to provide a jet pump that increases the flow rate of the jet pump nozzle is an urgent problem that those skilled in the art need to solve.
发明内容Contents of the invention
有鉴于此,本发明提供了一种多级加能的射流泵,旨在解决上述背景技术中的问题,实现对射流泵喷嘴流速的提升。In view of this, the present invention provides a multi-stage energized jet pump, aiming to solve the problems in the above background technology and achieve an increase in the flow rate of the jet pump nozzle.
为了实现上述目的,本发明采用如下技术方案:In order to achieve the above objects, the present invention adopts the following technical solutions:
一种多级加能的射流泵,包括:A multi-stage energized jet pump, including:
吸入室;suction chamber;
高压流体入口管,所述高压流体入口管与所述吸入室的第一端连接,所述高压流体入口管与所述吸入室的腔体连通,所述高压流体入口管的一端伸入至所述吸入室的腔体内;A high-pressure fluid inlet pipe, the high-pressure fluid inlet pipe is connected to the first end of the suction chamber, the high-pressure fluid inlet pipe is connected to the cavity of the suction chamber, and one end of the high-pressure fluid inlet pipe extends into the inside the cavity of the suction chamber;
中压流体出口管,所述中压流体出口管与所述吸入室的第二端连接,所述中压流体出口管与所述吸入室的腔体连通;a medium-pressure fluid outlet pipe, the medium-pressure fluid outlet pipe is connected to the second end of the suction chamber, and the medium-pressure fluid outlet pipe is connected to the cavity of the suction chamber;
低压流体入口管,所述低压流体入口管与所述吸入室的侧壁连接,所述低压流体入口管与所述吸入室的腔体连通;a low-pressure fluid inlet pipe, the low-pressure fluid inlet pipe is connected to the side wall of the suction chamber, and the low-pressure fluid inlet pipe is connected to the cavity of the suction chamber;
喷嘴,所述喷嘴与所述高压流体入口管伸入所述吸入室的一端连接,所述喷嘴由多个缓冲腔依次连接成型,多个所述缓冲腔的容积由靠近所述高压流体入口管向中压流体出口管方向依次减小,且远离所述高压流体入口管的缓冲腔的出口截面积小于靠近所述高压流体入口管的缓冲腔的出口截面积。The nozzle is connected to one end of the high-pressure fluid inlet pipe extending into the suction chamber. The nozzle is formed by a plurality of buffer chambers connected in sequence. The volumes of the plurality of buffer chambers are formed close to the high-pressure fluid inlet pipe. It gradually decreases toward the medium-pressure fluid outlet pipe, and the outlet cross-sectional area of the buffer chamber away from the high-pressure fluid inlet pipe is smaller than the outlet cross-sectional area of the buffer chamber close to the high-pressure fluid inlet pipe.
进一步地,所述高压流体入口管由远离所述吸入室的一端向靠近所述吸入室的一端为渐缩型结构。Furthermore, the high-pressure fluid inlet pipe has a tapered structure from an end far away from the suction chamber to an end close to the suction chamber.
进一步地,所述中压流体出口管包括直臂管和扩张管,所述扩张管的小口端与所述直臂管的一端连接,所述直臂管的另一端与所述吸入室连通。Further, the medium-pressure fluid outlet pipe includes a straight arm tube and an expansion tube. The small end of the expansion tube is connected to one end of the straight arm tube, and the other end of the straight arm tube is connected to the suction chamber.
进一步地,所述直臂管靠近所述吸入室的一端伸入至所述吸入室内。Further, one end of the straight arm tube close to the suction chamber extends into the suction chamber.
进一步地,所述中压流体出口管和高压流体入口管为同轴设置。Further, the medium-pressure fluid outlet pipe and the high-pressure fluid inlet pipe are coaxially arranged.
进一步地,所述喷嘴沿其轴线呈旋转体结构。Further, the nozzle has a rotating body structure along its axis.
进一步地,相邻两个所述缓冲腔之间通过连接管连通,且远离所述高压流体入口管的连接管直径小于靠近所述高压流体入口管的连接管直径。Further, two adjacent buffer chambers are connected through connecting pipes, and the diameter of the connecting pipe far away from the high-pressure fluid inlet pipe is smaller than the diameter of the connecting pipe close to the high-pressure fluid inlet pipe.
进一步地,所述连接管为渐缩管,且所述渐缩管的小口端朝向远离所述高压流体入口管的方向。Further, the connecting pipe is a reducer tube, and the small end of the reducer tube faces a direction away from the high-pressure fluid inlet pipe.
经由上述的技术方案可知,与现有技术相比,本发明公开提供了一种多级加能的射流泵,通过喷嘴由多个缓冲腔依次连接成型,且缓冲腔的容积由靠近高压流体入口管向中压流体出口管方向依次减小,相邻的缓冲腔之间能够实现对流体的加能效果,进而使流体流经喷嘴时流速增加,提高了射流泵的工作效率。It can be seen from the above technical solutions that, compared with the prior art, the present invention provides a multi-stage energized jet pump, which is formed by multiple buffer chambers connected in sequence through a nozzle, and the volume of the buffer chamber is increased from close to the high-pressure fluid inlet. The pipes gradually decrease in the direction of the medium-pressure fluid outlet pipe, and the adjacent buffer cavities can achieve an energizing effect on the fluid, thereby increasing the flow rate of the fluid when it flows through the nozzle, thereby improving the working efficiency of the jet pump.
附图说明Description of the drawings
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据提供的附图获得其他的附图。In order to explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the drawings needed to be used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings in the following description are only These are embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on the provided drawings without exerting creative efforts.
图1为本发明提供的一种多级加能的射流泵的结构示意图。Figure 1 is a schematic structural diagram of a multi-stage energized jet pump provided by the present invention.
图2为本发明提供的另一种多级加能的射流泵的结构示意图。Figure 2 is a schematic structural diagram of another multi-stage energized jet pump provided by the present invention.
其中:1为吸入室;2为高压流体入口管;3为中压流体出口管;31为直臂管;32为扩张管;4为低压流体入口管;5为喷嘴;6为缓冲腔;7为连接管。Among them: 1 is the suction chamber; 2 is the high-pressure fluid inlet pipe; 3 is the medium-pressure fluid outlet pipe; 31 is the straight arm pipe; 32 is the expansion pipe; 4 is the low-pressure fluid inlet pipe; 5 is the nozzle; 6 is the buffer chamber; 7 For connecting pipe.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts fall within the scope of protection of the present invention.
实施例1Example 1
参见图1,本发明实施例公开了一种多级加能的射流泵,包括:Referring to Figure 1, an embodiment of the present invention discloses a multi-stage energized jet pump, including:
吸入室1;suction chamber 1;
高压流体入口管2,高压流体入口管2与吸入室1的第一端连接,高压流体入口管2与吸入室1的腔体连通,高压流体入口管2的一端伸入至吸入室1的腔体内;The high-pressure fluid inlet pipe 2 is connected to the first end of the suction chamber 1. The high-pressure fluid inlet pipe 2 is connected to the cavity of the suction chamber 1. One end of the high-pressure fluid inlet pipe 2 extends into the cavity of the suction chamber 1. in vivo;
中压流体出口管3,中压流体出口管3与吸入室1的第二端连接,中压流体出口管3与吸入室1的腔体连通;The medium-pressure fluid outlet pipe 3 is connected to the second end of the suction chamber 1, and the medium-pressure fluid outlet pipe 3 is connected to the cavity of the suction chamber 1;
低压流体入口管4,低压流体入口管4与吸入室1的侧壁连接,低压流体入口管4与吸入室1的腔体连通;Low-pressure fluid inlet pipe 4, the low-pressure fluid inlet pipe 4 is connected with the side wall of the suction chamber 1, and the low-pressure fluid inlet pipe 4 is connected with the cavity of the suction chamber 1;
喷嘴5,喷嘴5与高压流体入口管2伸入吸入室1的一端连接,喷嘴5由多个缓冲腔6依次连接成型,多个缓冲腔6的容积由靠近高压流体入口管2向中压流体出口管3方向依次减小,且远离高压流体入口管2的缓冲腔6的出口截面积小于靠近高压流体入口管2的缓冲腔6的出口截面积。The nozzle 5 is connected to one end of the high-pressure fluid inlet pipe 2 extending into the suction chamber 1. The nozzle 5 is formed by a plurality of buffer chambers 6 connected in sequence. The volumes of the plurality of buffer chambers 6 change from close to the high-pressure fluid inlet pipe 2 to the medium-pressure fluid. The direction of the outlet pipe 3 decreases successively, and the outlet cross-sectional area of the buffer chamber 6 far away from the high-pressure fluid inlet pipe 2 is smaller than the outlet cross-sectional area of the buffer chamber 6 close to the high-pressure fluid inlet pipe 2 .
其中,在本实施例中,优选地,缓冲腔6设有三个,三个缓冲腔6的截面积均为矩形结构,即截面积由靠近高压流体入口管2到中压流体出口管3的缓冲腔6的截面积分别为S1、S2、S3,且S1>S2>S3,相邻的缓冲腔6通过直角过渡,当流体从第一个缓冲腔6流到第二个缓冲腔6时,过流面积在减小,在第二个缓冲腔6处的流速大于第一个缓冲腔6处的流速,同时,流体从高压流体入口管2进入至截面积为S1的缓冲腔6时,流体在第一个缓冲腔6内的压力减小,在压力差的作用下,由高压流体入口管2流入第一个缓冲腔6的流量在增加,同理,由第二个缓冲腔6道第三个缓冲腔6也遵循由第一个缓冲腔6到第二个缓冲腔6的原理,进而使得进入射流泵的流量在不断的增加,最终使得由喷嘴5喷出流体的速度在增加,使流体受到多级加能的作用,提高了射流泵喷嘴5的流速。Among them, in this embodiment, preferably, there are three buffer chambers 6, and the cross-sectional areas of the three buffer chambers 6 are all rectangular structures, that is, the cross-sectional areas range from the buffer near the high-pressure fluid inlet pipe 2 to the medium-pressure fluid outlet pipe 3. The cross-sectional areas of the chambers 6 are S1, S2, and S3 respectively, and S1>S2>S3. The adjacent buffer chambers 6 pass through a right-angle transition. When the fluid flows from the first buffer chamber 6 to the second buffer chamber 6, the flow The flow area is decreasing, and the flow velocity at the second buffer chamber 6 is greater than the flow velocity at the first buffer chamber 6. At the same time, when the fluid enters the buffer chamber 6 with a cross-sectional area of S1 from the high-pressure fluid inlet pipe 2, the fluid is The pressure in the first buffer chamber 6 decreases. Under the action of the pressure difference, the flow rate flowing from the high-pressure fluid inlet pipe 2 into the first buffer chamber 6 increases. In the same way, the flow rate from the second buffer chamber 6 to the third buffer chamber 6 increases. The buffer chambers 6 also follow the principle from the first buffer chamber 6 to the second buffer chamber 6, so that the flow rate entering the jet pump continues to increase, and ultimately the speed of the fluid ejected from the nozzle 5 increases, causing the fluid to Under the action of multi-stage energy addition, the flow rate of the jet pump nozzle 5 is increased.
在本实施例中,高压流体入口管2由远离吸入室1的一端向靠近吸入室1的一端为渐缩型结构,通过将高压流体入口管2沿流体的行径方向设置成逐渐收缩的结构,能够对流经高压流体入口管2的流体起到加速的作用。In this embodiment, the high-pressure fluid inlet pipe 2 has a tapered structure from the end far away from the suction chamber 1 to the end close to the suction chamber 1. By arranging the high-pressure fluid inlet pipe 2 into a gradually contracting structure along the path direction of the fluid, It can accelerate the fluid flowing through the high-pressure fluid inlet pipe 2 .
在本实施例中,优选地,中压流体出口管3包括直臂管31和扩张管32,扩张管32的小口端与直臂管31的一端连接,直臂管31的另一端与吸入室1连通。直臂管31靠近吸入室1的一端伸入至吸入室1内。由喷嘴5喷出的高压流体与由低压流体入口管4喷入的低压流体进行混合,混合后的流体在直臂管31内进行再次混合形成中压流体,中压流体最终由扩张管32喷出。In this embodiment, preferably, the medium pressure fluid outlet pipe 3 includes a straight arm tube 31 and an expansion tube 32. The small end of the expansion tube 32 is connected to one end of the straight arm tube 31, and the other end of the straight arm tube 31 is connected to the suction chamber. 1 connected. One end of the straight arm tube 31 close to the suction chamber 1 extends into the suction chamber 1 . The high-pressure fluid sprayed from the nozzle 5 is mixed with the low-pressure fluid sprayed from the low-pressure fluid inlet pipe 4 . The mixed fluid is mixed again in the straight arm pipe 31 to form a medium-pressure fluid. The medium-pressure fluid is finally sprayed from the expansion tube 32 out.
在本实施例中,优选地,中压流体出口管3和高压流体入口管2为同轴设置。In this embodiment, preferably, the medium-pressure fluid outlet pipe 3 and the high-pressure fluid inlet pipe 2 are coaxially arranged.
在上述实施例中,喷嘴5沿其轴线呈旋转体结构。通过将喷嘴5设置成旋转体结构,能够使得由喷嘴5喷出的高压流体在各方向上的受力均衡,确保从喷嘴5喷出的高压流体方向沿喷嘴5的轴线向前运动。In the above embodiment, the nozzle 5 has a rotating body structure along its axis. By arranging the nozzle 5 into a rotary structure, the force on the high-pressure fluid ejected from the nozzle 5 can be balanced in all directions, ensuring that the direction of the high-pressure fluid ejected from the nozzle 5 moves forward along the axis of the nozzle 5 .
在上述实施例中,优选地,相邻两个缓冲腔6之间通过连接管7连通,且远离高压流体入口管2的连接管7直径小于靠近高压流体入口管2的连接管7直径。通过将第一个缓冲腔6和第二个缓冲腔6之间的连接管7的截面积大于第二个缓冲腔6和第三个缓冲腔6之间的连接管7的截面积,能够使得流体流经第二个缓冲腔6和第三个缓冲腔6之间的连接管7的流速大于流经第一个缓冲腔6和第二个缓冲腔6之间的连接管7的流速,以实现对流体的加能作用。In the above embodiment, preferably, two adjacent buffer chambers 6 are connected through connecting pipes 7 , and the diameter of the connecting pipe 7 far away from the high-pressure fluid inlet pipe 2 is smaller than the diameter of the connecting pipe 7 close to the high-pressure fluid inlet pipe 2 . By making the cross-sectional area of the connecting tube 7 between the first buffer chamber 6 and the second buffer chamber 6 larger than the cross-sectional area of the connecting tube 7 between the second buffer chamber 6 and the third buffer chamber 6, it can be achieved The flow rate of fluid flowing through the connecting pipe 7 between the second buffer chamber 6 and the third buffer chamber 6 is greater than the flow rate flowing through the connecting pipe 7 between the first buffer chamber 6 and the second buffer chamber 6, so that Achieve the energizing effect on the fluid.
根据本发明的一些实施例,连接管7为渐缩管,且渐缩管的小口端朝向远离高压流体入口管2的方向。通过将连接管7设置为渐缩管的结构,且连接管7的小口端朝向流体的流经方向,进而能够实现对流体的加能作用。According to some embodiments of the present invention, the connecting tube 7 is a tapered tube, and the small end of the tapered tube faces away from the high-pressure fluid inlet pipe 2 . By configuring the connecting tube 7 to have a tapered tube structure, and having the small end of the connecting tube 7 facing the flow direction of the fluid, the energizing effect on the fluid can be achieved.
实施例2Example 2
参见图2,本实施例所公开的多级加能的射流泵,与实施例1的区别仅在于,在本实施例中,缓冲腔6设置有两个,两个缓冲腔6的截面积均为梯形结构,使得相邻的两个缓冲腔6在容积变化过程中,变化速率比较缓慢,靠近高压流体入口管2的缓冲腔6容积大于靠近中压流体出口管3的缓冲腔6容积,即靠近高压流体入口管2的缓冲腔6的出口截面积大于靠近中压流体出口管3的缓冲腔6的出口的截面积,在流体流经喷嘴时,压力减小趋势是连续、缓慢的变化,在一定程度上减小流体对缓冲腔6的冲击作用。Referring to Figure 2, the only difference between the multi-stage energized jet pump disclosed in this embodiment and Embodiment 1 is that in this embodiment, two buffer cavities 6 are provided, and the cross-sectional areas of the two buffer cavities 6 are equal. It is a trapezoidal structure, so that the change rate of the two adjacent buffer chambers 6 is relatively slow during the volume change process. The volume of the buffer chamber 6 near the high-pressure fluid inlet pipe 2 is larger than the volume of the buffer chamber 6 near the medium-pressure fluid outlet pipe 3, that is, The cross-sectional area of the outlet of the buffer chamber 6 close to the high-pressure fluid inlet pipe 2 is larger than the cross-sectional area of the outlet of the buffer chamber 6 close to the medium-pressure fluid outlet pipe 3. When the fluid flows through the nozzle, the pressure decrease trend is a continuous and slow change. The impact of fluid on the buffer chamber 6 is reduced to a certain extent.
本说明书中各个实施例采用递进的方式描述,每个实施例重点说明的都是与其他实施例的不同之处,各个实施例之间相同相似部分互相参见即可。对于实施例公开的装置而言,由于其与实施例公开的方法相对应,所以描述的比较简单,相关之处参见方法部分说明即可。Each embodiment in this specification is described in a progressive manner. Each embodiment focuses on its differences from other embodiments. The same and similar parts between the various embodiments can be referred to each other. As for the device disclosed in the embodiment, since it corresponds to the method disclosed in the embodiment, the description is relatively simple. For relevant details, please refer to the description in the method section.
对所公开的实施例的上述说明,使本领域专业技术人员能够实现或使用本发明。对这些实施例的多种修改对本领域的专业技术人员来说将是显而易见的,本文中所定义的一般原理可以在不脱离本发明的精神或范围的情况下,在其它实施例中实现。因此,本发明将不会被限制于本文所示的这些实施例,而是要符合与本文所公开的原理和新颖特点相一致的最宽的范围。The above description of the disclosed embodiments enables those skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be practiced in other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (7)
Priority Applications (1)
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Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2375180A (en) * | 1943-11-08 | 1945-05-01 | Vigo George | Apparatus for jet propulsive and other purposes |
| US2548563A (en) * | 1947-07-22 | 1951-04-10 | Smith Ellis | Air-cooled exhaust silencer |
| DE4011218A1 (en) * | 1990-04-06 | 1991-10-10 | Kruse Franz Josef | Multiple ejector pump assembly - has series of nozzles with inserted rod to create annular gaps |
| CN101054887A (en) * | 2006-04-13 | 2007-10-17 | 宋家雄 | Drilling bit installed with self-inspired pulse resonance jet nozzle |
| JP2011220127A (en) * | 2010-04-05 | 2011-11-04 | Denso Corp | Exhaust gas circulation device |
| CN102865256A (en) * | 2012-09-19 | 2013-01-09 | 上海大学 | Self-oscillation pulsed liquid-gas jet pump |
| CN105772265A (en) * | 2016-05-25 | 2016-07-20 | 太原理工大学 | Dual-fluid reflection convection type micro-mist dust suppression nozzle |
| CN205654618U (en) * | 2016-01-08 | 2016-10-19 | 无锡市大业通用设备厂 | Steam -jet ejector water pump |
| CN207126700U (en) * | 2017-04-24 | 2018-03-23 | 美的集团股份有限公司 | nozzle and injector |
| CN211398085U (en) * | 2019-12-31 | 2020-09-01 | 广州泰格测控技术有限公司 | Gas sampling jet pump |
| KR20210084113A (en) * | 2019-12-27 | 2021-07-07 | 주식회사 케이씨텍 | Nozzle and injector comprising the same |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8479878B2 (en) * | 2008-09-25 | 2013-07-09 | Parallaxial Innovation LLC | Channeling gas flow tube |
| CN110180693B (en) * | 2019-07-24 | 2019-10-22 | 常州江苏大学工程技术研究院 | An induction electrostatic atomization nozzle |
-
2022
- 2022-07-05 CN CN202210783698.3A patent/CN114962356B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2375180A (en) * | 1943-11-08 | 1945-05-01 | Vigo George | Apparatus for jet propulsive and other purposes |
| US2548563A (en) * | 1947-07-22 | 1951-04-10 | Smith Ellis | Air-cooled exhaust silencer |
| DE4011218A1 (en) * | 1990-04-06 | 1991-10-10 | Kruse Franz Josef | Multiple ejector pump assembly - has series of nozzles with inserted rod to create annular gaps |
| CN101054887A (en) * | 2006-04-13 | 2007-10-17 | 宋家雄 | Drilling bit installed with self-inspired pulse resonance jet nozzle |
| JP2011220127A (en) * | 2010-04-05 | 2011-11-04 | Denso Corp | Exhaust gas circulation device |
| CN102865256A (en) * | 2012-09-19 | 2013-01-09 | 上海大学 | Self-oscillation pulsed liquid-gas jet pump |
| CN205654618U (en) * | 2016-01-08 | 2016-10-19 | 无锡市大业通用设备厂 | Steam -jet ejector water pump |
| CN105772265A (en) * | 2016-05-25 | 2016-07-20 | 太原理工大学 | Dual-fluid reflection convection type micro-mist dust suppression nozzle |
| CN207126700U (en) * | 2017-04-24 | 2018-03-23 | 美的集团股份有限公司 | nozzle and injector |
| KR20210084113A (en) * | 2019-12-27 | 2021-07-07 | 주식회사 케이씨텍 | Nozzle and injector comprising the same |
| CN211398085U (en) * | 2019-12-31 | 2020-09-01 | 广州泰格测控技术有限公司 | Gas sampling jet pump |
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| CN114962356A (en) | 2022-08-30 |
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