CN1313737C - Anti-surge ring of axial fan - Google Patents
Anti-surge ring of axial fan Download PDFInfo
- Publication number
- CN1313737C CN1313737C CNB2005100236405A CN200510023640A CN1313737C CN 1313737 C CN1313737 C CN 1313737C CN B2005100236405 A CNB2005100236405 A CN B2005100236405A CN 200510023640 A CN200510023640 A CN 200510023640A CN 1313737 C CN1313737 C CN 1313737C
- Authority
- CN
- China
- Prior art keywords
- ring
- surge
- rings
- axial flow
- flow fan
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
轴流通风机防喘振环,属于风机与通风工程技术领域。防喘振环是隧道用轴流通风机外壳的一部分,是由外圈、内圈、圆环组成的,沿气流方向前后对称的、外形呈凹凸相间的圆环体,圆环的外径和外圈的直径一致,圆环的内径和内圈的直径一致,外圈数量在2和5之间,内圈数量比外圈数量少1,圆环数量是内圈数量的2倍。防喘振环的最常用形式由3个外圈、2个内圈和4个圆环组成。轴流风机叶片顶部前后缘分别位于防喘振环前后的凹形空间位置处。防喘振环的凹形空间会抑制进口涡流的发展。所以防喘振环能推迟风机喘振的发生,甚至不发生。由于防喘振环是前后对称的,所以在需要双向通风的地铁、铁路、公路隧道中,当风机反转时,会产生同样的防喘振效果。
An anti-surge ring for an axial flow fan belongs to the technical field of fan and ventilation engineering. The anti-surge ring is a part of the casing of the axial flow fan used in the tunnel. It is composed of an outer ring, an inner ring, and a ring. The diameter of the outer ring is the same, the inner diameter of the ring is the same as the diameter of the inner ring, the number of outer rings is between 2 and 5, the number of inner rings is 1 less than the number of outer rings, and the number of rings is twice the number of inner rings. The most common form of anti-surge ring consists of 3 outer rings, 2 inner rings and 4 circular rings. The front and rear edges of the blade top of the axial flow fan are respectively located at the concave space positions at the front and back of the anti-surge ring. The concave space of the anti-surge ring inhibits the development of inlet vortices. Therefore, the anti-surge ring can delay the occurrence of fan surge, or even prevent it from occurring. Since the anti-surge ring is front-to-back symmetrical, the same anti-surge effect will be produced when the fan is reversed in subway, railway, and road tunnels that require two-way ventilation.
Description
技术领域technical field
本发明涉及的是一种轴流通风机防喘振环,特别是一种适用于地铁或隧道的轴流通风机防喘振环,属于风机与通风工程技术领域。The invention relates to an anti-surge ring for an axial flow fan, in particular to an anti-surge ring for an axial flow fan suitable for subways or tunnels, and belongs to the technical field of fans and ventilation engineering.
背景技术Background technique
随着国家经济的发展,我国的交通事业也有了超常的发展。城市中的地铁、穿越大山的铁路、公路隧道越来越多。由于隧道的高度有限,长度又很长,隧道中的通风显得特别重要。现在地铁、铁路、公路隧道中的通风问题主要由中大型轴流风机来承担。但是因通风管网和消声器堵塞,或地铁列车、汽车逆向行驶造成的活塞风效应而导致瞬间背压过大,使风机的风量急剧下降。致使风机发生失速、喘振,并引起剧列振动,严重时会损坏风机。为了给人们提供一个安全、可靠的交通环境,消除轴流通风机的喘振是很必要的。而消除或减弱风叶进口顶端的气流回流,就可以抑制喘振的发生,或使喘振点向更小流量处偏移,减小发生喘振的可能。With the development of the country's economy, my country's transportation industry has also experienced extraordinary development. There are more and more subways in cities, railways passing through mountains, and road tunnels. Due to the limited height and length of the tunnel, ventilation in the tunnel is particularly important. At present, the ventilation problems in subways, railways, and highway tunnels are mainly borne by medium and large axial flow fans. However, due to the blockage of the ventilation pipe network and the muffler, or the piston wind effect caused by the reverse running of subway trains and automobiles, the instantaneous back pressure is too large, and the air volume of the fan drops sharply. Cause the fan to stall, surge, and cause severe vibration, and in severe cases, the fan will be damaged. In order to provide people with a safe and reliable traffic environment, it is necessary to eliminate the surge of the axial flow fan. Eliminating or weakening the backflow of the airflow at the top of the fan blade inlet can suppress the occurrence of surge, or shift the surge point to a place with a smaller flow rate, reducing the possibility of surge.
已有技术中,专利号为ZL 00218027.8,名称为“轴流通风机防喘振装置”的实用新型专利是采用在“外壳和内圈之间”设置“均匀分布的导向叶片”,而且“所述的导向叶片在外壳和内圈内的轴向倾斜角可为30°~90°,所述的导向叶片数可以为30~150片”,由于叶片多,装配时要保持一致,要求高,所以增加了生产的难度;专利号为ZL 01105719.x,名称为“隧道射流风机防喘振装置”的发明专利采用的内简体“是一个以风机轴心线为轴的旋转体,该旋转体的外表面是由圆柱面和圆弧面构成”,由于圆弧面的加工成型有一定的难度,而且风机的径向尺寸增加较大,占据了隧道中宝贵的空间。专利号为CN 2448969,名称为“防喘振轴流风机”的实用新型专利中“防喘环包括集涡槽,集涡槽内沿圆周方向均匀布置一组消蜗片、在消蜗片内侧靠近叶片处设置一整流环,集涡槽侧靠近叶片端还装导流环”。这种结构很复杂,安装时耗时费工。In the existing technology, the patent number is ZL 00218027.8, and the utility model patent named "anti-surge device of axial flow fan" adopts "evenly distributed guide vanes" "between the shell and the inner ring", and "all The axial inclination angle of the guide vanes in the outer shell and the inner ring can be 30°-90°, and the number of guide vanes can be 30-150". Therefore, the difficulty of production has been increased; the patent number is ZL 01105719.x, and the invention patent named "Tunnel Jet Fan Anti-Surge Device" uses the inner simplified "is a rotating body with the axis of the fan as the axis. The outer surface of the fan is composed of a cylindrical surface and an arc surface. Because the machining of the arc surface is difficult, and the radial size of the fan increases greatly, it occupies valuable space in the tunnel. The patent number is CN 2448969, and the utility model patent titled "Anti-surge Axial Flow Fan" states that "the anti-surge ring includes a vortex collecting groove, and a group of worm-elimination plates are evenly arranged in the vortex-collecting groove along the circumferential direction, and inside the worm-eliminating plates A rectifying ring is arranged near the blade, and a guide ring is installed on the side of the vortex near the end of the blade." This structure is very complicated and time-consuming and labor-intensive during installation.
发明内容Contents of the invention
为了克服已有技术的不足和缺陷,改善轴流风机在小流量时的工作条件,本发明设计一种结构更为简单、合理,加工方便并能有效消除轴流风机工作中可能出现的失速、喘振现象的防喘振环。In order to overcome the deficiencies and defects of the prior art and improve the working conditions of the axial flow fan at low flow rate, the present invention designs a structure which is simpler and more reasonable, which is convenient to process and can effectively eliminate the possible stall, Anti-surge ring for surge phenomenon.
防喘振环是一个沿气流方向前后对称、外形呈凹凸相间的圆环体,是隧道用轴流通风机外壳的一部分,安装在叶轮叶片位置。本发明包括外圈、内圈、圆环。圆环的外径和外圈的直径一致;圆环的内径和内圈的直径一致。外圈数量在2和5之间,内圈数量比外圈数量少1,圆环数量是内圈数量的2倍。防喘振环的最常用形式由3个外圈、2个内圈和4个圆环组成。第1个外圈的一端和第1个圆环的外径端焊接,第1个圆环的内径端和第1个内圈的一端焊接,第1个内圈的另一端和第2个圆环的内径端焊接,第2个圆环的外径端和第2个外圈的一端焊接,以此顺序,直到第4个圆环的外径端和第3个外圈的一端焊接,该防喘振环焊接成形后,在其前后两端分别焊接法兰,以便和轴流风机的前后外壳连接。防喘振环的前后两端与法兰之间构成了凹形空间。在和轴流风机相配时,轴流风机叶片顶部前后缘分别位于防喘振环前后的凹形空间位置处,而叶片顶部和内圈之间的间隙起着轴向气流的密封作用。The anti-surge ring is a circular body with front and back symmetry along the direction of airflow, with alternating concave and convex shapes. It is a part of the casing of the axial flow fan for tunnels and is installed at the position of the impeller blades. The present invention includes an outer ring, an inner ring and a circular ring. The outer diameter of the ring is consistent with the diameter of the outer ring; the inner diameter of the ring is consistent with the diameter of the inner ring. The number of outer rings is between 2 and 5, the number of inner rings is 1 less than the number of outer rings, and the number of rings is twice the number of inner rings. The most common form of anti-surge ring consists of 3 outer rings, 2 inner rings and 4 circular rings. One end of the first outer ring is welded to the outer diameter end of the first ring, the inner diameter end of the first ring is welded to one end of the first inner ring, and the other end of the first inner ring is welded to the second ring The inner diameter end of the ring is welded, the outer diameter end of the second ring is welded to one end of the second outer ring, in this order, until the outer diameter end of the fourth ring is welded to one end of the third outer ring, the After the anti-surge ring is welded and formed, flanges are respectively welded at its front and rear ends so as to be connected with the front and rear shells of the axial flow fan. A concave space is formed between the front and rear ends of the anti-surge ring and the flange. When matched with an axial flow fan, the front and rear edges of the blade top of the axial flow fan are respectively located in the concave space before and after the anti-surge ring, and the gap between the top of the blade and the inner ring acts as a seal for the axial air flow.
轴流风机工作时,随着风机流量的减小,在轴流风机叶片顶部进口处渐渐出现涡流,该涡流随着流量的减小而不断增大。但在轴流风机装有防喘振环后,该进口涡流位于防喘振环的凹形空间附近,此时防喘振环的凹形空间就会抑制进口涡流的发展。所以防喘振环能推迟风机喘振的发生,甚至不发生。在对某一轴流风机进行性能对比试验时,装有防喘振环后的轴流风机,在流量减小时,它的风压比不装防喘振环的轴流风机平均上升了10%左右。由于本发明的防喘振环是前后对称的,所以在需要双向通风的地铁、铁路、公路隧道中,当风机反转时,会产生同样的防喘振效果。When the axial flow fan is working, as the flow rate of the fan decreases, a vortex gradually appears at the inlet of the blade top of the axial flow fan, and the vortex increases continuously with the decrease of the flow rate. However, after the axial flow fan is equipped with an anti-surge ring, the inlet vortex is located near the concave space of the anti-surge ring, and the concave space of the anti-surge ring will inhibit the development of the inlet vortex. Therefore, the anti-surge ring can delay the occurrence of fan surge, or even prevent it from occurring. When performing a performance comparison test on a certain axial flow fan, the axial flow fan equipped with an anti-surge ring, when the flow rate decreases, its wind pressure rises by an average of 10% compared with the axial flow fan without an anti-surge ring about. Since the anti-surge ring of the present invention is front-to-back symmetrical, the same anti-surge effect will be produced when the fan is reversed in tunnels of subways, railways and roads that require two-way ventilation.
本发明结构简单、加工方便、防喘振效果明显,具有显著的社会效益和经济效益。The invention has the advantages of simple structure, convenient processing, obvious anti-surge effect, and remarkable social and economic benefits.
附图说明Description of drawings
图1是轴流通风机防喘振环的结构示意图。Fig. 1 is a structural schematic diagram of an anti-surge ring of an axial flow fan.
图2是防喘振环的立体图,Figure 2 is a perspective view of the anti-surge ring,
图中1是外圈、2是圆环、3是内圈、4是法兰、5是凹形空间、6是叶片。In the figure, 1 is an outer ring, 2 is a ring, 3 is an inner ring, 4 is a flange, 5 is a concave space, and 6 is a blade.
图3是轴流通风机安装防喘振环前后的性能比较图,Figure 3 is a performance comparison diagram of the axial flow fan before and after installing the anti-surge ring,
图中带“◆”号的曲线是未装防喘振环的风机性能曲线;带“■”号的曲线是装防喘振环后的风机性能曲线。The curve with "◆" in the figure is the performance curve of the fan without anti-surge ring; the curve with "■" is the performance curve of the fan with anti-surge ring installed.
具体实施方式Detailed ways
下面结合附图对本发明的具体实施作进一步的描述:The specific implementation of the present invention will be further described below in conjunction with accompanying drawing:
如图1、图2所示,本发明包括外圈1、圆环2和内圈3。圆环2的外径和外圈1的直径一致;圆环2的内径和内圈3的直径一致。外圈1数量在2和5之间,内圈3数量比外圈1数量少1,圆环2数量是内圈3数量的2倍。防喘振环的最常用形式由3个外圈1、2个内圈3和4个圆环2组成。第1个外圈1的一端和第1个圆环2的外径端焊接,第1个圆环2的内径端和第1个内圈3的一端焊接,第1个内圈3的另一端和第2个圆环2的内径端焊接,第2个圆环2的外径端和第3个外圈1的一端焊接,以此顺序,直到第4个圆环2的外径端和第3个外圈1的一端焊接,该防喘振环焊接成形后,在其前后两端分别焊接法兰4,以便和轴流风机的前后外壳连接。防喘振环前后两端和法兰4之间构成了凹形空间5。在和轴流风机相配时,轴流风机叶片6的顶部前后缘分别位于防喘振环前后的凹形空间5位置处,而叶片6顶部和内圈3之间的间隙起着轴向气流的密封作用。As shown in FIG. 1 and FIG. 2 , the present invention includes an outer ring 1 , a
轴流通风机防喘振环除了焊接成形外,也可使用冲压成形的方法,先按凹凸相间的形状开好成型模,按所需尺寸裁剪矩形铁板,再焊接成平圆环,然后在成型模上滚压成形。In addition to welding and forming, the anti-surge ring of axial flow fan can also be formed by stamping. First, the forming mold is opened according to the shape of concave and convex, and the rectangular iron plate is cut according to the required size, and then welded into a flat ring, and then formed. Die roll forming.
轴流风机工作时,随着风机流量的减小,在轴流风机叶片6顶部进口处渐渐出现涡流,该涡流随着流量的减小而不断增大。但在轴流风机装有防喘振环后,该进口涡流位于防喘振环的凹形空间5附近,此时防喘振环的凹形空间5就会抑制进口涡流的发展。所以防喘振环能推迟风机喘振的发生,甚至不发生。如图3所示,在对某一轴流风机进行性能对比试验时,装有防喘振环后的轴流风机,在流量减小时,它的风压比不装防喘振环的轴流风机平均上升了10%左右。由于本发明的防喘振环是前后对称的,所以在需要双向通风的地铁、铁路、公路隧道中,当风机反转时,会产生同样的防喘振效果。When the axial flow fan is working, as the flow rate of the fan decreases, a vortex gradually appears at the inlet of the
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005100236405A CN1313737C (en) | 2005-01-27 | 2005-01-27 | Anti-surge ring of axial fan |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005100236405A CN1313737C (en) | 2005-01-27 | 2005-01-27 | Anti-surge ring of axial fan |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1644930A CN1644930A (en) | 2005-07-27 |
| CN1313737C true CN1313737C (en) | 2007-05-02 |
Family
ID=34875923
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2005100236405A Expired - Fee Related CN1313737C (en) | 2005-01-27 | 2005-01-27 | Anti-surge ring of axial fan |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1313737C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109340144A (en) * | 2018-10-15 | 2019-02-15 | 佛山冠博机械科技发展有限公司 | Multi-stage centrifugal fan |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104632715A (en) * | 2013-11-15 | 2015-05-20 | 鸿富锦精密工业(深圳)有限公司 | fan |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4239452A (en) * | 1978-06-26 | 1980-12-16 | United Technologies Corporation | Blade tip shroud for a compression stage of a gas turbine engine |
| GB2158879A (en) * | 1984-05-19 | 1985-11-20 | Rolls Royce | Preventing surge in an axial flow compressor |
| US5707206A (en) * | 1995-07-18 | 1998-01-13 | Ebara Corporation | Turbomachine |
| CN2448969Y (en) * | 2000-11-08 | 2001-09-19 | 南通市同济申海大型风机有限公司 | Anti-surge axial fan |
| CN2547926Y (en) * | 2002-06-25 | 2003-04-30 | 天津市通风机厂 | Anti-surge two-way axial-flow fan |
| CN1147666C (en) * | 2001-03-22 | 2004-04-28 | 上海交通大学 | Anti-surge device for tunnel jet fan |
-
2005
- 2005-01-27 CN CNB2005100236405A patent/CN1313737C/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4239452A (en) * | 1978-06-26 | 1980-12-16 | United Technologies Corporation | Blade tip shroud for a compression stage of a gas turbine engine |
| GB2158879A (en) * | 1984-05-19 | 1985-11-20 | Rolls Royce | Preventing surge in an axial flow compressor |
| US5707206A (en) * | 1995-07-18 | 1998-01-13 | Ebara Corporation | Turbomachine |
| CN2448969Y (en) * | 2000-11-08 | 2001-09-19 | 南通市同济申海大型风机有限公司 | Anti-surge axial fan |
| CN1147666C (en) * | 2001-03-22 | 2004-04-28 | 上海交通大学 | Anti-surge device for tunnel jet fan |
| CN2547926Y (en) * | 2002-06-25 | 2003-04-30 | 天津市通风机厂 | Anti-surge two-way axial-flow fan |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109340144A (en) * | 2018-10-15 | 2019-02-15 | 佛山冠博机械科技发展有限公司 | Multi-stage centrifugal fan |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1644930A (en) | 2005-07-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106762824B (en) | Axial fan three-way impeller with vein-like structure and seagull-shaped splitter blades | |
| CN105332945B (en) | A kind of Centrifugal Fan Impeller of adjustable splitterr vanes | |
| CN205190327U (en) | Centrifugal fan impeller of adjustable splitterr vanes | |
| CN112814943A (en) | Integrally formed curved and swept combined blade, impeller and axial flow fan | |
| CN204663967U (en) | The multistage centrifugal pump impeller that a kind of and radial stator mates | |
| CN1313737C (en) | Anti-surge ring of axial fan | |
| CN208831322U (en) | Cross-flow fan blade and air conditioner | |
| CN105090048B (en) | Micro- head flow velocity type turbine pump | |
| CN208634100U (en) | A multi-arc centrifugal fan blade | |
| CN110857790B (en) | Range hood with current collector | |
| CN206929130U (en) | Axial flow blower 3 d impeller with leaf vein texture and sea-gull type splitterr vanes | |
| CN201963595U (en) | Centrifugal front or rear impeller of non-separated flow subcritical blade profile | |
| CN207004920U (en) | Axial flow blower 3 d impeller with leaf vein texture and circular arc post splitterr vanes | |
| CN214465105U (en) | High-efficiency low-noise centrifugal fan | |
| CN103016408B (en) | A kind of one-dimensional linear hollow guide vane | |
| CN207004919U (en) | Axial flow blower 3 d impeller with leaf vein texture and splitterr vanes | |
| CN106837867B (en) | Three-way impeller for axial fans with vein-like structure and splitter blades | |
| CN2466399Y (en) | Low-noise pipeline axialflow ventilator | |
| CN206929131U (en) | Axial flow blower 3 d impeller with leaf vein texture and non-homogeneous empennage | |
| CN104929973A (en) | Multiple-stage centrifugal pump impeller matched with radial guide vane | |
| CN114856717B (en) | A Novel Exhaust Diffuser Structure with Splitter Plate for Enhanced Aerodynamic Performance | |
| CN206636819U (en) | Subway axial flow blower rotary press modelling monoblock type anti-surge installation | |
| CN1147666C (en) | Anti-surge device for tunnel jet fan | |
| CN205401226U (en) | Impeller structure | |
| CN201865751U (en) | Air inlet channel of supercharger |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20070502 Termination date: 20140127 |