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CN202468498U - Axial-flow type jet flow air wave supercharger - Google Patents

Axial-flow type jet flow air wave supercharger Download PDF

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Publication number
CN202468498U
CN202468498U CN2012201155970U CN201220115597U CN202468498U CN 202468498 U CN202468498 U CN 202468498U CN 2012201155970 U CN2012201155970 U CN 2012201155970U CN 201220115597 U CN201220115597 U CN 201220115597U CN 202468498 U CN202468498 U CN 202468498U
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pressure
rotary drum
conduit
angle
drum
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胡大鹏
邹久朋
代玉强
刘培启
朱彻
赵文静
赵家权
刘凤霞
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Dalian University of Technology
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Dalian University of Technology
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Abstract

An axial-flow type jet flow air wave supercharger realizes the energy exchange between high-pressure and low-pressure gases through the operation of pressure wave, avoids the mixing diffusion energy loss, and has the advantages of higher isentropic efficiency, low rotational speed and the capability of operation with liquid. A rectangular pressure oscillation tube slotted channel with a variable cross section is adopted, the inlet loss and flowing loss of jet flow are reduced; a pressure balancing opening is arranged in the supercharger, so as to balance performances with different pressure ratios; a diffusion air director is arranged at a compression outflow port to effectively convert the kinetic energy of the airflow; and the axial-flow type jet flow air wave supercharger makes full use of the pressure energy in the manufacturing process and stratigraphic pressure energy of natural gas and the like, and is an efficient equipment choice for the effective utilization of pressure energy.

Description

轴流式射流气波增压器Axial jet air wave supercharger

技术领域 technical field

本实用新型轴流式射流气波增压器属于以气体射流实现增压的技术领域。  The utility model relates to an axial flow jet gas wave supercharger, which belongs to the technical field of realizing supercharging by gas jet flow. the

背景技术 Background technique

气体压力能的综合利用具有重要的经济效益和社会效益。在利用高压气体膨胀做功对低压气体进行压缩方面,常用的设备有膨胀机-压缩机组、涡轮增压器和喷射器。透平和涡轮增压器依靠叶轮传递能量,结构复杂,旋转速度高且难以带液操作。喷射器虽然具有无转动件、结构简单等特点,但其效率很低,只有百分之十几。  The comprehensive utilization of gas pressure energy has important economic and social benefits. In terms of using high-pressure gas expansion to do work to compress low-pressure gas, commonly used equipment includes expander-compressor units, turbochargers and ejectors. Turbines and turbochargers rely on impellers to transfer energy, have complex structures, high rotation speeds and are difficult to operate with liquid. Although the injector has the characteristics of no rotating parts and simple structure, its efficiency is very low, only more than ten percent. the

实用新型内容 Utility model content

本实用新型提供一种高效、低转速并可带液操作的气体射流增压装置-轴流式射流气波增压器。  The utility model provides a high-efficiency, low-speed gas jet supercharging device which can be operated with liquid-an axial flow jet gas wave supercharger. the

本实用新型增压器中,高压和低压两路气体直接接触,依靠气体压力波传递高压气体脉冲膨胀功的能量,直接对低压气体进行压缩,可得到一股居中压力的气体。与常规射流混合压缩不同,上述过程基本无两路气体的掺混,因此射流能量损失小,压缩效率高。  In the supercharger of the utility model, the high-pressure and low-pressure two-way gases are in direct contact, relying on the gas pressure wave to transfer the energy of the high-pressure gas pulse expansion work, and directly compress the low-pressure gas to obtain a gas with a middle pressure. Different from the conventional jet mixing and compression, the above process basically does not mix the two-way gas, so the jet energy loss is small and the compression efficiency is high. the

本实用新型提供了一种结构相对简单、高效、转速低、维护方便、可带液运行、处理量弹性大、介质适应性强的气体射流增压器,满足油、气田开采和其他场合下,对带压气体压力能高效利用的需求。  The utility model provides a gas jet supercharger with relatively simple structure, high efficiency, low rotating speed, convenient maintenance, operation with liquid, large processing capacity flexibility, and strong medium adaptability, which meets the needs of oil and gas field exploitation and other occasions. The need for efficient utilization of pressurized gas pressure. the

本实用新型所采取的技术解决方案为:  The technical solution that the utility model takes is:

本实用新型是一种依靠压力气体依次射流,做出非定常膨胀功而增压的轴流式射流气波增压器,主要由圆柱形、圆台形、或者圆柱接圆台形的转鼓9,转 鼓外套11,多条作为压力振荡管的槽道10,主轴18,左机体4,右机体16,外壳12,高压射流喷嘴2,低压气引射口8,中压出流口13,均压口20,高压进气口1和高压缓冲腔3,低压进气口7和低压缓冲腔6,中压出气口15和中压缓冲腔19所组成。在转鼓9的内部,圆周排布有多条作为压力振荡管的封闭槽道10,高压射流喷嘴2和中压出流口13静止,分别置于转鼓9的两端,二者的径向半径高度,分别对齐于转鼓9中槽道10的始端开口和末端开口。随着转鼓9的旋转,高压射流喷嘴2向圆周排布的槽道10中依次射流,产生压缩波压缩槽道10内的气体使其升压,待槽道10随转鼓转过一定角度之后,其末端开口与中压出流口13周向重合,升压后的气体排出槽道;射流后槽道10的始端开口由于转过高压射流喷嘴2,即被该喷嘴周边的固壁封堵,在始端开口处产生膨胀波使该处压力降低,当槽道10始端开口转到与低压气引射口8重合时,低压气被吸入槽道10,然后重复上述的射流和压缩过程。  The utility model is an axial flow jet air wave supercharger relying on the sequential jet flow of pressure gas to make unsteady expansion work and supercharging. Drum jacket 11, a plurality of grooves 10 as pressure oscillation tubes, main shaft 18, left body 4, right body 16, shell 12, high-pressure jet nozzle 2, low-pressure air injection port 8, medium-pressure outlet 13, all The pressure port 20, the high-pressure air inlet 1 and the high-pressure buffer chamber 3, the low-pressure air inlet 7 and the low-pressure buffer chamber 6, the medium-pressure air outlet 15 and the medium-pressure buffer chamber 19 are formed. Inside the drum 9, there are a plurality of closed grooves 10 as pressure oscillation tubes arranged around the circumference. The high-pressure jet nozzle 2 and the medium-pressure outlet 13 are stationary and placed at the two ends of the drum 9 respectively. To the height of the radius, they are respectively aligned with the opening at the beginning and the opening at the end of the channel 10 in the drum 9 . With the rotation of the drum 9, the high-pressure jet nozzles 2 sequentially jet into the circumferentially arranged channels 10, generating compression waves to compress the gas in the channels 10 to increase the pressure, and the channels 10 rotate through a certain angle with the drum. Afterwards, its end opening coincides with the medium pressure outlet 13 in the circumferential direction, and the gas after the boost is discharged from the channel; after the jet flow, the beginning opening of the channel 10 is sealed by the solid wall around the nozzle due to turning over the high-pressure jet nozzle 2. Blocking, an expansion wave is generated at the opening at the beginning to reduce the pressure there. When the opening at the beginning of the channel 10 turns to coincide with the low-pressure air ejection port 8, the low-pressure air is sucked into the channel 10, and then the above jet and compression process is repeated. the

本实用新型增压器中转鼓9的旋转,只是为产生周期性的射流、压缩、排气和吸气所需,而不是像涡轮机械那样进行能量转换,因此其转速不需要很高(<5000r/min)。  The rotation of the rotating drum 9 in the supercharger of the utility model is only required for generating periodic jet flow, compression, exhaust and air intake, rather than performing energy conversion like a turbomachinery, so its rotating speed does not need to be very high (<5000r /min). the

转鼓9外圆和转鼓外套11内圆之间围成的环腔内,以多条长的沿纵向隔断的窄壁即栅板21对环腔进行周向切分,在环腔内形成多条两端开口、而周边封闭的槽道10,槽道10的轴线与转鼓9的轴线成一定的径向扩张角,也与转鼓9表面的母线成一定的周向夹角,槽道的通流截面为等截面、变截面或者等截面加变截面;变截面的通流面积,采用将槽道10的深度、宽度,或深、宽尺寸不断增加的方式,沿着槽道10中的流体流向渐扩式增加,高压射流喷嘴2与中压出流口13分别与压力振荡管槽道10的始端口和末端口径向对齐,且二者的轴线沿着转鼓的转向错开一定的圆周夹角,中压出流口13与中压缓冲腔19相接 处设有扩压导流器14,右机体16上还设有能使槽道10与中压缓冲腔19相通的均压孔20。  In the ring cavity surrounded by the outer circle of the drum 9 and the inner circle of the drum jacket 11, the ring cavity is divided circumferentially by a plurality of long narrow walls partitioned along the longitudinal direction, that is, grid plates 21, forming a ring cavity in the ring cavity. A plurality of channels 10 that are open at both ends and closed at the periphery. The axis of the channel 10 forms a certain radial expansion angle with the axis of the drum 9, and also forms a certain circumferential angle with the generatrix of the surface of the drum 9. The grooves The flow section of the channel is equal section, variable section or equal section plus variable section; the flow area of variable section adopts the method of continuously increasing the depth, width, or depth and width of the channel 10 along the channel 10. The fluid flow in the medium increases gradually, the high-pressure jet nozzle 2 and the medium-pressure outlet 13 are radially aligned with the beginning port and the end port of the pressure oscillation pipe groove 10, and the axes of the two are staggered by a certain amount along the turning direction of the drum. The included angle of the circle, the medium pressure outlet 13 and the medium pressure buffer chamber 19 are connected by a diffuser deflector 14, and the right body 16 is also provided with an equalizer that enables the channel 10 to communicate with the medium pressure buffer chamber 19 Pressure hole 20. the

为使本实用新型轴流式射流气波增压器具有较高的效率和适应性,还采用了如下几种结构特征:  In order to make the axial-flow jet air wave supercharger of the utility model have higher efficiency and adaptability, the following structural features are also adopted:

1.作为压缩过程关键流道的槽道10,其通流面积沿流向为逐渐扩张、或部分长度段是逐渐扩张的,以削弱压缩波叠加成激波的强度,改善过程的等熵性,提高压缩效率。  1. As the key channel of the compression process, the flow area of the channel 10 gradually expands along the flow direction, or part of the length section gradually expands, so as to weaken the intensity of compression waves superimposed into shock waves and improve the isentropy of the process. Improve compression efficiency. the

2.在中压出流口13与中压缓冲腔19之间设置扩压导流器14,将出流中压气的动能无损失地转化成压力能。  2. A diffuser deflector 14 is provided between the medium pressure outlet 13 and the medium pressure buffer chamber 19 to convert the kinetic energy of the outflow medium pressure gas into pressure energy without loss. the

3.为保证不同压比下设备的性能均较佳,右机体16上设有能使槽道10与中压缓冲腔(19)相通的均压孔20,当完成一个循环后,若槽道10内的压力高于均压孔20,部分气体经由均压孔20排入中压缓冲腔19,使槽道内的压力降低;反之亦然。这样可使槽道10内的压力基本与中压出流口13的压力持平,避免在下一个循环,槽道10末端开口与中压出流口13重合时,产生干扰压力波。  3. In order to ensure better performance of the equipment under different pressure ratios, the right body 16 is provided with a pressure equalizing hole 20 that enables the channel 10 to communicate with the medium pressure buffer chamber (19). After a cycle is completed, if the channel The pressure in 10 is higher than the pressure equalizing hole 20, and part of the gas is discharged into the medium pressure buffer chamber 19 through the pressure equalizing hole 20, reducing the pressure in the channel; and vice versa. In this way, the pressure in the channel 10 can be substantially equal to the pressure of the medium pressure outlet 13, so as to avoid interference pressure waves when the opening at the end of the channel 10 coincides with the medium pressure outlet 13 in the next cycle. the

本实用新型的有益效果是:  The beneficial effects of the utility model are:

获得一种转速低、结构相对简单,能量传递速度快、可带液运行,能高效实现两种气体之间压力交换、有效利用压力能的新型增压设备。本实用新型轴通式射流气波增压器适合于各种气体介质间的压力能交换,在利用高压高产气井天然气压力能来提升低压低产气井的压力等级,使低压气井稳产高产具有很大的应用价值。此外,在工业废气压力能利用、以及石油和化学工业中的真空蒸发、真空提纯等也适用。  Obtain a new supercharger equipment with low rotation speed, relatively simple structure, fast energy transfer speed, liquid-carrying operation, high-efficiency pressure exchange between two gases, and effective use of pressure energy. The utility model shaft-through jet gas wave supercharger is suitable for the exchange of pressure energy among various gas media. It has great advantages in using the natural gas pressure energy of high-pressure and high-yield gas wells to increase the pressure level of low-pressure and low-yield gas wells, so as to make low-pressure gas wells stable and high-yield. Value. In addition, it is also applicable to the utilization of industrial waste gas pressure, as well as vacuum evaporation and vacuum purification in petroleum and chemical industries. the

下面结合附图和具体实施方式对本实用新型做进一步的说明。  The utility model will be further described below in conjunction with the accompanying drawings and specific embodiments. the

附图说明 Description of drawings

图1为本实用新型轴流式射流气波增压器的结构示意图。  Fig. 1 is a structural schematic diagram of an axial-flow jet air wave supercharger of the present invention. the

图2为转鼓槽道第一种结构形示意图。  Fig. 2 is a schematic diagram of the first structure of the drum channel. the

图3为转鼓槽道第二种结构形示意图。  Fig. 3 is a schematic diagram of the second structure of the drum channel. the

图4为均压口位置和形状的示意图。  Figure 4 is a schematic diagram of the position and shape of the pressure equalizing port. the

图中:1高压进气口,2高压射流喷嘴,3高压缓冲腔,4左机体,  In the figure: 1 high-pressure air inlet, 2 high-pressure jet nozzle, 3 high-pressure buffer chamber, 4 left body,

5左机体压紧法兰,6低压缓冲腔,7低压进气口,8低压气引射口,9转鼓,10压力振荡管槽道,11转鼓外套,12外壳,13中压出流口,14扩压导流器,15中压出气口,16右机体,17右机体压紧法兰,18主轴,19中压缓冲腔,20均压口,21纵向隔断栅壁。  5 Compression flange of the left body, 6 Low-pressure buffer chamber, 7 Low-pressure air inlet, 8 Low-pressure air injection port, 9 Rotary drum, 10 Pressure oscillation pipe groove, 11 Rotary drum jacket, 12 Shell, 13 Medium-pressure outlet Mouth, 14 diffuser deflector, 15 medium pressure air outlet, 16 right body, 17 right body compression flange, 18 main shaft, 19 medium pressure buffer cavity, 20 pressure equalizing port, 21 longitudinal partition grid wall. the

具体实施方式 Detailed ways

本实用新型轴流式射流气波增压器的一种典型的实施方式描述如下,但不只局限于此种实施方式:  A typical implementation of the utility model axial flow jet air wave supercharger is described as follows, but not limited to this implementation:

轴流式射流气波增压器,主要由圆柱形、圆台形、或圆柱与圆台组合形的转鼓9,转鼓外套11、多条压力振荡管槽道10、主轴18、左机体4、右机体16、外壳12、高压射流喷嘴2、低压气引射口8、中压出流口13、均压口20、高压进气口1和高压缓冲腔3、低压进气口7和低压缓冲腔6、中压出气口15和中压缓冲腔19所组成,在转鼓9外圆和转鼓外套11内圆之间,由多条长纵向隔断的窄壁21对转鼓9外圆和转鼓外套11内圆之间所围成的环腔进行切分,形成多条圆周环向排布的两端敞口、周边封闭的槽道10,槽道10沿着转鼓9的轴向纵贯排布。  Axial-flow jet air wave supercharger mainly consists of a cylindrical, truncated, or combined cylindrical and truncated drum 9, a drum jacket 11, multiple pressure oscillation pipe channels 10, a main shaft 18, a left body 4, Right body 16, shell 12, high-pressure jet nozzle 2, low-pressure air injection port 8, medium-pressure outlet 13, pressure equalization port 20, high-pressure air inlet 1 and high-pressure buffer chamber 3, low-pressure air inlet 7 and low-pressure buffer Cavity 6, medium pressure air outlet 15 and medium pressure buffer chamber 19 are formed. Between the outer circle of drum 9 and the inner circle of drum jacket 11, a plurality of long and longitudinally separated narrow walls 21 pair the outer circle of drum 9 and the inner circle of drum jacket 11. The ring cavity surrounded by the inner circle of the drum jacket 11 is divided to form a plurality of circumferentially arranged grooves 10 with both ends open and the periphery closed. The grooves 10 are along the axial direction of the drum 9 Arranged vertically. the

多条长纵向隔断的窄壁21对转鼓9外圆和转鼓外套11内圆之间围成的环腔进行切分,在环腔内形成多条两端开口槽道10的结构形式之一是,在转鼓9外圆表面和转鼓外套11内圆表面纵向加工出沿周向均布、且数量相同的窄沟槽, 将转鼓9和转鼓外套11同心布置,并使转鼓9和转鼓外套11上的各窄沟槽沿径向辐射方向对齐,将栅板21插入对齐的窄沟槽后浸焊密封,形成鼓、套之间多条纵向沿程密闭的槽道10。  A plurality of long and longitudinally partitioned narrow walls 21 divide the ring cavity formed between the outer circle of the drum 9 and the inner circle of the drum jacket 11, and form a structural form of a plurality of open channels 10 in the ring cavity. One is to longitudinally process narrow grooves uniformly distributed in the circumferential direction and in the same number on the outer surface of the drum 9 and the inner surface of the drum jacket 11, arrange the drum 9 and the drum jacket 11 concentrically, and make the drum 9 Align with the narrow grooves on the drum jacket 11 along the radial radial direction, insert the grid plate 21 into the aligned narrow grooves and then dip solder and seal to form multiple longitudinally sealed channels 10 between the drum and the jacket. the

多条长纵向隔断的窄壁21对转鼓9外圆和转鼓外套11内圆之间围成的环腔进行切分,在环腔内形成多条两端开口槽道10的结构形式之二是,在转鼓9外圆表面纵向加工出沿周向均布的槽道,再将转鼓外套11套入转鼓9,其转鼓外套11的内径和锥度与转鼓9的外径和锥度相等,形成鼓、套之间多条纵向沿程密闭的槽道10。  A plurality of long and longitudinally partitioned narrow walls 21 divide the ring cavity formed between the outer circle of the drum 9 and the inner circle of the drum jacket 11, and form a structural form of a plurality of open channels 10 in the ring cavity. The second is to longitudinally process grooves evenly distributed along the circumferential direction on the outer surface of the drum 9, and then insert the drum jacket 11 into the drum 9, and the inner diameter and taper of the drum jacket 11 are the same as the outer diameter and taper of the drum 9. Equal, form a plurality of longitudinally sealed channels 10 between the drum and the sleeve. the

槽道10的通流面积沿程变化,变化的形式为下述中的一种:自始端向末端逐渐扩大,或先逐渐扩大后再保持不变,或先保持不变之后再逐渐扩大,或始终不变,即渐扩段的长度占整个槽道10长度的0%~100%。槽道10通流面积渐扩的方法是在其深度、宽度方向上逐增,渐扩角为0~60°之间,槽道10通流截面的高度范围为1~100mm,宽度范围为1~100mm。  The flow area of the channel 10 changes along the way, and the form of change is one of the following: it gradually expands from the beginning to the end, or first gradually expands and then remains constant, or first remains unchanged and then gradually expands, or It is always the same, that is, the length of the diverging section accounts for 0% to 100% of the length of the entire channel 10 . The method for the gradual expansion of the flow area of the channel 10 is to increase gradually in the direction of its depth and width, and the gradual expansion angle is between 0° and 60°. ~100mm. the

槽道10沿着转鼓的纵向排列,其轴线与转鼓9表面母线之间的夹角为0~50°;在转鼓9的圆台段内,槽道10的轴线沿着纵向逐渐向径向扩张,与转鼓轴线的夹角为0~60°。  The grooves 10 are arranged along the longitudinal direction of the drum, and the angle between the axis and the generatrix of the surface of the drum 9 is 0-50°; in the circular platform section of the drum 9, the axes of the grooves 10 gradually extend radially along the longitudinal direction. To expand, the angle with the axis of the drum is 0-60°. the

中压出流口13与中压缓冲腔19相接处设有扩压导流器14,它由曲面过渡的渐扩封闭流道构成,流道的扩张角为5~60°,流道轴线与转鼓9轴线之间的径向弯曲夹角逐渐过渡增大,为0~90°。  A diffuser deflector 14 is provided at the junction of the medium pressure outlet 13 and the medium pressure buffer chamber 19, which is composed of a gradually expanding and closed flow channel with a curved surface transition. The expansion angle of the flow channel is 5-60°, and the axis of the flow channel The radial bending angle with the axis of the rotating drum 9 gradually increases and is 0-90°. the

高压射流喷嘴2与中压出流口13按圆周转向错的开夹角为5~330°,由左、右机体4和16的相对转动定位,来调整确定该夹角。  The open angle between high-pressure jet nozzle 2 and medium-pressure outlet 13 is 5~330° according to the circumferential steering stagger, and the relative rotation positioning of left and right body 4 and 16 is adjusted to determine this angle. the

均压口20与中压出流口13之间具有10~180°的圆周旋转错角,顺转鼓转动方向,中压出流口13在前,均压口20在后。  There is a staggered rotation angle of 10-180° between the pressure equalizing port 20 and the medium pressure outlet 13 , and along the rotation direction of the drum, the medium pressure outlet 13 is in front and the pressure equalizing port 20 is behind. the

槽道10的数量为5~300条,长度为10~4000mm,转鼓9的直径为10~4000mm。  The number of channels 10 is 5-300, the length is 10-4000 mm, and the diameter of the drum 9 is 10-4000 mm. the

本实用新型轴流式射流气波增压器的工作机理叙述如下:  The working mechanism of the utility model axial flow jet air wave supercharger is described as follows:

高压气体从高压进气口1进到高压缓冲腔3,经静止的高压射流喷嘴2加速成射流,随着转鼓9的转动而依次射入转鼓的各个槽道10内,在槽道10内产生压缩波,增压槽道10内的气体,之后槽道转到对齐中压出流口13,增压气排出。槽道10与高压射流喷嘴2转开和被封堵后,会产生向槽道内传播的膨胀波,使槽道10始端的压力下降,槽道10随即又与低压气引射口8接通,低压气体进入槽道10。由于旋转,使各个槽道依次不断地工作,所以增压过程可连续进行,气体在中压缓冲腔19内汇集后连续排出。  The high-pressure gas enters the high-pressure buffer chamber 3 from the high-pressure air inlet 1, accelerates into a jet flow through the stationary high-pressure jet nozzle 2, and is injected into each channel 10 of the drum in sequence with the rotation of the drum 9. A compression wave is generated in the pressurized channel 10 to pressurize the gas in the channel 10, and then the channel is turned to align with the middle pressure outlet 13, and the pressurized gas is discharged. After the channel 10 and the high-pressure jet nozzle 2 are turned away and blocked, an expansion wave propagating into the channel will be generated, so that the pressure at the beginning of the channel 10 will drop, and the channel 10 will be connected to the low-pressure air injection port 8 again immediately. Gas at low pressure enters channel 10 . Due to the rotation, each channel continuously works successively, so the pressurization process can be carried out continuously, and the gas is collected in the medium-pressure buffer chamber 19 and then discharged continuously. the

轴流式射流气波增压器的运行参数如下:  The operating parameters of the axial flow jet air wave supercharger are as follows:

主轴18与转鼓9的转速:300~6000r/min;  The speed of the main shaft 18 and the drum 9: 300~6000r/min;

进出口的压力范围:0~15MPa;  Pressure range of inlet and outlet: 0~15MPa;

高低压气体的压比范围:1.2~6。  The pressure ratio range of high and low pressure gas: 1.2~6. the

Claims (9)

1. one kind relies on pressed gas jet successively, makes non-permanent expansion work and the axial flow jet wave pressure supercharger of supercharging, is mainly connect the rotary drum (9) of frustoconic shape by cylindrical, frustoconic shape or cylinder; Rotary drum overcoat (11), many conduits (10), main shaft (18) as the pressure oscillation pipe; Left side body (4), right body (16), shell (12); High-pressure spray nozzle (2), low pressure gas ejecting port (8), middle extrusion head piece (13); All press mouthful (20), high pressure admission mouth (1) and high-pressure buffer chamber (3), low-pressure admission mouth (7) and low pressure buffer chamber (6); Middle extrusion gas port (15) and middle pressure buffer cavity (19) are formed, and it is characterized in that: in the ring cavity that surrounds between the circle in rotary drum (9) cylindrical and the rotary drum overcoat (11), be that screen (21) carries out circumferential cutting to ring cavity with many long narrow walls that longitudinally cut off; In ring cavity, form many both ends opens and the conduit (10) of border seal, the axis of conduit (10) becomes certain radial dilatation angle with the axis of rotary drum (9), and also the bus with rotary drum (9) surface becomes certain circumferential angle; The passage section of conduit (10) is that uniform section, variable cross section or uniform section add variable cross section, and the flow area of variable cross section adopts the degree of depth, width with conduit (10); Or the ever-increasing mode of dark, wide size; Direction of flow gradually expansion type in the conduit (10) increases, high-pressure spray nozzle (2) and middle extrusion head piece (13) respectively with the top mouth and the end port radially aligned in pressure oscillation tube seat road (10), and the axis of the two staggers along turning to of rotary drum the circumference angle certain; The middle head piece (13) that extrudes is provided with diffusion fluid director (14) with middle pressure buffer cavity (19) connecting part, also is provided with the balancing orifice (20) that conduit (10) is communicated with middle pressure buffer cavity (19) on the right body (16).
2. pressurized machine as claimed in claim 1; It is characterized in that: the narrow wall (21) of many long vertical partitions carries out cutting to the ring cavity that surrounds between the circle in rotary drum (9) cylindrical and the rotary drum overcoat (11); One of structural type that in ring cavity, forms many both ends open conduits (10) is: vertically process along the narrow groove that circumferentially is uniformly distributed with and quantity is identical at rotary drum (9) outer round surface and rotary drum overcoat (11) internal circular surfaces; With rotary drum (9) and rotary drum overcoat (11) arranged concentric; And make the radially radiation direction alignment of each narrow groove on rotary drum (9) and the rotary drum overcoat (11); Screen (21) is inserted immersed solder sealing behind the narrow groove of alignment, form between drum, the cover many vertically along the airtight conduit of journey (10).
3. pressurized machine as claimed in claim 1; It is characterized in that: the narrow wall (21) of many long vertical partitions carries out cutting to the ring cavity that surrounds between the circle in rotary drum (9) cylindrical and the rotary drum overcoat (11); Two of the structural type of many both ends open conduits of formation (10) are in ring cavity: vertically process along the conduit that circumferentially is uniformly distributed with at rotary drum (9) outer round surface; Again rotary drum overcoat (11) is inserted in rotary drum (9); The internal diameter of its rotary drum overcoat (11) and tapering equate with the external diameter and the tapering of rotary drum (9), forms between drum, the cover many vertically along the airtight conduit of journey (10).
4. pressurized machine as claimed in claim 1 is characterized in that: the form that conduit (10) flow area changes is a kind of in following: terminad enlarges gradually from top; Remain unchanged again after enlarging gradually earlier; Enlarge gradually again after remaining unchanged earlier; All the time constant, promptly the length of gradually expanding section accounts for 0%~100% of whole conduit (10) length:
The method of conduit (10) flow area flaring is on its degree of depth, width direction, to pursue to increase, and the flaring angle is between 0~60 °, and the altitude range of conduit (10) passage section is 1~100mm, and width range is 1~100mm.
5. pressurized machine as claimed in claim 1 is characterized in that: conduit (10) is along vertical arrangement of rotary drum, and the angle between the surperficial bus of its axis and rotary drum (9) is 0~50 °; In the round platform section of rotary drum (9), the axis of conduit (10) along vertically gradually to radially expansion, with the angle of rotary drum axis be 0~60 °.
6. pressurized machine as claimed in claim 1; It is characterized in that: the diffusion fluid director (14) that middle extrusion head piece (13) and middle pressure buffer cavity (19) connecting part are provided with; Be that flaring closed flow by surface blending constitutes; The angle of flare of runner is 5~60 °, between runner axis and rotary drum (9) axis radially bend angle gradually transition increase, be 0~90 °.
7. pressurized machine as claimed in claim 1 is characterized in that: it is 5~330 ° that high-pressure spray nozzle (2) turns to the wrong angle of opening with middle extrusion head piece (13) by circumference, by the location that relatively rotates of left and right body (4) and (16), adjusts and confirms this angle.
8. pressurized machine as claimed in claim 1 is characterized in that: all press the circumference rotation alternate angle that has 10~180 ° between mouthful (20) and the middle extrusion head piece (13), clockwise bulging sense of rotation, middle extrusion head piece (13) is preceding, all press mouth (20) after.
9. pressurized machine as claimed in claim 1 is characterized in that: the quantity of conduit (10) is 5~300, and length is 10~4000mm, and the diameter of rotary drum (9) is 10~4000mm.
CN2012201155970U 2012-03-23 2012-03-23 Axial-flow type jet flow air wave supercharger Expired - Lifetime CN202468498U (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102606547A (en) * 2012-03-23 2012-07-25 大连理工大学 Axial-flow type jet flow gas wave pressure supercharger
CN111397235A (en) * 2020-03-23 2020-07-10 大连理工大学 Frequency-adjustable sonic wave jet oscillator
CN113669309A (en) * 2021-08-11 2021-11-19 大连理工大学 Condensation separation type air wave supercharging device and method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102606547A (en) * 2012-03-23 2012-07-25 大连理工大学 Axial-flow type jet flow gas wave pressure supercharger
CN111397235A (en) * 2020-03-23 2020-07-10 大连理工大学 Frequency-adjustable sonic wave jet oscillator
CN113669309A (en) * 2021-08-11 2021-11-19 大连理工大学 Condensation separation type air wave supercharging device and method
CN113669309B (en) * 2021-08-11 2022-12-20 大连理工大学 Condensation separation type air wave supercharging device and method

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