CN103075204B - Back steam seal device of steam turbine - Google Patents

Back steam seal device of steam turbine Download PDF

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Publication number
CN103075204B
CN103075204B CN201310030043.XA CN201310030043A CN103075204B CN 103075204 B CN103075204 B CN 103075204B CN 201310030043 A CN201310030043 A CN 201310030043A CN 103075204 B CN103075204 B CN 103075204B
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China
Prior art keywords
seal ring
rotor
steam
resistance vapour
labyrinth casing
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CN201310030043.XA
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CN103075204A (en
Inventor
王立君
信景光
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WEIFANG LEINUO POWER EQUIPMENT CO Ltd
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WEIFANG LEINUO POWER EQUIPMENT CO Ltd
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Priority to CN201310030043.XA priority Critical patent/CN103075204B/en
Publication of CN103075204A publication Critical patent/CN103075204A/en
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  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention belongs to steam turbine technology field, provide a kind of back steam seal device of steam turbine, comprise envelope body, the first seal ring is provided with in rotor recesses, the second seal ring is provided with in labyrinth casing groove, described first seal ring has two rotor resistance vapour anchor rings extended along described rotor radial to described second seal ring, and the diameter being positioned at the described rotor resistance vapour anchor ring of upstream along airflow direction is greater than the diameter of the described rotor resistance vapour anchor ring being positioned at downstream; Described second seal ring has two labyrinth casings resistance vapour anchor rings, labyrinth casing resistance vapour anchor ring described in two stretch out described labyrinth casing and described in two between labyrinth casing resistance vapour anchor ring shape have angle.Compared with traditional stage teeth structure, the travel of steam between seal ring increases, it is more that vapor pressure reduces, the leakage rate of steam reduces, sealing effect is better, the axis allowed during rotor expanded by heating and radial displacement are all amid a sharp increase, alleviate the wearing and tearing of packing, extend the working life of packing.

Description

Back steam seal device of steam turbine
Technical field
The invention belongs to steam turbine technology field, particularly relate to a kind of back steam seal device of steam turbine.
Background technique
Steam turbine is a kind of is power with steam, and is the rotating machinery of mechanical work by the thermal energy of steam, and be most widely used prime mover in modern thermal power plant, steam turbine has the advantages such as single-machine capacity is large, efficiency is high, the life-span is long.The air loss of steam turbine accounts for about 1/3 of internal losses, and the packing of steam turbine can prevent ambient air from entering vapor mixing in steam turbine and steam turbine, reduces steam leakage.
The seal arrangement of conventional construction, it is less than normal that packing makes a concession gap design, vibrate when particularly crossing critical speed of rotation and strengthen, cause kinematics and static friction, packing heavy wear, after running a period of time, there will be steam leakage phenomenon, along with the lengthening of unit service time, steam leakage phenomenon can be on the rise, and the efficiency of steam turbine also reduces greatly.
Summary of the invention
Technical problem to be solved by this invention is: provide a kind of back steam seal device of steam turbine, is intended to solve the technical problem that traditional gland seal structure makes a concession the little easy wearing and tearing in gap.
For solving the problems of the technologies described above, technological scheme of the present invention is: back steam seal device of steam turbine, comprise the labyrinth casing be arranged between the cylinder body of steam turbine and rotor, described rotor radial direction is provided with the rotor recesses of annular, the first seal ring is provided with in described rotor recesses, described labyrinth casing is provided with the labyrinth casing groove of annular in the radial direction, the second seal ring has been provided with in described labyrinth casing groove, described first seal ring has two rotor resistance vapour anchor rings extended along described rotor radial to described second seal ring, the diameter being positioned at the described rotor resistance vapour anchor ring of upstream along airflow direction is greater than the diameter of the described rotor resistance vapour anchor ring being positioned at downstream, described second seal ring has two labyrinth casings resistance vapour anchor rings, labyrinth casing resistance vapour anchor ring described in two stretch out described labyrinth casing and described in two between labyrinth casing resistance vapour anchor ring shape have angle, form air-flow path between described second seal ring and described first seal ring.
Improve as one, the radial clearance between described second seal ring and described first seal ring is 0.5 millimeter.
After have employed technique scheme, the invention has the beneficial effects as follows:
Because the second seal ring be provided with in labyrinth casing groove has two labyrinth casing resistance vapour anchor rings, two labyrinth casing resistance vapour anchor rings stretch out labyrinth casing and between two labyrinth casing resistance vapour anchor rings, shape has angle, the travel of steam between seal ring increases, it is more that vapor pressure reduces, the leakage rate of steam reduces, and sealing effect is better; Again owing to being provided with gap between the second seal ring and the first seal ring radial direction, the axis allowed when rotor expanded by heating and all more traditional stage teeth of radial displacement increase greatly, and the wearing and tearing of labyrinth ring can reduce greatly, extend the working life of labyrinth ring; In addition, can not consider axially to touch mill, can more seal ring be arranged, reduce leakage losses to greatest extent, improve leakage efficiency.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention;
Fig. 2 is the enlarged view at A place in Fig. 1;
In figure, 1, cylinder body, 11, bleeder hole, 2, rotor, 3, labyrinth casing, 31, exhaust port, the 4, first seal ring, the 5, second seal ring, the 6, the 3rd seal ring, 7, exhaust cavity.
Embodiment
In order to make object of the present invention, technological scheme and advantage clearly understand, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, be not intended to limit the present invention.
Fig. 1 shows the structural representation of the back steam seal device of steam turbine that the embodiment of the present invention provides, and Fig. 2 is the enlarged view at A place in Fig. 1, for convenience of explanation, only gives part related to the present invention in figure.
As Fig. 1, Fig. 2 jointly shown in, the back steam seal device of steam turbine that the embodiment of the present invention provides, comprise the labyrinth casing 3 be arranged between the cylinder body 1 of steam turbine and rotor 2, rotor 2 is provided with the rotor recesses of annular in the radial direction, the first seal ring 4 is provided with in rotor recesses, labyrinth casing 3 is provided with the labyrinth casing groove of annular in the radial direction, the second seal ring 5 has been provided with in labyrinth casing groove, first seal ring 4 has two rotor resistance vapour anchor rings extended along rotor 2 radial direction to the second seal ring 5, the diameter being positioned at the rotor resistance vapour anchor ring of upstream along airflow direction is greater than the diameter of the rotor resistance vapour anchor ring being positioned at downstream, second seal ring 5 has two labyrinth casing resistance vapour anchor rings, two labyrinth casing resistance vapour anchor rings stretch out labyrinth casing 3 and between two labyrinth casing resistance vapour anchor rings, shape has angle, form air-flow path between second seal ring 5 and the first seal ring 4, the radial clearance between the second seal ring 5 and the first seal ring 4 is 0.5 millimeter.The second seal ring 5 be provided with in labyrinth casing 3 groove has two labyrinth casing resistance vapour anchor rings, two labyrinth casing resistance vapour anchor rings stretch out labyrinth casing 3 and between two labyrinth casing resistance vapour anchor rings, shape has angle, the travel of steam between seal ring increases, it is more that vapor pressure reduces, the leakage rate of steam reduces, and sealing effect is better; Be provided with gap between second seal ring 5 and the first seal ring 4 radial direction, the axis allowed when rotor 2 expanded by heating and all more traditional stage teeth of radial displacement increase greatly, and the wearing and tearing of labyrinth ring can reduce greatly, extend the working life of labyrinth ring; In addition, can not consider axially to touch mill, can more seal ring be arranged, reduce leakage losses to greatest extent, improve leakage efficiency.
Radial clearance is provided with between cylinder body 1 and labyrinth casing 3, the 3rd seal ring 6 is provided with between cylinder body 1 and labyrinth casing 3, cylinder body 1 is provided with annular groove in radial directions, labyrinth casing 3 is provided with annular groove in axial direction, 3rd seal ring 6 is arranged in the groove on the groove of cylinder body 1 and labyrinth casing 3 axial direction, both make the 3rd seal ring 6 play seal action, also do not affect the expansion of labyrinth casing 3.
Exhaust cavity 7 is provided with between cylinder body 1 and labyrinth casing 3, labyrinth casing 3 is provided with exhaust port 31, cylinder body 1 is provided with bleeder hole 11, exhaust port 31 is connected by exhaust cavity 7 with bleeder hole 11, exhaust port 31 on labyrinth casing 3, can extract out the steam between rotor 2 and labyrinth casing 3, the bleeder hole 11 of cylinder body 1 connects vapor extractor and the condenser that draws gas, the steam of extraction is become condensed water and send into thermodynamic system re-using, economize on resources.
The foregoing is only preferred embodiment of the present invention, not in order to limit the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.

Claims (2)

1. back steam seal device of steam turbine, comprise the labyrinth casing be arranged between the cylinder body of steam turbine and rotor, described rotor radial direction is provided with the rotor recesses of annular, the first seal ring is provided with in described rotor recesses, described labyrinth casing is provided with the labyrinth casing groove of annular in the radial direction, the second seal ring is provided with in described labyrinth casing groove, it is characterized in that, described first seal ring has two rotor resistance vapour anchor rings extended along described rotor radial to described second seal ring, the diameter being positioned at the described rotor resistance vapour anchor ring of upstream along airflow direction is greater than the diameter of the described rotor resistance vapour anchor ring being positioned at downstream, described second seal ring has two labyrinth casings resistance vapour anchor rings, labyrinth casing resistance vapour anchor ring described in two stretch out described labyrinth casing and described in two between labyrinth casing resistance vapour anchor ring shape have angle, form air-flow path between described second seal ring and described first seal ring.
2. back steam seal device of steam turbine as claimed in claim 1, it is characterized in that, the radial clearance between described second seal ring and described first seal ring is 0.5 millimeter.
CN201310030043.XA 2013-01-25 2013-01-25 Back steam seal device of steam turbine Active CN103075204B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310030043.XA CN103075204B (en) 2013-01-25 2013-01-25 Back steam seal device of steam turbine

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Application Number Priority Date Filing Date Title
CN201310030043.XA CN103075204B (en) 2013-01-25 2013-01-25 Back steam seal device of steam turbine

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CN103075204B true CN103075204B (en) 2015-11-18

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104343473B (en) * 2014-09-02 2015-09-09 华中科技大学 A kind of shaft end seal device for organic working medium radial-inward-flow turbine
CN110206593A (en) * 2019-07-04 2019-09-06 杭州汽轮机股份有限公司 Floating can make a concession formula interstage gland

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4046388A (en) * 1976-03-09 1977-09-06 Westinghouse Electric Corporation Seal arrangement utilizing deflector seals of reduced radial dimension
SU756048A1 (en) * 1977-12-12 1980-08-15 Boris N Korablev Turbomachine labirinth seal
CN101876259A (en) * 2009-05-01 2010-11-03 株式会社日立制作所 Sealing configuration and controlling method thereof
CN102269016A (en) * 2011-07-09 2011-12-07 潍坊雷诺特动力设备有限公司 Clapboard steam seal for steam power device
CN203081512U (en) * 2013-01-25 2013-07-24 潍坊雷诺特动力设备有限公司 Turbine rear vapor seal device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2408548A (en) * 2003-11-25 2005-06-01 Alstom Technology Ltd Finned seals for turbomachinery

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4046388A (en) * 1976-03-09 1977-09-06 Westinghouse Electric Corporation Seal arrangement utilizing deflector seals of reduced radial dimension
SU756048A1 (en) * 1977-12-12 1980-08-15 Boris N Korablev Turbomachine labirinth seal
CN101876259A (en) * 2009-05-01 2010-11-03 株式会社日立制作所 Sealing configuration and controlling method thereof
CN102269016A (en) * 2011-07-09 2011-12-07 潍坊雷诺特动力设备有限公司 Clapboard steam seal for steam power device
CN203081512U (en) * 2013-01-25 2013-07-24 潍坊雷诺特动力设备有限公司 Turbine rear vapor seal device

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