CN1276849A - Exhaust duct for steam turbine - Google Patents
Exhaust duct for steam turbine Download PDFInfo
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- CN1276849A CN1276849A CN 98810253 CN98810253A CN1276849A CN 1276849 A CN1276849 A CN 1276849A CN 98810253 CN98810253 CN 98810253 CN 98810253 A CN98810253 A CN 98810253A CN 1276849 A CN1276849 A CN 1276849A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/30—Exhaust heads, chambers, or the like
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- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
本发明属于动力机器制造,可应用于蒸气涡轮机排气管的设计和改进。The invention belongs to power machine manufacturing and can be applied to the design and improvement of steam turbine exhaust pipes.
已知的蒸气涡轮机排气管包括带水平拆接口的管体,拆接口把管体分割为两部分:上面部分和下面部分,在管体中安装着蒸气涡轮机的最后一级工作叶轮,可能还安装着有内圈和外圈的轴径向辐射喇叭形风筒(参阅,例如a.c.SU 1605003,КЛ.F 01D 25/30,07.11.90和RU2040697,КЛ.F 01D 25/30,27.07.95)。Known steam turbine exhaust pipes consist of a pipe body with a horizontal split which divides the pipe body into two parts: an upper part and a lower part, in which the last working impeller of the steam turbine is installed, possibly also Mounted axially radially radiating horn with inner and outer rings (cf. e.g. a.c.SU 1605003, КЛ.F 01D 25/30, 07.11.90 and RU2040697, КЛ.F 01D 25/30, 27.07.95 ).
这些排气管的共同缺点是在向地下冷凝器排放蒸汽流的同时,在排气管的上面部分转动180度,卷压成为两股强大的涡流束。这些涡流束堵塞排气管管体下面部分通行面积相当大的部分,造成在冷凝器入口处速度场严重不均匀。结果作用在涡轮机结构部件和冷凝器联接管上的动态压力急剧增大。还有,气流输出的不均匀性使得蒸汽到冷却水的排热率降低。The common disadvantage of these exhaust pipes is that when the steam flow is discharged to the underground condenser, it turns 180 degrees at the upper part of the exhaust pipe, and is rolled into two powerful vortex bundles. These vortex bundles block a relatively large part of the passage area below the exhaust pipe body, resulting in a severe inhomogeneity of the velocity field at the condenser inlet. As a result, the dynamic pressures acting on the structural components of the turbine and the condenser connecting pipes increase dramatically. Also, non-uniformity in the airflow output reduces the rate of heat removal from steam to cooling water.
已知在a.c.SU 169947,КЛ.F 01D 25/30,17.03.65描述的蒸汽涡轮机排气管,其中管体制作成带水平拆接接口的,附有分割棱系统。这样排气管的主要缺点是曲线棱的复杂系统,使得在每一个曲线沟槽里产生次级气流强度和涡流束,结果损耗猛增,甚至在管入口无量纲速度M较小的条件下也会发生。此外,虽然排气管刚度略微增强,由于气流的不良空气动力学,使用棱系统不能显著降低装入排气管管体内的涡轮机轴承的震动。There is known a steam turbine exhaust pipe described in a.c.SU 169947, КЛ.F 01D 25/30, 17.03.65, wherein the pipe body is made with a horizontal detachable joint, with a split edge system. The main disadvantage of such an exhaust pipe is the complex system of curved edges, which creates secondary airflow intensities and vortex bundles in each curved groove, with the result that the losses increase sharply, even at low dimensionless velocity M at the pipe inlet. will happen. Furthermore, although the exhaust pipe is slightly stiffer, the vibration of the turbine bearings housed in the exhaust pipe body cannot be significantly reduced using the rib system due to the poor aerodynamics of the air flow.
本发明以两个实施方案在降低能耗和同时降低蒸汽涡轮机排气管的全部结构的震动的条件下,解决提高蒸汽涡轮机排气管可靠性和经济性的任务。解决这个任务依靠减少在排气管的出口剖面速度场的不均匀性,这也是实现本发明取得的技术效果。The invention solves the problem of increasing the reliability and economy of steam turbine exhaust pipes in two embodiments while reducing energy consumption and at the same time reducing vibrations of the overall structure of the steam turbine exhaust pipe. Solving this task depends on reducing the inhomogeneity of the velocity field at the exit section of the exhaust pipe, which is also the technical effect achieved by the present invention.
在本发明的第一个实施例中,该技术效果依靠以下措施取得:蒸汽涡轮机排气管管体由刚性部件制成,包括可拆接的带水平拆接平面的两个部分(上和下),在管体的下面部分装着两个防涡旋装置,相对排气管纵轴对称分布,其距离为最后一级工作叶轮直径的1-1.2倍,每个防涡旋装置都是由重叠平板构成的栅格,每块板的长度是最后一级工作叶片长度的45-60%,重叠平板组成横剖面为矩形的孔格,其对边的距离为最后一级工作叶片长度的30-40%。防涡旋装置刚性固定在可卸接管体下面部分的侧壁上,重叠平板的上端与接口水平面重合,矩形孔格剖面和接口平面平行。In the first embodiment of the present invention, this technical effect is achieved by means of the following measures: the exhaust pipe body of the steam turbine is made of rigid parts, consisting of two parts (upper and lower) ), two anti-vortex devices are installed on the lower part of the pipe body, which are symmetrically distributed relative to the longitudinal axis of the exhaust pipe, and the distance is 1-1.2 times the diameter of the last stage of the working impeller. Each anti-vortex device is composed of overlapping The grid composed of flat plates, the length of each plate is 45-60% of the length of the last-stage working blade, and the overlapped flat plates form a grid with a rectangular cross-section, and the distance between the opposite sides is 30-60% of the length of the last-stage working blade. 40%. The anti-vortex device is rigidly fixed on the side wall of the lower part of the detachable connecting pipe body, the upper end of the overlapping plate coincides with the interface horizontal plane, and the section of the rectangular cell is parallel to the interface plane.
在本发明的第二个实施例中,涉及的是带径向喇叭形风筒的涡轮机排气管,上述的技术效果的获得是由于蒸汽涡轮机排气管管体由刚性元件制成,包含带水平结合面的可拆接的两个部分(上与下),在管体的下面部分配置两对防涡旋装置,而且每对防涡旋装置相对管体的纵轴对称分布,这时其中任何一个抗涡流装置都由重叠平板构成栅格状,每个平板的长度为最后一级工作叶片长度的45-60%,重叠平板构成矩形孔格,其对边的距离为最后一级工作叶片长度的30-40%,而且有一对防涡旋装置中的任何一个都刚性地固定在可拆接管体下面部分的侧壁和喇叭形风筒的外围筒上。另一对防涡旋装置的任何一个都固定在可拆接管体下部的侧壁和喇叭形风筒的内围筒上,重叠平板的上端和接口水平平面重合,孔格的矩形剖面平面与接口平行。In the second embodiment of the present invention, it relates to a turbine exhaust pipe with a radial horn-shaped fan cylinder. The above-mentioned technical effects are obtained because the steam turbine exhaust pipe body is made of rigid elements, including strips The two detachable parts (upper and lower) of the horizontal joint surface are equipped with two pairs of anti-vortex devices on the lower part of the pipe body, and each pair of anti-vortex devices is symmetrically distributed relative to the longitudinal axis of the pipe body. Any anti-vortex device is composed of overlapping plates to form a grid shape, and the length of each plate is 45-60% of the length of the last-stage working blade. The overlapping plates form a rectangular hole, and the distance between the opposite sides is the last-stage working blade. 30-40% of the length, and any one of a pair of anti-vortex devices is rigidly fixed on the side wall of the lower part of the detachable pipe body and the peripheral tube of the trumpet-shaped air duct. Any one of the other pair of anti-vortex devices is fixed on the side wall of the lower part of the detachable connecting pipe body and the inner circumference of the horn-shaped air cylinder. parallel.
本发明的实质用附图说明,附图1示意地表示本发明的第一个实施例蒸气涡轮机排气管下面部分的纵剖面,图2示意地描绘该排气管的全貌(第一实施例),在图3上展示发明的第二个实施例蒸气涡轮机排气管下面部分的纵剖面,图4示意地描绘这个涡轮机排气管的全貌(第二实施例)。Essence of the present invention is explained with accompanying drawing, and accompanying drawing 1 shows schematically the longitudinal section of the lower portion of the steam turbine exhaust pipe of the first embodiment of the present invention, and Fig. 2 schematically depicts the overall view of the exhaust pipe (first embodiment ), on Fig. 3, show the longitudinal section of the second embodiment of the steam turbine exhaust pipe of the invention, and Fig. 4 schematically depicts the overall view of the turbine exhaust pipe (the second embodiment).
在图1,2,3,4上使用的标识如下:The logos used on Figures 1, 2, 3, and 4 are as follows:
1-管体(在图1和图3上刚性固定部件未画出)1-pipe body (the rigid fixing parts are not shown in Fig. 1 and Fig. 3)
2-管体1的上面部分2 - the upper part of the tube body 1
3-管体1的下面部分3 - the lower part of the tube body 1
4-管体1上面部分2和下面部分3的水平结合面4-Horizontal joint surface of
5-矩形孔格5-rectangular hole
6-管体1下面部分3的侧壁6 - The side wall of the
7-由重叠平板8构成的栅格状的防涡旋装置(第一实施例)7-Grid-shaped anti-vortex device (first embodiment) composed of overlapping plates 8
9,10-两对防涡旋装置,其中任何一个都由重叠平板11制作成栅格状(发明的第二实施例)9,10-Two pairs of anti-vortex devices, any one of which is made into a grid by overlapping flat plates 11 (the second embodiment of the invention)
12-喇叭形风筒的外围筒(发明的第二实施例)12-Peripheral cylinder of horn-shaped air cylinder (the second embodiment of the invention)
13-喇叭形风筒的内围筒(发明的第二实施例)13-The inner circumference of the trumpet-shaped air duct (the second embodiment of the invention)
在本发明的第一实施例中,在管体1的可拆接的下面部分3,对称于管体的纵轴0安装两个防涡旋装置7,二者之间的距离为最后一级工作叶轮直径的1-1.2倍。防涡旋装置7之中的任何一个都用重叠平板8组成栅格状,每块平板的长度为最后一级工作叶片长度的45-60%,平板构成剖面为矩形的孔格5,孔格对边的距离为最后一级工作轮叶长度的30-40%。每个防涡旋装置7刚性地固定在管体1可拆接的下面部分3的侧壁6上,重叠平板8的上部与接口水平面4重合,矩形孔格5的横断面与接口平行。In the first embodiment of the invention, on the detachable
在本发明的第二实施例中,在管体1的可拆接的下面部分3,对称于管体的纵轴0安装两对防涡旋装置9和10,其中任何一个都用重叠平板11组成栅格形状,每块平板的长度为最后一级工作叶片长度的45-60%,平板构成剖面为矩形的孔格5,对边的距离为最后一级工作轮叶长度的30-40%。防涡旋装置9之中的任何一个刚性地固定在管体1可拆接的下面3的侧壁和6和喇叭形风筒的外围筒12上,而防涡旋装置10之中的任何一个都固定在管体1的下面可拆接部分的侧壁6和喇叭形风筒的内围筒13上,要求重叠平板11的上部与管体1上面部分2和下面部分3的接口水平面4吻合,矩形孔格5的横断面与接口平行。In a second embodiment of the invention, on the detachable
依照建议的实施方案,蒸汽涡轮机排气管这样工作。来自最后一级工作涡轮的蒸汽进入排气管的管体1,在它的上部2蒸气流转向180度,结果形成两股强大的涡流束,它们快速增长并且到达管体1的出口截面时,占据它的面积的大部分,结果不仅大大增加排气管的流体阻力,特别是在管的入口无量纲速度值M1可观的条件下,而且涡流的不稳定性会引起排气管管体1和与它联接的涡轮机部件强烈低频震荡。但是,在排气管中应用本发明提出的防涡旋装置7和9,10可在蒸汽旋涡强度急剧增长的地方把它们击碎。防涡旋装置由板8和板11来实现,它们的纵向布置允许蒸汽流沿管体1,沿整个宽度畅通无阻地流过,并藉此保证蒸汽流较完全地填充整个出气面。还有,防涡旋装置7或9,10的由重叠平板8或11组成的两个栅格管组安装在管体1下面部分3上,直接在管体的水平接口处,使结构的刚性增强,它的震动大大地降低。评估所用平板8或11的尺寸和由它们组成的栅格从以下考虑出发。相邻板8和11之间的距离直接影响击碎涡流束的效率。间距愈小,击碎涡流束愈好,但同时流体阻力愈大。作为基准尺寸,相对此基准尺寸选取平板8和11以及由它们组成的格栅的最合适的尺寸,取工作涡轮的直径和最后一级叶片的高度。平板8和11彼此之间和与管的管体1的连接,合理地藉助于承力元件,做成例如以圆形截面的杆的形式。圆形截面的杆对气流流入角度变化不敏感。考虑到蒸汽在管体1中流动的复杂性和空间分布特性,连接部件很大。According to the proposed embodiment, the steam turbine exhaust pipe works in this way. The steam from the last working turbine enters the pipe body 1 of the exhaust pipe, and in its
发明可用于建造新的,和改进已经制成的,和正在运行的蒸汽涡轮机排气管,在存在上面列举的主要特征总和的条件下,确保击碎在排气管管体上面部分生成的涡流束,使排气管出口剖面的速度场均匀,减低排气管的流体阻力和震动,于是可以制造出可靠和经济的排气管。Invention applicable to the construction of new and improved existing and operating steam turbine exhaust pipes which, in the presence of the sum of the main features enumerated above, ensure the breakdown of vortices generated in the upper part of the exhaust pipe body The beam can make the velocity field of the outlet section of the exhaust pipe uniform, and reduce the fluid resistance and vibration of the exhaust pipe, so that a reliable and economical exhaust pipe can be manufactured.
Claims (2)
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU97116794 | 1997-10-17 | ||
| RU97116795 | 1997-10-17 | ||
| RU97116794A RU2117773C1 (en) | 1997-10-17 | 1997-10-17 | Steam-turbine exhaust pipe |
| RU97116795A RU2117774C1 (en) | 1997-10-17 | 1997-10-17 | Steam-turbine exhaust pipe |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1276849A true CN1276849A (en) | 2000-12-13 |
| CN1089136C CN1089136C (en) | 2002-08-14 |
Family
ID=26653939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN98810253A Expired - Fee Related CN1089136C (en) | 1997-10-17 | 1998-10-19 | Exhaust duct for steam turbine |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN1089136C (en) |
| AU (1) | AU1181199A (en) |
| WO (1) | WO1999020874A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100340743C (en) * | 2003-07-08 | 2007-10-03 | Gea能源技术有限公司 | Exhaust steam line for steam plants |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2762689B1 (en) | 2013-02-05 | 2017-06-07 | General Electric Technology GmbH | Steam power plant with a second low-pressure turbine and an additional condensing system and method for operating such a steam power plant |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0035838B1 (en) * | 1980-03-10 | 1985-02-06 | Rolls-Royce Plc | Diffusion apparatus |
| SU916770A1 (en) * | 1980-05-23 | 1982-03-30 | Gudkov Eduard | Exhaust pipe of steam turbine low-pressure end |
| SU1295840A1 (en) * | 1985-06-07 | 1987-10-30 | Proizv Ob Nevskij Z Im V I | Turbomachine diffuser |
| CH672004A5 (en) * | 1986-09-26 | 1989-10-13 | Bbc Brown Boveri & Cie | |
| CS272676B1 (en) * | 1988-06-07 | 1991-02-12 | Stastny Miroslav | Outlet branch for bladed machine |
| DE59001693D1 (en) * | 1989-09-12 | 1993-07-15 | Asea Brown Boveri | AXIAL FLOWED TURBINE. |
-
1998
- 1998-10-19 CN CN98810253A patent/CN1089136C/en not_active Expired - Fee Related
- 1998-10-19 AU AU11811/99A patent/AU1181199A/en not_active Abandoned
- 1998-10-19 WO PCT/RU1998/000329 patent/WO1999020874A1/en not_active Ceased
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100340743C (en) * | 2003-07-08 | 2007-10-03 | Gea能源技术有限公司 | Exhaust steam line for steam plants |
Also Published As
| Publication number | Publication date |
|---|---|
| WO1999020874A9 (en) | 1999-07-22 |
| CN1089136C (en) | 2002-08-14 |
| AU1181199A (en) | 1999-05-10 |
| WO1999020874A1 (en) | 1999-04-29 |
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