CN208718729U - A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure - Google Patents

A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure Download PDF

Info

Publication number
CN208718729U
CN208718729U CN201821577848.0U CN201821577848U CN208718729U CN 208718729 U CN208718729 U CN 208718729U CN 201821577848 U CN201821577848 U CN 201821577848U CN 208718729 U CN208718729 U CN 208718729U
Authority
CN
China
Prior art keywords
labyrinth casing
labyrinth
ring
seal cover
shaft seal
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.)
Withdrawn - After Issue
Application number
CN201821577848.0U
Other languages
Chinese (zh)
Inventor
姚福锋
赵世群
郭佳
齐佳品
王超
付兴伟
刘殊
刘殊一
张俊博
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
703th Research Institute of CSIC
Original Assignee
703th Research Institute of CSIC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 703th Research Institute of CSIC filed Critical 703th Research Institute of CSIC
Priority to CN201821577848.0U priority Critical patent/CN208718729U/en
Application granted granted Critical
Publication of CN208718729U publication Critical patent/CN208718729U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure, it is related to energy source and power technical field.The utility model solves heavy workload when existing low parameter back pressure turbine has replacement end packing, and has the problem of leakage vapour hidden danger at the vertical and horizontal flange face intersection of former quick disassembly end gland seal structure.First labyrinth casing of the utility model is arranged between cylinder upper half and rotor, second labyrinth casing is arranged between shaft seal cover and rotor, shaft seal cover is affixed by mutually matched annular table and annular groove and cylinder upper half, shaft seal cover passes through half-connection under horizontal flange and cylinder, first labyrinth casing and the second labyrinth casing are composed of two semi-circular packing units, two semi-circular packing units of the first labyrinth casing pass through split flanged joint by split flanged joint, two semi-circular packing units of the second labyrinth casing.The utility model is used for the fast assembling-disassembling of low parameter back pressure turbine end gland seal structure.

Description

A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure
Technical field
The utility model relates to energy source and power technical fields, are specifically related to a kind of low parameter back pressure turbine Quick Release ready-package Hold gland seal structure.
Background technique
Low parameter back pressure turbine refer to initial steam pressure between 0.7MPa~1MPa, exhaust steam pressure 0.1MPa~ The back pressure turbine of 0.3MPa.Discontinuity heat supply is needed in China certain areas, each generating set is to improve the thermal efficiency, all one after another Carry out heat supply transformation, and low parameter steam turbine can be taken out the four of the above Turbo-generator Set of 600MW and 1000MW power grade and steam Vapour drives the acting such as various pumps, blower, compressor and generator or power generation, replaces simultaneously on the basis of meeting heat demand For temperature-decreased pressure reducer, the cascade utilization of the energy is realized, greatly improve energy utilization rate, and can also be achieved the unit outage phase Between, the original system thermal efficiency is not had an impact.
Steam turbine may cause rotor and packing because of reasons such as start and stop, abnormal vibrations or misoperations in the process of running Mill is touched, the gap between packing and rotor is caused to increase.The increase of labyrinth clearance certainly will increase steam loss, and then may lead Origin or beginning gland leak-off.Thoroughly to solve the problems, such as end gland leak-off, it is necessary to steam seal ring is replaced, and general steam turbine replaces steam seal ring When, it requires to open cylinder upper half, workload is very big.Some units also use the end gland seal structure fast dismantled, but should Structure has vertically and horizontally flange face simultaneously, and leakage vapour phenomenon is also easy to produce at the intersection of vertical and horizontal flange face.
In conclusion existing low parameter back pressure turbine has heavy workload when replacing end packing, and original is fast torn open Unloading has the problem of leakage vapour hidden danger at the vertical and horizontal flange face intersection of end gland seal structure.
Utility model content
There is work when replacement end packing purpose of the utility model is to solve existing low parameter back pressure turbine Work amount is big, and has the problem of leakage vapour hidden danger, Jin Erti at the vertical and horizontal flange face intersection of former quick disassembly end gland seal structure For a kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure.
The technical solution of the utility model is:
A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure, it includes the first labyrinth casing, shaft seal cover and the Two labyrinth casings, shaft seal cover are mounted on the end of cylinder, and the side of shaft seal cover and cylinder upper half are tightly connected, the horizontal ends of shaft seal cover Face and the horizontal end face of cylinder lower half are affixed;First labyrinth casing is arranged between cylinder upper half and rotor, the setting of the second labyrinth casing Between shaft seal cover and rotor, annular groove is radially opened up on the outer wall of cylinder upper half end, shaft seal cover is semicircular configuration, axle envelope The inner wall of lid is radially equipped with the annular table for cooperating with annular groove, and shaft seal cover passes through mutually matched annular table and annular groove Affixed with cylinder upper half, the lower end surface level of processing flange face of shaft seal cover, shaft seal cover is connected by horizontal flange and cylinder lower half It connects, the first labyrinth casing and the second labyrinth casing are composed of two semi-circular packing units, each semi-circular packing unit Both ends of the surface are equipped with split flange, and two semi-circular packing units of the first labyrinth casing pass through split flanged joint, the second vapour Two semi-circular packing units for sealing body pass through split flanged joint.
Further, the end gland seal structure further includes the first adjustment gasket and second adjustment gasket;Outside first labyrinth casing Circle is radially equipped with first boss, and the inner ring of cylinder upper half and cylinder lower half is radially opened up for cooperating with first boss First groove, the first labyrinth casing are connected with cylinder upper half and cylinder lower half respectively by mutually matched first boss and the first groove It connects, the first adjustment gasket is equipped between the first labyrinth casing and cylinder upper half and cylinder lower half;Second labyrinth casing outer ring is radially set There is a second boss, the inner ring of shaft seal cover and cylinder lower half radially opens up the second groove for cooperating with second boss, and Two labyrinth casings by mutually matched second boss and the second groove respectively with half-connection under shaft seal cover and cylinder, the second labyrinth casing Second adjustment gasket is equipped between shaft seal cover and cylinder lower half.
Further, the end gland seal structure further includes the first steam seal ring and the second steam seal ring, the first steam seal ring and second The structure of steam seal ring is identical, and the outer ring of the first steam seal ring and the second steam seal ring is radially equipped with T stage;The setting of first steam seal ring exists Between first labyrinth casing and rotor, the first labyrinth casing inner ring is radially equipped with the first T-slot for cooperating with T stage, and first Steam seal ring is connect by mutually matched T stage and the first T-slot with the first labyrinth casing;Second steam seal ring is arranged in the second packing Between body and rotor, the second labyrinth casing inner ring is radially equipped with the second T-slot for cooperating with T stage, and the second steam seal ring is logical It crosses mutually matched T stage and the second T-slot is connect with the second labyrinth casing.
Further, the inner ring of the first steam seal ring and the second steam seal ring is equipped with for more with rotor outer ring tooth socket fit Grade annular tooth.
Further, the quantity of the first steam seal ring is two, and the quantity of the second steam seal ring is one.
Further, the end gland seal structure further includes multiple positioning pins, two semi-circular packing lists of the first labyrinth casing It is fixed by positioning pin between member, between two semi-circular packing units of the second labyrinth casing.
The utility model has the effect that compared with prior art
1, low parameter back pressure turbine novel quick release ready-package described in the utility model end gland seal structure structure is simple, realizes It is simple and efficient, reliable operation.It can be realized in the case where not opening cylinder upper half, so that it may replace end packing, improve low ginseng The maintainability of number back pressure turbine, reduces workload when low parameter back pressure turbine replacement end packing, and unit replaces end vapour Feng Shi, can first dismantle the fasteners such as shaft seal cover and the bolt of half-connection under cylinder, then dismantle shaft seal cover, then dismantle the second packing Body split flange bolt, the second labyrinth casing are composed of two semi-circular packing units, can divide after dismantling shaft seal cover It is not taken out from top, carries out the replacement of the second steam seal ring of end.After replacement, dress is returned in reverse order.
2, the shaft seal cover of the utility model be semicircular configuration, the inner wall of shaft seal cover be radially equipped with for cylinder upper half Annular groove cooperation annular table, shaft seal cover is affixed by mutually matched annular table and annular groove and cylinder upper half, not only can It enough realizes the axially position between shaft seal cover and cylinder upper half, also achieves the sealed connection of the two, eliminate previous with vertical Leakage vapour hidden danger at the straight and fast-type end gland seal structure intersection of horizontal flange.
Detailed description of the invention
Fig. 1 is the sectional view of the utility model;
Fig. 2 is partial enlarged view of the Fig. 1 at I;
Fig. 3 is the sectional view of the first steam seal ring;
Fig. 4 is the cross-sectional view of the first labyrinth casing;
Fig. 5 is the cross-sectional view of the second labyrinth casing.
Specific embodiment
Specific embodiment 1: illustrating present embodiment, a kind of low parameter back pressure of present embodiment in conjunction with Fig. 1 and Fig. 2 Steam turbine Quick Release ready-package end gland seal structure, it includes the first labyrinth casing 2, shaft seal cover 5 and the second labyrinth casing 7, and shaft seal cover 5 is installed In the end of cylinder, the side of shaft seal cover 5 and cylinder upper half 4 are tightly connected, horizontal end face and the cylinder lower half 10 of shaft seal cover 5 Horizontal end face is affixed;
First labyrinth casing 2 is arranged between cylinder upper half 4 and rotor 9, and the second labyrinth casing 7 is arranged in shaft seal cover 5 and rotor 9 Between, annular groove 4-1 is radially opened up on 4 end outer wall of cylinder upper half, shaft seal cover 5 is semicircular configuration, the inner wall of shaft seal cover 5 It is radially equipped with the annular table 5-1 for cooperating with annular groove 4-1, shaft seal cover 5 passes through mutually matched annular table 5-1 and annular Slot 4-1 and cylinder upper half 4 are affixed, the lower end surface level of processing flange face of shaft seal cover 5, and shaft seal cover 5 passes through horizontal flange and vapour Cylinder lower half 10 connects, and the first labyrinth casing 2 and the second labyrinth casing 7 are composed of two semi-circular packing units, each semi-ring The both ends of the surface of shape packing unit are equipped with split flange, and two semi-circular packing units of the first labyrinth casing 2 pass through split method Two semi-circular packing units of orchid connection, the second labyrinth casing 7 pass through split flanged joint.
Specific embodiment 2: illustrating present embodiment, the end packing of present embodiment in conjunction with Fig. 1, Fig. 4 and Fig. 5 Structure further includes the first adjustment gasket 3 and second adjustment gasket 6;
First labyrinth casing, 2 outer ring is radially equipped with first boss 2-1, the equal edge of the inner ring of cylinder upper half 4 and cylinder lower half 10 Radial direction opens up the first groove for cooperating with first boss 2-1, and the first labyrinth casing 2 passes through mutually matched first boss 2-1 It is connect respectively with cylinder upper half 4 and cylinder lower half 10 with the first groove, the first labyrinth casing 2 and cylinder upper half 4 and cylinder lower half 10 Between be equipped with the first adjustment gasket 3;
Second labyrinth casing, 7 outer ring is radially equipped with second boss 7-1, and the inner ring of shaft seal cover 5 and cylinder lower half 10 is along diameter To the second groove opened up for cooperating with second boss 7-1, the second labyrinth casing 7 by mutually matched second boss 7-1 and Second groove is connect with shaft seal cover 5 and cylinder lower half 10 respectively, is set between the second labyrinth casing 7 and shaft seal cover 5 and cylinder lower half 10 There is second adjustment gasket 6.So set, the first labyrinth casing 2 realizes axially position, the second labyrinth casing 7 by the first adjustment gasket 3 Axially position is realized by second adjustment gasket 6.Other compositions and connection relationship are same as the specific embodiment one.
Specific embodiment 3: illustrating present embodiment, the end of present embodiment in conjunction with Fig. 1, Fig. 3, Fig. 4 and Fig. 5 Gland seal structure further includes the first steam seal ring 1 and the second steam seal ring 8, and the first steam seal ring 1 is identical with the structure of the second steam seal ring 8, the The outer ring of one steam seal ring 1 and the second steam seal ring 8 is radially equipped with T stage 1-1;
First steam seal ring 1 is arranged between the first labyrinth casing 2 and rotor 9, and 2 inner ring of the first labyrinth casing, which is radially equipped with, to be used for With the first T-slot 2-2 of T stage 1-1 cooperation, the first steam seal ring 1 passes through mutually matched T stage 1-1 and the first T-slot 2-2 It is connect with the first labyrinth casing 2;
Second steam seal ring 8 is arranged between the second labyrinth casing 7 and rotor 9, and 7 inner ring of the second labyrinth casing, which is radially equipped with, to be used for With the second T-slot 7-2 of T stage 1-1 cooperation, the second steam seal ring 8 passes through mutually matched T stage 1-1 and the second T-slot 7-2 It is connect with the second labyrinth casing 7.So set, the first steam seal ring 1 by mutually matched T stage 1-1 and the first T-slot 2-2 with The connection of first labyrinth casing 2, ensure that the bonding strength of the first steam seal ring 1 and the first labyrinth casing 2;Second steam seal ring 8 passes through mutual The T stage 1-1 of cooperation and the second T-slot 7-2 are connect with the second labyrinth casing 7, ensure that the second steam seal ring 8 and the second labyrinth casing 7 Bonding strength, reliable operation.Other compositions and connection relationship are the same as one or two specific embodiments.
Specific embodiment 4: embodiment is described with reference to Fig. 3, the first steam seal ring 1 of present embodiment and the second vapour The inner ring of seal 8 is equipped with for the multi-stage annular tooth 1-2 with 9 outer ring tooth socket fit of rotor.So set, the first steam seal ring 1 And second steam seal ring 8 by multi-stage annular tooth 1-2 guarantee and rotor 9 between leakproofness.Other compositions and connection relationship and tool Body embodiment one, 2 is three identical.
Specific embodiment 5: embodiment is described with reference to Fig. 1, the quantity of the first steam seal ring 1 of present embodiment is Two, the quantity of the second steam seal ring 8 is one.So set, can be realized it is multi-stage sealed, have preferable sealing effect.Its It forms identical with connection relationship and specific embodiment one, two, three or four.
Specific embodiment 6: embodiment is described with reference to Fig. 1, the end gland seal structure of present embodiment further includes Multiple positioning pins, between two semi-circular packing units of the first labyrinth casing 2, two semi-circular packing lists of the second labyrinth casing 7 It is fixed by positioning pin between member.Other compositions and connection relationship and specific embodiment one, two, three, four or five are identical.
Working principle
It is illustrated with reference to Fig. 1 working principle of the utility model is: can first dismantle shaft seal cover 5 and vapour when unit replaces end packing Then the fasteners such as the bolt that cylinder lower half 10 connects dismantle shaft seal cover 5, then dismantle 7 split flange bolt of the second labyrinth casing, the Two labyrinth casings 7 are composed of two semi-circular packing units, can be taken out respectively from top after dismantling shaft seal cover 5, are carried out The replacement of the second steam seal ring of end 8.After replacement, dress is returned in reverse order.

Claims (6)

1. a kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure, it includes the first labyrinth casing (2), shaft seal cover (5) With the second labyrinth casing (7), shaft seal cover (5) is mounted on the end of cylinder, and the side of shaft seal cover (5) and cylinder upper half (4) sealing connect It connects, the horizontal end face of shaft seal cover (5) and the horizontal end face of cylinder lower half (10) are affixed;
It is characterized by: the first labyrinth casing (2) is arranged between cylinder upper half (4) and rotor (9), the second labyrinth casing (7) setting Between shaft seal cover (5) and rotor (9), radially opened up annular groove (4-1) on the outer wall of cylinder upper half (4) end, shaft seal cover (5) For semicircular configuration, the inner wall of shaft seal cover (5) is radially equipped with the annular table (5-1) for cooperating with annular groove (4-1), axle envelope Lid (5) is affixed by mutually matched annular table (5-1) and annular groove (4-1) and cylinder upper half (4), the lower end of shaft seal cover (5) Face level of processing flange face, shaft seal cover (5) are connect by horizontal flange with cylinder lower half (10), the first labyrinth casing (2) and the Two labyrinth casings (7) are composed of two semi-circular packing units, the both ends of the surface of each semi-circular packing unit be equipped in point Face flange, two semi-circular packing units of the first labyrinth casing (2) are by split flanged joint, and the two of the second labyrinth casing (7) A semi-circular packing unit passes through split flanged joint.
2. a kind of low parameter back pressure turbine Quick Release ready-package end according to claim 1 gland seal structure, it is characterised in that: The end gland seal structure further includes the first adjustment gasket (3) and second adjustment gasket (6);
First labyrinth casing (2) outer ring is radially equipped with first boss (2-1), the inner ring of cylinder upper half (4) and cylinder lower half (10) The first groove for cooperating with first boss (2-1) is radially opened up, the first labyrinth casing (2) passes through mutually matched first Boss (2-1) and the first groove are connect with cylinder upper half (4) and cylinder lower half (10) respectively, on the first labyrinth casing (2) and cylinder Half is equipped with the first adjustment gasket (3) between (4) and cylinder lower half (10);
Second labyrinth casing (7) outer ring is radially equipped with second boss (7-1), and the inner ring of shaft seal cover (5) and cylinder lower half (10) is equal The second groove for cooperating with second boss (7-1) is radially opened up, the second labyrinth casing (7) is convex by mutually matched second Platform (7-1) and the second groove are connect with shaft seal cover (5) and cylinder lower half (10) respectively, the second labyrinth casing (7) and shaft seal cover (5) and Second adjustment gasket (6) are equipped between cylinder lower half (10).
3. a kind of low parameter back pressure turbine Quick Release ready-package end according to claim 2 gland seal structure, it is characterised in that: The end gland seal structure further includes the first steam seal ring (1) and the second steam seal ring (8), the first steam seal ring (1) and the second steam seal ring (8) Structure it is identical, the outer ring of the first steam seal ring (1) and the second steam seal ring (8) is radially equipped with T stage (1-1);
First steam seal ring (1) is arranged between the first labyrinth casing (2) and rotor (9), and the first labyrinth casing (2) inner ring is radially equipped with The first T-slot (2-2) for cooperating with T stage (1-1), the first steam seal ring (1) by mutually matched T stage (1-1) and First T-slot (2-2) is connect with the first labyrinth casing (2);
Second steam seal ring (8) is arranged between the second labyrinth casing (7) and rotor (9), and the second labyrinth casing (7) inner ring is radially equipped with The second T-slot (7-2) for cooperating with T stage (1-1), the second steam seal ring (8) by mutually matched T stage (1-1) and Second T-slot (7-2) is connect with the second labyrinth casing (7).
4. a kind of low parameter back pressure turbine Quick Release ready-package end according to claim 3 gland seal structure, it is characterised in that: The inner ring of first steam seal ring (1) and the second steam seal ring (8) is equipped with for the multi-stage annular tooth with rotor (9) outer ring tooth socket fit (1-2)。
5. a kind of low parameter back pressure turbine Quick Release ready-package end according to claim 3 or 4 gland seal structure, feature exist In: the quantity of the first steam seal ring (1) is two, and the quantity of the second steam seal ring (8) is one.
6. a kind of low parameter back pressure turbine Quick Release ready-package end according to claim 1,2 or 3 gland seal structure, feature Be: the end gland seal structure further includes multiple positioning pins, between two semi-circular packing units of the first labyrinth casing (2), It is fixed by positioning pin between two semi-circular packing units of two labyrinth casings (7).
CN201821577848.0U 2018-09-25 2018-09-25 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure Withdrawn - After Issue CN208718729U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821577848.0U CN208718729U (en) 2018-09-25 2018-09-25 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821577848.0U CN208718729U (en) 2018-09-25 2018-09-25 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure

Publications (1)

Publication Number Publication Date
CN208718729U true CN208718729U (en) 2019-04-09

Family

ID=65982846

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821577848.0U Withdrawn - After Issue CN208718729U (en) 2018-09-25 2018-09-25 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure

Country Status (1)

Country Link
CN (1) CN208718729U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109026185A (en) * 2018-09-25 2018-12-18 中国船舶重工集团公司第七0三研究所 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109026185A (en) * 2018-09-25 2018-12-18 中国船舶重工集团公司第七0三研究所 A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure
CN109026185B (en) * 2018-09-25 2023-11-28 中国船舶重工集团公司第七0三研究所 Quick-dismantling and quick-assembling type end steam seal structure of low-parameter back pressure steam turbine

Similar Documents

Publication Publication Date Title
US10443615B2 (en) Alignment of flanged components
CN104047640B (en) A kind of brush seal structure of adjustable radial gap
CN106536867A (en) Stator blade, gas turbine, split ring, method for modifying stator blade, and method for modifying split ring
CN208718729U (en) A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure
CN204783137U (en) High middling pressure integral type inner casing structure of steam turbine
CN109026185A (en) A kind of low parameter back pressure turbine Quick Release ready-package end gland seal structure
CN109538309A (en) A kind of shaft end self sealing structure of high revolving speed High Pressure Difference
CN101216111A (en) Method for implementing bearing hermetic sealing for machining inner screw thread copper pipe
CN205330739U (en) End vapor seal can swiftly be dismantled to high back pressure steam turbine
CN202866911U (en) Turbine high-pressure cylinder structure
US10502057B2 (en) System and method for blade access in turbomachinery
CN105673091A (en) Sealing clearance self-adjusting steam sealing device having gas suspension effect
CN105240053A (en) Screw expander
CN106703900A (en) Novel self-adjustment spring type steam seal
CN205089370U (en) Screw expander
CN203522437U (en) Improved turbine generator
CN105545373B (en) High-back-pressure turbine end vapor seal capable of being rapidly detached
CN203420927U (en) Blower labyrinth seal structure
CN205260081U (en) Double -deck cylinder of high back pressure steam turbine
CN203703140U (en) Nitrogen sealing device
JPH112104A (en) Seal structure of gas turbine flange sealing face
CN203822435U (en) Exhaust connection structure of supercharger of diesel
CN206753666U (en) A kind of critical oil supply system of turbine LP rotors
CN202520958U (en) Gas sealing system for hydrogenerator
CN218717014U (en) Online cleaning device of turbine

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20190409

Effective date of abandoning: 20231128

AV01 Patent right actively abandoned

Granted publication date: 20190409

Effective date of abandoning: 20231128

AV01 Patent right actively abandoned
AV01 Patent right actively abandoned