CN109973656A - From centering stern shaft seal gland - Google Patents

From centering stern shaft seal gland Download PDF

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Publication number
CN109973656A
CN109973656A CN201910331248.9A CN201910331248A CN109973656A CN 109973656 A CN109973656 A CN 109973656A CN 201910331248 A CN201910331248 A CN 201910331248A CN 109973656 A CN109973656 A CN 109973656A
Authority
CN
China
Prior art keywords
seat
stationary
ring
stern
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.)
Pending
Application number
CN201910331248.9A
Other languages
Chinese (zh)
Inventor
高峰
曹海建
张志谊
叶华
徐贞高
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.)
DONGTAI MARINE PARTS Co Ltd
Original Assignee
DONGTAI MARINE PARTS Co Ltd
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 DONGTAI MARINE PARTS Co Ltd filed Critical DONGTAI MARINE PARTS Co Ltd
Priority to CN201910331248.9A priority Critical patent/CN109973656A/en
Publication of CN109973656A publication Critical patent/CN109973656A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/32Other parts
    • B63H23/34Propeller shafts; Paddle-wheel shafts; Attachment of propellers on shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/162Special parts or details relating to lubrication or cooling of the sealing itself
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/3204Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings with at least one lip
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/40Sealings between relatively-moving surfaces by means of fluid

Abstract

It is of the invention from centering stern shaft seal gland, including the rotating seat being anchored on stern tube shaft, moving sealing ring is fixedly installed on rotating seat, rotating support has stationary ring bracket on the rotating seat, the stationary ring bracket is fixedly connected with seal receptacle, it is movably installed with stationary seat on seal receptacle, stationary ring pressure spring is supported between seal receptacle and stationary seat, the rotary centerline of the rotating seat, stationary ring bracket and stationary seat is on same straight line;The stationary seal ring and moving sealing ring being fixedly installed on stationary seat constitute end face seal pair;One end of seal receptacle and flexibility connection pipe is mutually connected, the other end and ship stern seat of flexibility connection pipe are mutually connected, the rear end for the ship stern seat being placed on stern tube shaft is fixedly installed with blanket gas placenta, embedded with sealing pneumatic tyre on the blanket gas placenta, the tire that the air inflation nozzle being installed on blanket gas placenta leads to sealing pneumatic tyre is intracavitary.The sealing device ensure that moving sealing ring, stationary ring rotate coaxially always, and the two position is fixed, and sealing effect is stablized.

Description

From centering stern shaft seal gland
Technical field
The present invention relates to the stern shaft seal glands of marine propulsion shafting more particularly to one kind can follow stern tube shaft axial float Or the face seals of radial displacement.
Background technique
Stern tube shaft is the important component on ship, and one end connects propeller, other end tooth connection roller box or shaft coupling again with Engine is connected, to prevent seawater from penetrating into cabin along stern tube shaft, it is necessary to by stern shaft seal gland to the stern tube shaft for passing through cabin Strict sealing is carried out, to ensure safety of ship, efficient operation.
End surface of screw shaft of ship mechanical sealing structure is currently used screw shaft of ship water sealing device, stern shaft seal dress Setting includes the opposite stationary seal ring and moving sealing ring slided, and stationary seal ring is installed on stationary seal ring seat, and the stationary seal ring seat is again It is fixed on hull stern tube socket by elastic compensating body and sealing device mounting seat;And moving sealing ring then passes through moving sealing ring seat It is anchored on screw shaft of ship with components such as transmission snap rings.Due in existing stern tube shaft end surface mechanical sealing structure stationary seal ring with Sealing device mounting seat (or cabin body) keeps relatively fixed state, and moving sealing ring is then in solid with the screw shaft of ship of rotation Determine connection status, i.e. stationary seal ring is mutually fixed with mounting seat, and moving sealing ring is then servo-actuated with stern tube shaft, not can avoid dynamic and static ring Between play to axial and circular runout.
The revolution of propeller for vessels both can generate propulsive force to ship, but also stern tube shaft generates periodic vibration and flexure, And cause reciprocal axial float, and axial float of the stern tube shaft with respect to cabin and circular runout, necessarily cause existing end face seal to fill Set the variation of axial seal and the drift or oscillation of sealing surface position, thus deteriorate stern tube shaft end surface mechanical sealing working environment and Sealing performance.It will lead between rotating ring and stationary ring in the play of stern tube shaft in existing structure and bounce first and irregular sealing occur Gap variation, since this irregular gap variation has the higher characteristic of the frequency, the response speed of elastic compensating part is difficult to The variation in the gap is compensated, so that the sealing performance decline and sealing performance between rotating ring and stationary ring is unstable, water is caused to leak And lose sealing effect.Secondly the relatively radially bounce between this dynamic and static ring and axial float, increase the mill between sealing surface Speed and abrasion loss are damaged, the damage and failure of end surface mechanical sealing are not only accelerated, but also similarly will lead between sealing cooperation Gap increases, and water leakage rate increases.Furthermore play and bounce, moving sealing ring and stationary seal ring structure with stern tube shaft with respect to ship cabin At sealing contact surface position be always formed radially random drift in the two, or even form oscillation, lead to palette face position Set unstable, increase water leakage probability, reduction sealing performance.Therefore existing stern tube shaft end face mechanical sealing device is due to intrinsic Fault of construction, so that there is play and circular runout to axial with not can avoid between stationary seal ring and moving sealing ring, it is this Being not fixed for dynamic and static ring relative position necessarily causes sealing performance unstable, and sealing effect reduces, and service life is short, or even meeting There is catching phenomenon.
Summary of the invention
For above-mentioned deficiency present in the prior art, technical problem to be solved by the invention is to provide a kind of sealing is dynamic Ring, stationary ring position are fixed, and sealing effect is stable from centering stern shaft seal gland.
In order to solve the above-mentioned technical problem, of the invention from centering stern shaft seal gland, it is dynamic on stern tube shaft including being anchored on Ring seat is fixedly installed with moving sealing ring on rotating seat, and rotating support has stationary ring bracket on the rotating seat, the stationary ring bracket with Seal receptacle is fixedly connected, and stationary seat is movably installed on seal receptacle, and stationary ring pressure spring, institute are supported between seal receptacle and stationary seat The rotary centerline for stating rotating seat, stationary ring bracket and stationary seat is on same straight line;The sealing being fixedly installed on stationary seat Stationary ring and moving sealing ring constitute end face seal pair;One end of seal receptacle and flexibility connection pipe is mutually connected, the other end of flexibility connection pipe It is mutually connected with ship stern seat, the rear end for the ship stern seat being placed on stern tube shaft is fixedly installed with blanket gas placenta, the blanket gas placenta Upper to be embedded with sealing pneumatic tyre, the tire that the air inflation nozzle being installed on blanket gas placenta leads to sealing pneumatic tyre is intracavitary.
In said structure, since the stationary seat for being equipped with stationary seal ring is supported on by seal receptacle and stationary ring holder pivots Rotating seat, and the rotary centerline of rotating seat, stationary ring bracket and stationary seat is on same straight line, the stationary seat of stationary seal ring It is to be fixed on stern tube shaft by rotating seat, this allows for the rotating ring for constituting end face seal pair and stationary ring relative position is protected always It holds constant, forms the follower structure of rotating ring and stationary ring, the end face seal pair that dynamic and static ring is constituted is not opposite between by stern tube shaft and cabin The influence of axial float and circular runout not only effectively prevents the irregular eccentric wear between rotating ring, stationary ring, but also keeps dynamic and static Ring fits closely always, there is sealing performance to stablize, significant advantage with long service life.Again since flexibility connection pipe one end is fixed in On the attachment base of end face, the other end and ship stern seat are mutually connected, which has not only blocked leakage of the water into ship cabin, and And axial float of the stern tube shaft with respect to ship cabin and circular runout can be fully compensated, it is entirely avoided because of stern between stern tube shaft and cabin The influence of axis rotary vibration, hull and stern tube shaft deflection deformation to face seals, it is ensured that face seals are run on well Working condition in.Also due to ship stern seat is placed on stern tube shaft, so that the bearing state of stern tube shaft is effectively improved, even if hull Stern deforms, and is also easy to adjustment stern tube shaft position;The structure also effectively simplifies stern tube shaft mounting process simultaneously, eliminates Complicated stern tube shaft hole bore hole process;It is fixedly installed on the blanket gas placenta of stern tube shaft base rear end embedded with sealing pneumatic tyre and inflation Mouth, the structure can not only be used for low speed operation sealing and safeguard sealing again convenient for forming shafting.
The preferred embodiment of the present invention, the stationary ring bracket is by stationary ring bracket bearing rotating support on rotating seat. Guarantee Positive rotational of the stationary ring bracket on rotating seat.
Further embodiment of the invention, the stationary seat being socketed on seal receptacle can slide axially, in seal receptacle and Sealing ring is provided in the set junction of stationary seat.The structure ensure that the dynamic and static ring of sealing is reliably axially bonded, effective to be formed End face seal pair.
The preferred embodiment of the present invention, the seal receptacle are placed on stern tube shaft, which passes through sealing device flange It is mutually connected with flexibility connection pipe.The ship stern seat is fixedly connected with by ship stern seat flange with flexibility connection pipe.Facilitate flexibility connection pipe with Tight connecting seat and ship stern seat are connected and fixed.
Further embodiment of the invention is provided with rotating ring pin, the sealing between the moving sealing ring and rotating seat Stationary ring pin is set between stationary ring and stationary seat.The relative rotation of dynamic and static ring can effectively be driven.
The preferred embodiment of the present invention is equipped with cooling water nozzle on the seal receptacle, on the sealed seat of the cooling water nozzle Cooling water channel lead to moving sealing ring and stationary seal ring.The frictional heat that sealing pair is taken away by cooling water guarantees the close of sealing pair Sealing property.
The preferred embodiment of the present invention, the flexibility connection pipe are metal bellows or rubber bellows.Using bellows Structure can be realized the compensation of axial direction, radial displacement.
The preferred embodiment of the present invention, the blanket gas placenta seals pneumatic tyre embedded with two column, on blanket gas placenta Two air inflation nozzles are at least installed, each column sealing pneumatic tyre is corresponding with an air inflation nozzle.Pneumatic tyre structure, Ke Yifen are sealed using two column It Shi Xian not high-low pressure inflation.
Further embodiment of the invention is pressed with lip packing by sealing gland in the rear end of blanket gas placenta Circle.Silt in outside water can be effectively obstructed to invade.
Detailed description of the invention
The present invention is described further from centering stern shaft seal gland with reference to the accompanying drawings and detailed description.
Fig. 1 is of the invention from a kind of the schematic diagram of the section structure of specific embodiment of centering stern shaft seal gland;
Fig. 2 is the enlarged diagram of end face seal structure in structure shown in Fig. 1.
In figure, 1-moving sealing ring, 2-rotating ring pins, 3-rotating seats, 4-stationary ring bracket bearings, 5-bearing inner shield rings, The outer retaining ring of 6-bearings, 7-stationary ring brackets, 8-stationary seal rings, 9-stationary ring pressing rings, 10-stationary ring pins, 11-stationary seats, 12- Sealing ring, 13-stationary ring pressure springs, 10-seal receptacles, 15-sealing device flanges, 16-flexibility connection pipes, 17-stern tube shafts, 18-ships Stern seat flange, 19-ship stern seats, 20-blanket gas placentas, 21-air inflation nozzles, 22-sealing pneumatic tyres, 23-sealing glands, 24- Lip-type packing, 25-cooling water nozzles, 26-cooling water channels.
Specific embodiment
It is as shown in Figure 1 and Figure 2 from centering stern shaft seal gland, which includes being fixedly installed on stern tube shaft 17 Rotating seat 3, the rotating seat 3 is rotated with stern tube shaft 17 when work.Moving sealing ring 1, moving sealing ring are embedded in the rear end face of rotating seat 3 1 using copper alloy as material.Several rotating ring pins 2 are fitted between moving sealing ring 1 and rotating seat 3, rotating ring pin 2 makes moving sealing ring 1 rotates together with rotating seat 3.
Stationary ring bracket bearing 4 is fixedly installed with by bearing inner shield ring 5 on rotating seat 3, which is rolling Dynamic ball bearing;Stationary ring bracket 7 is set on stationary ring bracket bearing 4, be fixedly connected with the outer retaining ring 6 of bearing on stationary ring bracket 7 and It is allowed to axially position.The other end of stationary ring bracket 7 is mutually permanently connected with seal receptacle 14, which is placed in stern tube shaft 17 On.Due to maintaining gap between seal receptacle 14 and stern tube shaft 17, seal receptacle 14 is by stationary ring bracket 7 and stationary ring bracket 4 rotating support of bearing is on rotating seat 3;And the center of rotation of seal receptacle 14, stationary seat 11, stationary ring bracket 7 and rotating seat 3 Line is on same straight line.
Slip is set with stationary seat 11 dynamicly on seal receptacle 14, sets in the set junction of seal receptacle 14 and stationary seat 11 It is equipped with sealing ring 12.Several stationary ring pressure springs 13 are supported between seal receptacle 14 and stationary seat 11, stationary ring pressure spring 13 is cylinder pressure Contracting spring.Stationary seal ring 8 is pressed with by stationary ring pressing ring 9 on stationary seat 11, stationary seal ring 8 using hard alloy as material, Several stationary ring pins 10 are fitted between stationary seal ring 8 and stationary seat 11.Moving sealing ring 1 and stationary seal ring 8 mutually can be slided circumferentially It fits closely dynamicly and constitutes end face seal pair, and rotate coaxially always.
Seal receptacle 14 and one end of flexibility connection pipe 16 are mutually permanently connected by sealing device flange 15.Flexibility connection pipe 16 is adopted With metal bellows, can also using rubber bellows etc., common bellows, the flexibility connection pipe 16 are placed in stern tube shaft in the market On 17 axis periphery.It is mutually connected in the other end of flexibility connection pipe 16 by ship stern seat flange 18 and ship stern seat 19, ship stern seat 19 Also it is placed on 17 periphery of stern tube shaft, blanket gas placenta 20 is fixedly installed in the rear end of ship stern seat 19, on blanket gas placenta 20 Pneumatic tyre 22 is sealed embedded with two column by the pressing ring of two sides.In the rear end of blanket gas placenta 20, by gland 23, to be pressed with lip shape close Seal 24.Two air inflation nozzles 21 are installed on blanket gas placenta 20, each column sealing pneumatic tyre 22 is accordingly communicated with an inflation Mouth 21.
It is screwed with cooling water nozzle 25 on seal receptacle 14, is additionally provided with cooling water channel 26 on seal receptacle 14, it is cooling when work Water is after cooling water nozzle 25, cooling water channel 26 flow through the sealing surface that moving sealing ring 1 and stationary seal ring 8 are constituted, then along stern tube shaft surface Gap outflow.
It is above-mentioned only to have enumerated a kind of preferred embodiment of the invention, but the present invention is not limited thereto, as long as end face is close It seals secondary rotating ring and stationary ring to be bonded to each other, and remains that confronting coaxial rotates, should all fall within the scope of protection of the present invention.

Claims (10)

1. a kind of from centering stern shaft seal gland, including the rotating seat (3) being anchored on stern tube shaft, the fixed peace on rotating seat (3) Equipped with moving sealing ring (1), it is characterised in that: rotating support has stationary ring bracket (7) on the rotating seat (3), the stationary ring bracket (7) It is fixedly connected, is movably installed on seal receptacle (14) stationary seat (11) with seal receptacle (14), seal receptacle (14) and stationary seat (11) be supported between stationary ring pressure spring (13), the rotating seat (3), stationary ring bracket (7) and stationary seat (11) rotary centerline On same straight line;The stationary seal ring (8) being fixedly installed on stationary seat (11) and moving sealing ring (1) constitute end face seal It is secondary;One end of seal receptacle (14) and flexibility connection pipe (16) is mutually connected, the other end and ship stern seat (19) phase of flexibility connection pipe (16) It is mutually connected, the rear end for the ship stern seat (19) being placed on stern tube shaft (17) is fixedly installed with blanket gas placenta (20), the sealing pneumatic tyre Embedded with sealing pneumatic tyre (22) on seat (20), the air inflation nozzle (21) being installed on blanket gas placenta (20) leads to sealing pneumatic tyre (22) Tire it is intracavitary.
2. according to claim 1 from centering stern shaft seal gland, it is characterised in that: the stationary ring bracket (7) passes through quiet Ring support bearing (4) rotating support is on rotating seat (3).
3. according to claim 1 from centering stern shaft seal gland, it is characterised in that: be socketed on quiet on seal receptacle (14) Ring seat (11) can slide axially, and be provided with sealing ring (12) in the set junction of seal receptacle (14) and stationary seat (11).
4. according to claim 1 from centering stern shaft seal gland, it is characterised in that: the seal receptacle (14) is placed in stern On axis (17), which is mutually connected by sealing device flange (15) and flexibility connection pipe (16).
5. according to claim 1 or 4 from centering stern shaft seal gland, it is characterised in that: the ship stern seat (19) passes through Ship stern seat flange is fixedly connected with flexibility connection pipe (16).
6. according to claim 1 from centering stern shaft seal gland, it is characterised in that: the moving sealing ring (1) and rotating ring It is provided with rotating ring pin (2) between seat (3), stationary ring pin (10) is set between the stationary seal ring (8) and stationary seat (11).
7. according to claim 1 from centering stern shaft seal gland, it is characterised in that: be equipped on the seal receptacle (14) Cooling water nozzle (25), the cooling water channel (26) on cooling water nozzle (25) the sealed seat (14) lead to moving sealing ring (11) and sealing Stationary ring (8).
8. according to claim 1 from centering stern shaft seal gland, it is characterised in that: the flexibility connection pipe (16) is metal Bellows or rubber bellows.
9. according to claim 1 from centering stern shaft seal gland, it is characterised in that: the blanket gas placenta (20) is embedded in There are two column to seal pneumatic tyre (22), two air inflation nozzles (21) are at least installed on blanket gas placenta (20), each column seals pneumatic tyre (22) air inflation nozzle (21) are corresponding with.
10. according to claim 1 from centering stern shaft seal gland, it is characterised in that: after blanket gas placenta (20) End is pressed with lip-type packing (24) by sealing gland (23).
CN201910331248.9A 2019-04-24 2019-04-24 From centering stern shaft seal gland Pending CN109973656A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910331248.9A CN109973656A (en) 2019-04-24 2019-04-24 From centering stern shaft seal gland

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910331248.9A CN109973656A (en) 2019-04-24 2019-04-24 From centering stern shaft seal gland

Publications (1)

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CN109973656A true CN109973656A (en) 2019-07-05

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Country Status (1)

Country Link
CN (1) CN109973656A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114633865A (en) * 2022-03-02 2022-06-17 中国船舶重工集团公司第七一九研究所 Magnetically supported flexible propulsion shaft system and ship

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201187580Y (en) * 2008-04-25 2009-01-28 东台船用配件有限公司 Metal composite ring type water lubricating trailing axle seal device
CN201915909U (en) * 2010-12-10 2011-08-03 丹东波纹管密封有限公司 Screw oil pumping unit seal
CN209990908U (en) * 2019-04-24 2020-01-24 东台船用配件有限公司 Self-centering stern shaft sealing device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201187580Y (en) * 2008-04-25 2009-01-28 东台船用配件有限公司 Metal composite ring type water lubricating trailing axle seal device
CN201915909U (en) * 2010-12-10 2011-08-03 丹东波纹管密封有限公司 Screw oil pumping unit seal
CN209990908U (en) * 2019-04-24 2020-01-24 东台船用配件有限公司 Self-centering stern shaft sealing device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114633865A (en) * 2022-03-02 2022-06-17 中国船舶重工集团公司第七一九研究所 Magnetically supported flexible propulsion shaft system and ship
CN114633865B (en) * 2022-03-02 2023-10-27 中国船舶重工集团公司第七一九研究所 Magnetically supported flexible propulsion shafting and vessel

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