CN102207198A - Radial annular mixed seal - Google Patents

Radial annular mixed seal Download PDF

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Publication number
CN102207198A
CN102207198A CN2011100886644A CN201110088664A CN102207198A CN 102207198 A CN102207198 A CN 102207198A CN 2011100886644 A CN2011100886644 A CN 2011100886644A CN 201110088664 A CN201110088664 A CN 201110088664A CN 102207198 A CN102207198 A CN 102207198A
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CN
China
Prior art keywords
sealing
seal
regulator plate
rotor
stuffing box
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Pending
Application number
CN2011100886644A
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Chinese (zh)
Inventor
杨建刚
张万福
曹浩
郭瑞
孙丹
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Southeast University
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Southeast University
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Publication date
Application filed by Southeast University filed Critical Southeast University
Priority to CN2011100886644A priority Critical patent/CN102207198A/en
Publication of CN102207198A publication Critical patent/CN102207198A/en
Pending legal-status Critical Current

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  • Sealing Devices (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

The invention discloses a radial annular mixed seal, which comprises a rotor and a sealing sleeve sleeved on the rotor, wherein a pressure cavity air outlet and a pressure cavity air inlet are formed on the sealing sleeve; an adjusting plate and a bellow section are arranged inside the sealing sleeve; one end of the bellow section is fixed on the sealing sleeve, and the other end of the bellow section is connected with the adjusting plate; and a pressure cavity is formed between the adjusting plate and the sealing sleeve. The radial annular mixed seal is characterized in that: a honeycomb sealing disc is arranged on the rotor and is positioned in the middle of the adjusting plate; and a sealing cavity is formed between the adjusting plate and the honeycomb sealing disc. By the radial annular mixed seal, axial flow of gas is changed into radial flow, axial spiral flow is eliminated, the leakage rate is greatly reduced compared with the common seal because the honeycomb sealing disc is arranged, a sealing gap has high adaptive adjusting capacity, the seal has long service life, the exciting force of the airflow in the seal is obviously reduced, and the airflow excitation is greatly reduced.

Description

Radial ringed hybrid sealing
Technical field
The present invention relates to a kind of seal style that is applied in the rotating machinery, relate in particular to a kind of radial ringed hybrid sealing that is used for rotating machinery.
Background technique
At present, reducing the seal leakage amount and improving the sealing wear resistance is the focus that people pay close attention to always, these 2 statistics (synergy) that can regard sealing as.In recent years, sealed motive force characteristic (vibration damping) has obtained increasing the attention both at home and abroad.This is because along with the raising of running parameter, the sealing excitation force that inner fluid produced is increasing, and is also increasing to the harm that unit safety operation brought.People dredge in tradition on the basis of tooth sealing for this reason, have proposed novel seal patterns such as honeycomb, brush, derotation stream, damping, spiral chute, ladder, mixing by the structure that changes sealing itself, have obtained certain effect.But the sealing configuration pattern becomes increasingly complex, and the contradiction between leakage rate and the wear resistance does not obtain fine solution.In order to solve the contradiction between sealing wear resistance and the leakage rate, the nineties in last century, the U.S. proposes adjustable seal concept, and its main thought is to introduce one gas to flow to the sealing back, changes dynamic and static gaps by changing gas pressure.Nineteen ninety, U.S. GE company has researched and developed positive seal, manually controls the folding of sealing block by introducing high pressure steam.Nineteen ninety-five, Toshiba Corp has proposed to adopt the adjustable sealing of pressure ripple management and control system.In recent years, the somebody proposed various seal clearances and adjusted controlling method.Above-mentioned sealing can unify to regard " axial seal " as,, all belongs to " axial seal " in essence though mechanism is incomplete same, promptly along the rotor axis direction arrange some groups (to) sealing, reach sealing effect by decompression step by step.For " axial seal ", mainly there is following problem: (1) helical flow, under the acting in conjunction of fluid leakage flow and rotor high-speed rotation vertically, inevitably the helical flow phenomenon can appear in the Seal cage, this present just confessed Airflow Exciting-Vibration Force main source; (2) prewhirl the influence of convection cell excitation force greatly, prewhirling can appear in mechanical rotary seal inlet, prewhirls and can strengthen the helical flow phenomenon, thereby produce bigger Airflow Exciting-Vibration Force; (3) there is contradiction between leakage rate and the wear resistance; (4) the seal clearance self adaption is adjusted difficulty, axial arranged sealing, and the gap adjustment need be carried out on circumferentially, requires sealing block " expansion " and " contraction " freely, and this has brought very big difficulty for the adjustment of seal clearance self adaption.Practice shows that sealing bite fault appears in this class sealing especially easily.Because the existence of above problem, the flow-induced vibration problem can not be solved at all.
Summary of the invention
Technical problem to be solved by this invention is at above-mentioned the deficiencies in the prior art, and proposes a kind of radial ringed hybrid sealing of eliminating flow-induced vibration.
The technical solution adopted for the present invention to solve the technical problems is:
A kind of radial ringed hybrid sealing, comprise: rotor and be set in epitrochanterian stuffing box gland, on stuffing box gland, be provided with pressure chamber exhaust port and pressure chamber inlet hole, in described stuffing box gland, be provided with regulator plate and ripple joint, one end of described ripple joint is fixed on the stuffing box gland, the other end of ripple joint is connected with described regulator plate, formed pressure chamber between regulator plate and the stuffing box gland, it is characterized in that, described rotor is provided with the honeycomb seal dish, this honeycomb seal dish is positioned in the middle of the described regulator plate, has formed Seal cage between regulator plate and the honeycomb seal dish.
Between described stuffing box gland and regulator plate, also be provided with supported spring.
On regulator plate, be provided with the ring packing tooth, and this ring packing tooth is provided with acceleration transducer between honeycomb seal dish and regulator plate on regulator plate.
Compared with prior art, the beneficial effect of the radial ringed hybrid sealing of the present invention's proposition is as follows:
(1) simple in structure, any fixed sealing all can be changed into corresponding radial ringed hybrid sealing in view of the above;
(2) except the existing energy dissipation mechanism of conventional seals, be provided with the honeycomb seal dish, can form a plurality of whirlpools in this process, energy dissipation is big, and it is obvious that turbulent flow increases the resistance effect, and the also therefore and conventional sealing of leakage rate is little.By numerical simulation calculation result in early stage, radial ringed hybrid sealing reduces leakage rate 30%~50% than traditional labyrinth seal.
(3) seal clearance is easy to adjust, avoid impact and rub, by being arranged on acceleration transducer on the regulator plate and the intake and exhaust pressure regulating hole on the stuffing box gland, can monitor tribological failure, and can adjust gap between regulator plate and the honeycomb seal dish easily by changing pressure in the pressure chamber, dynamic and static gaps can reach optimum.
(4) because the existence of honeycomb seal dish, flow spiral shape is flowed and is cut off in the sealing, and the sealing gap direction is perpendicular to main direction of vibration, and insensitive to the radially sound off-centre of axle, the flow-induced vibration problem is greatly improved, near eliminating.
Description of drawings
Fig. 1 is radial ringed hybrid sealed structure chart;
Fig. 2 is radial ringed hybrid sealing schematic representation;
Fig. 3 is that radial ringed hybrid sealing Airflow Exciting-Vibration Force is analyzed schematic representation;
Among the figure, the 1st, airflow inlet, the 2nd, radial ring seal tooth, the 3rd, acceleration transducer, the 4th, supported spring, the 5th, regulator plate, the 6th, axial seal tooth, the 7th, Seal cage, the 8th, ripple joint, the 9th, pressure chamber, the 10th, honeycomb seal dish, the 11st, flow outlet, the 12nd, rotor, the 13rd, stuffing box gland, the 14th, pressure chamber exhaust port, the 15th, pressure chamber inlet hole.
Embodiment
A kind of radial ringed hybrid sealing, comprise: rotor 12 and be set in stuffing box gland 13 on the rotor 12, in stuffing box gland 13, be provided with regulator plate 5, regulator plate 5 links to each other with stuffing box gland 13 with supported spring 4 by the ripples joint 8 that is installed in the stuffing box gland 13, formed pressure chamber 9 between regulator plate 5 and the stuffing box gland 13, regulator plate 5 and be installed between the honeycomb seal dish 10 on the rotor 12 and formed Seal cage 7, be provided with ring packing tooth 2 and ring packing tooth 2 on the regulator plate 5 between honeycomb seal dish 10 and regulator plate 5, on regulator plate 5, be provided with acceleration transducer 3, on stuffing box gland 13, be provided with pressure chamber exhaust port 14 and pressure chamber inlet hole 15.
Shown in Figure 1, in rotating shaft, designed the honeycomb seal dish, honeycomb hole promptly is set on card.Respectively there is a regulator plate seal disc both sides, the ring packing that the array diameter does not wait has been installed on the regulator plate, gap between ring packing and the honeycomb seal dish can be regulated by regulating pressure in pressure cavity easily, and judge whether to bump mill by the acceleration transducer that is located on the regulator plate, if friction phenomenon occurs, then can reduce pressure chamber pressure by regulating pressure chamber inlet hole aperture, increase the gap, avoid friction, it is optimum that dynamic and static gaps can reach.Radially the ring packing tooth of Bu Zhiing and honeycomb seal dish are combined to form mixes the leakage rate that sealing can effectively reduce sealing in the rotating machinery (as steam turbine, compressor etc.), and can significantly improve the anti-flow-induced vibration ability of sealing, reaches the synergy effectiveness in vibration suppression.
As shown in Figure 3, under the honeycomb seal dish intercepted, gas mainly radially flowed in the novel sealing, is hindered by the honeycomb seal dish in the flow leakage process, and form a large amount of whirlpools in honeycomb, had increased dissipation effect, and had avoided air-flow helical flow phenomenon vertically.Rotor oscillation direction (x direction and y direction) is vertical with seal clearance adjustment direction (z direction), therefore rotor oscillation and eccentric very little to the sealability influence, the Seal cage internal pressure to the rotor effect mainly vertically, seal disc both sides gas flow direction is opposite, two sidewind power can partial offset, therefore, Airflow Exciting-Vibration Force can be very little, and the main cause that Airflow Exciting-Vibration Force produces is eliminated.

Claims (3)

1. radial ringed hybrid sealing, comprise: rotor (12) and be set in stuffing box gland (13) on the rotor (12), on stuffing box gland (13), be provided with pressure chamber exhaust port (14) and pressure chamber inlet hole (15), in described stuffing box gland (13), be provided with regulator plate (5) and ripple joint (8), one end of described ripple joint (8) is fixed on the stuffing box gland, the other end of ripple joint (8) is connected with described regulator plate (5), formed pressure chamber (9) between regulator plate (5) and the stuffing box gland (13), it is characterized in that, described rotor (12) is provided with honeycomb seal dish (10), this honeycomb seal dish (10) is positioned in the middle of the described regulator plate (5), has formed Seal cage (7) between regulator plate (5) and the honeycomb seal dish (10).
2. radial ringed hybrid sealing according to claim 1 is characterized in that: also be provided with supported spring (4) between described stuffing box gland and regulator plate (5).
3. radial ringed hybrid sealing according to claim 1, it is characterized in that: on regulator plate (5), be provided with ring packing tooth (2), and this ring packing tooth (2) is positioned between honeycomb seal dish (10) and the regulator plate (5), is provided with acceleration transducer (3) on regulator plate (5).
CN2011100886644A 2011-04-11 2011-04-11 Radial annular mixed seal Pending CN102207198A (en)

Priority Applications (1)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102619577A (en) * 2012-04-06 2012-08-01 东南大学 Device for inhibiting clearance leakage of blade tip and reducing steam flow exciting force
CN103591299A (en) * 2013-11-20 2014-02-19 东南大学 Orthogonal embedded sealing method and device for blocking spiral flow phenomenon
CN110985433A (en) * 2019-12-30 2020-04-10 蓝箭航天空间科技股份有限公司 Adjustable and controllable dynamic sealing device for turbine pump and turbine pump set
CN114483211A (en) * 2022-03-03 2022-05-13 南京航空航天大学 Sealing device for reducing gap leakage

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030147782A1 (en) * 2000-09-13 2003-08-07 Rolf Bruck Assembly having a honeycomb body and a shortened, slit, inner casing tube
CN1683766A (en) * 2004-04-14 2005-10-19 通用电气公司 Flexible seal assembly between gas turbine components and methods of installation
CN1707110A (en) * 2004-06-11 2005-12-14 云晓璎 Rotor pump
CN201225402Y (en) * 2008-07-11 2009-04-22 中国石油化工股份有限公司 Adjustable automatic following and cellular compound oil seal
CN201461958U (en) * 2009-06-15 2010-05-12 北京中智渝桐节能设备有限公司 Floating metal cellular seal
CN101776148A (en) * 2010-03-19 2010-07-14 东南大学 Radial ring seal
CN101858230A (en) * 2009-04-06 2010-10-13 通用电气公司 Method, system and/or device about the sealed department that is used for turbogenerator
CN201973243U (en) * 2011-04-11 2011-09-14 东南大学 Radial annular mixing sealing

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030147782A1 (en) * 2000-09-13 2003-08-07 Rolf Bruck Assembly having a honeycomb body and a shortened, slit, inner casing tube
CN1683766A (en) * 2004-04-14 2005-10-19 通用电气公司 Flexible seal assembly between gas turbine components and methods of installation
CN1707110A (en) * 2004-06-11 2005-12-14 云晓璎 Rotor pump
CN201225402Y (en) * 2008-07-11 2009-04-22 中国石油化工股份有限公司 Adjustable automatic following and cellular compound oil seal
CN101858230A (en) * 2009-04-06 2010-10-13 通用电气公司 Method, system and/or device about the sealed department that is used for turbogenerator
CN201461958U (en) * 2009-06-15 2010-05-12 北京中智渝桐节能设备有限公司 Floating metal cellular seal
CN101776148A (en) * 2010-03-19 2010-07-14 东南大学 Radial ring seal
CN201973243U (en) * 2011-04-11 2011-09-14 东南大学 Radial annular mixing sealing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102619577A (en) * 2012-04-06 2012-08-01 东南大学 Device for inhibiting clearance leakage of blade tip and reducing steam flow exciting force
CN102619577B (en) * 2012-04-06 2015-06-10 东南大学 Device for inhibiting clearance leakage of blade tip and reducing steam flow exciting force
CN103591299A (en) * 2013-11-20 2014-02-19 东南大学 Orthogonal embedded sealing method and device for blocking spiral flow phenomenon
CN110985433A (en) * 2019-12-30 2020-04-10 蓝箭航天空间科技股份有限公司 Adjustable and controllable dynamic sealing device for turbine pump and turbine pump set
CN114483211A (en) * 2022-03-03 2022-05-13 南京航空航天大学 Sealing device for reducing gap leakage

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Application publication date: 20111005