WO2016127702A1 - 一种基于多层级管式衰减单元的压缩机进气消声器 - Google Patents

一种基于多层级管式衰减单元的压缩机进气消声器 Download PDF

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WO2016127702A1
WO2016127702A1 PCT/CN2015/097265 CN2015097265W WO2016127702A1 WO 2016127702 A1 WO2016127702 A1 WO 2016127702A1 CN 2015097265 W CN2015097265 W CN 2015097265W WO 2016127702 A1 WO2016127702 A1 WO 2016127702A1
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intake
compressor
muffler
expansion chamber
port
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PCT/CN2015/097265
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English (en)
French (fr)
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耿爱农
陈威龙
阮勤江
陈君立
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浙江鸿友压缩机制造有限公司
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Publication of WO2016127702A1 publication Critical patent/WO2016127702A1/zh

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00

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  • the invention belongs to the technical field of compressors, and relates to a compressor intake noise elimination device, in particular to an air compressor intake elimination device with a multi-layer tubular attenuation unit based on a capacitive anti-sounding composite impedance silencing principle. Sound device.
  • this paper proposes a compressor intake muffler based on the multi-layer tubular attenuating unit, which aims to effectively reduce the intake noise of the compressor.
  • the object of the present invention is achieved by a compressor intake muffler based on a multi-layer tubular attenuating unit, characterized in that the muffler comprises at least two intake expansion chambers, and each intake expansion chamber is connected in series Or / and the parallel structure are interconnected, at least one of the intake expansion chamber is provided with an intake muffler unit, the intake muffler tube includes an intake port and an outlet port, and the gas working medium of the compressor can be advanced The air port and the air outlet port flow in or out and pulsate.
  • the above is provided with an intake expansion chamber of the intake muffler unit, and an intake port of the intake muffler communicates with the upper intake expansion chamber or the filter chamber of the compressor.
  • the air inlet expansion chamber of the intake muffling tube unit is disposed above, and the air outlet port of the intake muffler tube is disposed adjacent to the wall of the air inlet expansion chamber.
  • the two intake air expansion chambers in the above-mentioned muffler have a spatially dislocated layout of the intake port of the intake silencer tube of the upper intake air expansion chamber and the intake port of the intake silencer tube of the lower intake air expansion chamber.
  • the above muffler is used in a two-cylinder air compressor and is arranged in the middle of two cylinders of the compressor.
  • the advantage of the present invention over the prior art is that a multi-stage air intake muffler including a tube type muffling unit is used, and the air outlet port of the small flow cross section of the intake muffler tube faces the huge space of the expansion chamber, especially The outlet port is disposed adjacent to the wall of the inlet expansion chamber, thereby obtaining a very small echo reflection coefficient, thereby greatly reducing the chance of sound being reflected back from the compressor filter chamber to the outside atmosphere, thereby effectively reducing the compressor's progress. Gas noise.
  • FIG. 1 is a cross-sectional view of a compressor intake muffler based on a multi-layer tubular attenuating unit of the present invention
  • Figure 2 is a cross-sectional view of the compressor intake muffler of the present invention shown in Figure 1;
  • FIG. 3 is an isometric cross-sectional view of a compressor intake muffler based on a multi-stage tubular attenuating unit for use in a two-cylinder compressor;
  • Figure 4 is a cross-sectional view of the compressor intake muffler of the present invention shown in Figure 3.
  • a compressor intake muffler based on a multi-layer tubular attenuating unit comprising at least two intake expansion chambers 1, each of which is interconnected by a series or/and a parallel structure, at least one intake
  • the expansion chamber 1 is provided with an intake muffler 2 unit, the intake muffler 2 includes an intake port 2a and an outlet port 2b, and the gas working fluid of the compressor can flow in and out from the intake port 2a and the outlet port 2b.
  • the present invention is provided with an intake muffling tube 2, since the dimension of the outlet port 2b is much smaller than the spatial volume of the expansion chamber 1, thereby greatly reducing the echo reflection coefficient, in other words, when the gas pulsation is generated
  • the intake muffler 2 is a hollow tube structure, which can be a circular hollow tube or other shaped hollow tubes.
  • the working fluid can flow along the tunnel in the pipe; of course, since the compressor is basically intermittent exhaust gas, gas pulsation is inevitably generated, and this pulsation is also the source of the intake noise, and the inside of the intake muffler 2
  • the gas working fluid will have a phenomenon of reciprocating pulsation, that is, the flow of gas flowing through the inlet port 2a is not necessarily the flow of the intake air, but there is also a certain so-called back-spraying phenomenon, and the same phenomenon also exists.
  • the air outlet port 2b of the intake muffler 2 is provided. It is to be noted that the intake expansion chamber 1 of the unit of the intake muffler 2 is provided, and the intake port 2a of the intake muffler 2 communicates with the upper intake expansion chamber 1 or the filter chamber 3 of the communication compressor.
  • the intake expansion chamber 1 provided with the unit of the intake muffler 2 is disposed adjacent to the outlet port 2a of the intake muffler 2
  • the cavity wall 1a is arranged (as shown in Fig. 1 to Fig. 2), so that the echo reflection coefficient will be smaller, that is, the noise cancellation effect is better; it should be noted that the echo reflection coefficient here can be analogous to the heat transfer in the heat transfer.
  • the geometric angle coefficient it is obvious that the closer the outlet port 2a is to the cavity wall 1a, the smaller the echo reflection coefficient is, and the better the noise reduction effect is, but The premise is that the flow of gas cannot be prevented too much, otherwise it will adversely affect the gas output of the compressor.
  • the present invention is also capable of obtaining a better air intake muffling effect, and between the two intake expansion chambers 1 that are in communication with each other, the outlet port of the intake muffler 2 of the intake expansion chamber 1 of the upper stage can be connected.
  • 2b is spatially misaligned with the intake port 2a of the intake muffler 2 of the intake expansion chamber 1 of the next stage (as shown in FIGS. 1 to 2), which can also effectively reduce the echo reflection coefficient, thereby obtaining Better noise reduction.
  • the present invention is applied to a two-cylinder type air compressor (as shown in Figures 3 and 4), in which case the intake muffler can be placed between the two cylinders 4 of the compressor (see Figure 3), such that
  • the intake muffler is more compact, and it is more advantageous to use the two cylinders 4 of the compressor to alternately perform intake and compression, so that the pulsation of the gas in the intake muffler is more uniform and the pulsation amplitude is smaller. That is, the intake noise of the compressor will be lower.
  • the advantage of the present invention over the prior art is that a multi-stage intake muffler including a tubular muffling unit is used, and the outlet port 2b of the smaller flow section of the intake muffler 2 faces the intake expansion chamber 1 A large space, in particular, the outlet port 2b is disposed adjacent to the chamber wall 1a of the intake expansion chamber 1, and further, the intake of the upper-stage intake expansion chamber 1 between the two intake expansion chambers 1 that are in communication with each other is eliminated.
  • the outlet port 2b of the sound tube 2 is spatially displaced from the intake port 2a of the intake muffler 2 of the intake expansion chamber 1 of the next stage, thereby obtaining an extremely small echo reflection coefficient, thereby greatly reducing the number of The sound is reflected from the compressor filter chamber back to the outside atmosphere, so the intake noise of the compressor can be effectively reduced.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)
  • Exhaust Silencers (AREA)

Abstract

一种基于多层级管式衰减单元的压缩机进气消声器,包含有至少两个进气膨胀腔(1),各进气膨胀腔(1)之间采用串联或/和并联相互联系,至少有一个进气膨胀腔(1)设置有进气消声管(2),进气消声管(2)包含有进气端口(2a)和出气端口(2b),压缩机的气体工质可从进气端口(2a)和出气端口(2b)进出流动或往返脉动。利用进气消声管(2)较小流通截面的出气端口(2b)面对膨胀腔(1)的巨大空间,尤其让出气端口(2b)紧邻所在进气膨胀腔(1)的腔壁(1a)设置,获得极小的回声反射系数,极大地减少了声音从压缩机过滤腔(3)反射回外界大气的机会,可有效减少压缩机的进气噪声。

Description

一种基于多层级管式衰减单元的压缩机进气消声器 技术领域
本发明属于压缩机技术领域,涉及一种压缩机进气消声装置,具体地说涉及一种基于容抗消声复合阻抗消声原理的具有多层级管式衰减单元的空气压缩机进气消声装置。
背景技术
现有空气压缩机工作时均会产生令人烦厌的噪声,众所周知在这些噪声构成当中又以进气噪声的贡献值最大。当前,消减进气噪声主要依赖进气消声器,其原理是采用阻抗法和容抗法对压缩机吸气过程派生的气体脉动噪声进行消减,前者通过阻挡、阻尼、阻滞和吸收等多种途径消减声音的能量,后者则主要利用足够的空间体积通过使声音在其内作多次折返和反射,以此实现衰减噪声的能量。现有空气压缩机产品中,所使用的消声器往往与空气滤清器一体设计与制作,由于用于消声功能的膨胀腔太小以及消声单元的结构设计及布局不够合理,致使传统的消声器达不到理想的消声效果。
发明内容
针对现有技术中消声器消声效果不好的缺陷,本文提出一种基于多层级管式衰减单元的压缩机进气消声器,目的在于有效减少压缩机的进气噪声。
本发明的目的是这样实现的:一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:该消声器包含有至少两个进气膨胀腔,各进气膨胀腔之间采用串联或/和并联架构相互联系,至少有一个进气膨胀腔设置有进气消声管单元,所述进气消声管包含有进气端口和出气端口,压缩机的气体工质可从进 气端口和出气端口进出流动或往返脉动。
上述设置有进气消声管单元的进气膨胀腔,其进气消声管的进气端口连通上级进气膨胀腔或连通压缩机的过滤腔。
上述设置有进气消声管单元的进气膨胀腔,其进气消声管的出气端口紧邻所在进气膨胀腔的腔壁设置。
上述的消声器中相互联系的两个进气膨胀腔,其上级进气膨胀腔进气消声管的出气端口与下级进气膨胀腔进气消声管的进气端口呈空间错位布局。
上述的消声器使用于双缸空气压缩机,并布局在压缩机的两个气缸中间。
本发明相比现有技术突出的优点是:采用包含有管式消声单元的多层级进气消声器,利用进气消声管较小流通截面的出气端口面对膨胀腔的巨大空间,尤其让该出气端口紧邻所在进气膨胀腔的腔壁设置,由此获得极小的回声反射系数,因此极大地减少了声音从压缩机过滤腔反射回外界大气的机会,故可有效减少压缩机的进气噪声。
附图说明
图1是本发明一种基于多层级管式衰减单元的压缩机进气消声器的轴测剖视图;
图2是图1所示实施例本发明压缩机进气消声器的剖视图;
图3是本发明一种基于多层级管式衰减单元的压缩机进气消声器使用于双缸压缩机的轴测剖视图;
图4是图3所示本发明压缩机进气消声器的剖视图。
具体实施方式
下面以具体实施例对本发明作进一步描述,参见图1-4:
一种基于多层级管式衰减单元的压缩机进气消声器,包含有至少两个进气膨胀腔1,各进气膨胀腔1之间采用串联或/和并联架构相互联系,至少有一个进气膨胀腔1设置有进气消声管2单元,所述进气消声管2包含有进气端口2a和出气端口2b,压缩机的气体工质可从进气端口2a和出气端口2b进出流动或往返脉动;本发明设置有进气消声管2,由于其出气端口2b的尺度相对于膨胀腔1的空间体积狭小很多,由此极大地减少了回声反射系数,换句话说当气体脉动产生的声音在进气膨胀腔1内来回震荡反射并衰减时,其从出气端口2b进入并沿进气消声管2内部反射折回上级进气消声管2或反射折回压缩机过滤腔3的概率将大大减少,故能有效减少压缩机的进气噪声;需要说明的是,进气消声管2为空心管结构,可以是圆形空心管也可以是其他异形空心管,当压缩机进气时气体工质可以沿着管内的孔道进行流动;当然,由于压缩机基本上为间歇式排气,因此必然产生气体脉动,而这个脉动也是产生进气噪声的根源,此时进气消声管2内部的气体工质将会出现往返脉动的现象,亦即意味着流经进气端口2a的气体其流动并不一定是进气流动,而是也存在一定的所谓反喷现象,同样的现象也存在于进气消声管2的出气端口2b。需要指出的是,设置有进气消声管2单元的进气膨胀腔1,其进气消声管2的进气端口2a连通上级进气膨胀腔1或连通压缩机的过滤腔3。
本发明为了获得更好的进气消声效果,在设置有进气消声管2单元的进气膨胀腔1,让其进气消声管2的出气端口2a紧邻所在进气膨胀腔1的腔壁1a设置(如图1至图2所示),这样回声反射系数将更小,亦即消声效果更佳;需要说明的是,这里的回声反射系数可以类比传热学中辐射传热的几何角系数,显然出气端口2a越靠近腔壁1a其回声反射系数越小,消声效果也就越佳,但其 前提是不能过大妨碍气体的流动,否则将对压缩机的气体输出量产生不利影响。
本发明同样为了获得更好的进气消声效果,可以在相互联系的两个进气膨胀腔1之间,让其上一级的进气膨胀腔1的进气消声管2的出气端口2b与其下一级的进气膨胀腔1的进气消声管2的进气端口2a呈空间错位布局(如图1至图2所示),这样也能有效减少回声反射系数,由此获得更好的消声效果。
特别地,本发明使用于双缸型式的空气压缩机(如图3和图4所示),此时进气消声器可以布局在压缩机的两个气缸4之间(参见图3),这样一来不仅使得进气消声器更加紧凑,更为有利的是可以利用压缩机的两个气缸4交替实施进气和压缩,从而使得进气消声器内气体的脉动更趋均匀以及脉动幅值更小,亦即压缩机的进气噪声将会更低。
本发明相比现有技术突出的优点是:采用包含有管式消声单元的多层级进气消声器,利用进气消声管2较小流通截面的出气端口2b面对进气膨胀腔1的巨大空间,尤其让该出气端口2b紧邻所在进气膨胀腔1的腔壁1a设置,进一步,让相互联系的两个进气膨胀腔1之间的上一级进气膨胀腔1的进气消声管2的出气端口2b与其下一级的进气膨胀腔1的进气消声管2的进气端口2a呈空间错位的布局,由此获得极小的回声反射系数,因此极大地减少了声音从压缩机过滤腔反射回外界大气的机会,故可有效减少压缩机的进气噪声。
上述实施例仅为本发明的较佳实施例之一,并非依此限制本发明的保护范围,故:凡依本发明的结构、形状、原理所做的各种等效变化,均应涵盖于本发明的保护范围之内。

Claims (5)

  1. 一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:该消声器包含有至少两个进气膨胀腔,各进气膨胀腔之间采用串联或/和并联架构相互联系,至少有一个进气膨胀腔设置有进气消声管单元,所述进气消声管包含有进气端口和出气端口,压缩机的气体工质可从进气端口和出气端口进出流动或往返脉动。
  2. 如权利要求1所述的一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:设置有进气消声管单元的进气膨胀腔,其进气消声管的进气端口连通上级进气膨胀腔或连通压缩机的过滤腔。
  3. 如权利要求1所述的一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:设置有进气消声管单元的进气膨胀腔,其进气消声管的出气端口紧邻所在进气膨胀腔的腔壁设置。
  4. 如权利要求1所述的一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:相互联系的两个进气膨胀腔,其上级进气膨胀腔进气消声管的出气端口与下级进气膨胀腔进气消声管的进气端口呈空间错位布局。
  5. 如权利要求1至4任意一项所述的一种基于多层级管式衰减单元的压缩机进气消声器,其特征在于:所述进气消声器使用于双缸空气压缩机,并布局在压缩机的两个气缸中间。
PCT/CN2015/097265 2015-02-14 2015-12-14 一种基于多层级管式衰减单元的压缩机进气消声器 WO2016127702A1 (zh)

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WO2024073538A1 (en) * 2022-09-30 2024-04-04 Gast Manufacturing, Inc. Sound reduction device for rocking piston compressors

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CN104612941A (zh) * 2015-02-14 2015-05-13 浙江鸿友压缩机制造有限公司 一种基于多层级管式衰减单元的压缩机进气消声器
CN109356818B (zh) * 2018-11-30 2024-03-19 浙江鸿友压缩机制造有限公司 一种空气压缩机进气消声器
WO2020223293A1 (en) * 2019-04-29 2020-11-05 Gast Manufacturing, Inc. Sound reduction device for rocking piston pumps and compressors

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