CN207471096U - A kind of quick filling tailing axle is by the device of army cap lubricant grease - Google Patents

A kind of quick filling tailing axle is by the device of army cap lubricant grease Download PDF

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Publication number
CN207471096U
CN207471096U CN201721540855.9U CN201721540855U CN207471096U CN 207471096 U CN207471096 U CN 207471096U CN 201721540855 U CN201721540855 U CN 201721540855U CN 207471096 U CN207471096 U CN 207471096U
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CN
China
Prior art keywords
cylinder
driving
linkage
piston
inner cavity
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Withdrawn - After Issue
Application number
CN201721540855.9U
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Chinese (zh)
Inventor
杨俊东
邝学军
李德朝
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Guangzhou Wenchong Shipbuilding Co ltd
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Boat In Guangzhou Wenchong Dock Co Ltd
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Priority to CN201721540855.9U priority Critical patent/CN207471096U/en
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Publication of CN207471096U publication Critical patent/CN207471096U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of quick filling tailing axle is by the device of army cap lubricant grease, including sequentially connected grease tank, greasing cylinder, driving cylinder and linkage air cylinder, the grease bottom of the barrel connects fixation at the top of greasing cylinder by connecting rod, the cylinder bottom concatenation driving cylinder of the greasing cylinder, the driving cylinder bottom connect fixation at the top of the linkage air cylinder by connecting rod;The inner cavity of the greasing cylinder is connected with the inner cavity of driving cylinder, and is provided with first piston component in the inner cavity of the greasing cylinder and driving cylinder;The inner cavity of the driving cylinder is connected with the inner cavity of linkage air cylinder, and is provided with second piston component in the inner cavity of the driving cylinder and linkage air cylinder;Concatenation one at the top of the bottom of the first piston component and second piston component, and can synchronize reciprocating in the greasing cylinder, driving cylinder and linkage air cylinder.The present apparatus greatly promotes the injection efficiency of grease by being aspirated to form certain vacuum degree by linkage air cylinder by army cap inner cavity when concatenation linkage air cylinder drives cylinder operation on driving cylinder.

Description

A kind of quick filling tailing axle is by the device of army cap lubricant grease
Technical field
The utility model is related to Ship's Repair field more particularly to a kind of quick filling tailing axles by the dress of army cap lubricant grease It puts.
Background technology
It is a hemispheric interior empty cap body for being set in marine rear shaft end by army cap, at present in Ship's Repair industry In, after the shafting maintenance installation of every ship, it is required for that a large amount of lubricant grease is perfused in the inner cavity by army cap to prevent tail The seawater corrosion that axis and nut are compromised protects tailing axle and nut by the way that the sealing of grease in army cap inner cavity is coated.By In general's cap bulky on marine shafting, cavity volume is big, and army cap is needed several barrels of greases by perfusion one, general Manual grease method for implanting needs a large amount of manpower and materials, inefficiency.A kind of Normal practice is that the common oil pressure pump of borrow is past Lubricant grease will be perfused in army cap inner cavity, but lubricant grease is different from common fluid oil after all, in entirely perfusion grease mistake Heavy workload that time-consuming in journey, easily fever leads to mechanical breakdown to common oil pressure pump, along with the general of various different models The inner cavity capacity of cap is different, it is often necessary to replace the oil pressure pump of different model grease is perfused to by army cap, seriously affect work Efficiency.
Utility model content
The purpose of the utility model is to overcome shortcoming and deficiency of the prior art, and providing a kind of quick filling tailing axle will The device of army cap lubricant grease is linked army cap inner cavity when concatenation linkage air cylinder to drive cylinder operation on driving cylinder Cylinder-suction forms certain vacuum degree, greatly promotes the injection efficiency of grease.
The utility model is achieved through the following technical solutions:A kind of quick filling tailing axle is by the dress of army cap lubricant grease It puts, including a sequentially connected grease tank from top to bottom, a greasing cylinder, a driving cylinder and a linkage air cylinder, the grease tank Bottom connects fixation, the cylinder bottom concatenation driving cylinder of the greasing cylinder, the driving cylinder bottom at the top of greasing cylinder by connecting rod Portion connects fixation at the top of the linkage air cylinder by connecting rod;The inner cavity of the greasing cylinder is connected with the inner cavity of driving cylinder, and A shared first piston component is provided in the inner cavity of the greasing cylinder and driving cylinder;The inner cavity of the driving cylinder and linkage The inner cavity connection of cylinder, and a shared second piston component is provided in the inner cavity of the driving cylinder and linkage air cylinder;It is described Concatenation one at the top of the bottom of first piston component and second piston component, and can synchronize the greasing cylinder, driving cylinder and It is reciprocating in linkage air cylinder.
Further, a grease entrance and a grease outlets are provided at the top of the greasing cylinder, which passes through one First check-valve is connected to the grease tank, which is connected to by a second check-valve by army cap pouring orifice;The note The cylinder bottom center of fat cylinder is provided with a First piston bar pilot hole and is connected with the driving cylinder, the First piston bar pilot hole Side is provided with one first driving stomata, which is also connected to driving cylinder, the bottom end of the casing wall of the greasing cylinder A greasing cylinder stomata is provided with, which is connected to the inner cavity of greasing cylinder.
Further, the cylinder bottom center of the driving cylinder is provided with a second piston bar pilot hole, second piston bar dress Distribution side is provided with the inner cavity that one second driving stomata is connected to driving cylinder;It is provided on the outer wall of the driving cylinder on the other hand Dynamic driving reversal valve, the driving reversal valve include three-way connection, which connects described the by the first driving tracheae One driving stomata connects the second driving stomata by the second driving tracheae, tracheae is driven to connect compressed air by third Air source.
Further, the cylinder top center of the linkage air cylinder is provided with a third piston rod pilot hole, in the third piston rod Pilot hole side is provided with one first linkage stomata, which is connected in the inner cavity of linkage air cylinder;In linkage gas The cylinder bottom of cylinder be provided with one second linkage stomata with first linkage stomata it is opposite, this second link stomata be also connected to linkage air cylinder Inner cavity in;A manually linkage reversing valve is provided on the outer wall of the linkage air cylinder, which includes three-way connection, The three-way connection connects the first linkage stomata, by the second linkage tracheae connection described second by the first linkage tracheae Take offence hole, by third link tracheae be connected to army cap exhaust outlet.
Further, the first piston component, including the first piston in the First piston bar pilot hole Bar, the First piston bar upper end are located in the inner cavity of the greasing cylinder and lower end and are located in the inner cavity of the driving cylinder;This One piston rod upper end is fixedly installed first piston head, which is fixedly installed second piston head;Institute It states first piston head and the bore seal of the greasing cylinder is isolated into first cavity on top and the second cavity of lower part, described The bore seal of the driving cylinder is isolated into the 4th cavity of the third cavity and lower part on top by two piston heads;Described second Cavity connects the greasing cylinder stomata;The third cavity is connected by the described first driving stomata, the first driving tracheae To the driving reversal valve;4th cavity is connected to described by the described second driving stomata, the second driving tracheae Drive reversal valve.
Further, the second piston component is mounted on the second piston bar pilot hole and third piston including one Second piston bar in bar pilot hole;The second piston bar upper end is located in the 4th cavity and lower end is located at the linkage gas In the inner cavity of cylinder;The second piston bar upper end is fixedly installed third piston head, second piston bar lower end fixed setting There is the 4th piston head;At the top of the third piston head fixation is connect with the second piston head bottom;4th piston head will The bore seal of the linkage air cylinder is isolated into the 5th cavity on top and the 6th cavity of lower part;5th cavity passes through institute State the first linkage stomata, it is described first linkage tracheae be connected to the linkage reversing valve, the 6th cavity passes through described second Linkage stomata, the second linkage tracheae are connected to the linkage reversing valve.
Further, an exhaust cover board is provided in the grease tank, the center of the exhaust cover board is vertically provided with an exhaust Conduit, the exhaust manifolds connect the inner cavity of grease tank, a rubber plug are provided in the exhaust manifolds.
Further, the linkage reversing valve connects the driving reversal valve by a linkage reversing handle.
Further, the First piston bar pilot hole, second piston bar pilot hole and third piston rod pilot hole it is coaxial and Aperture is identical;The First piston bar and second piston bar it is coaxial and respectively Matching installation in First piston bar pilot hole, second In piston rod pilot hole and third piston rod pilot hole.
Relative to the prior art, the advantageous effect of this case is:
1., the quick filling tailing axle of this case by the device of army cap lubricant grease, pass through the concatenation linkage gas on driving cylinder Cylinder, and cylinder is driven to connect the third linkage tracheae of army cap pouring orifice, linkage air cylinder by oil fuel tube connection and arranges army cap Gas port so that drive cylinder, linkage air cylinder and gas circuit will be recycled in the connecting line formation one of army cap, being given when driving cylinder will While army cap injects grease, linkage air cylinder is aspirated the air inside army cap so that army cap inner cavity is formed to certain vacuum Degree, can greatly promote the injection rate of grease in this way, and grease injection efficiency is high;
2., pass through the reversing handle connection driving reversal valve and linkage reversing valve that links so that driving reversal valve is changed with linkage It is synchronized to the gas circuit handover operation of valve, it is easy to operate, it can effectively reduce the manpower and materials of grease implant operation;
3., be provided with peephole on the operational platform, observed the injection rate of grease in army cap, avoided by peephole Since grease spilling causes to waste;Meanwhile drive cylinder and linkage air cylinder and can be along operation by the connecting line between army cap Platform is laid with, and avoids causing gas circuit obstructed due to pipeline bending, grease injection process is reliable.
In order to be able to apparent understanding the utility model illustrates the preferable of the utility model below with reference to description of the drawings Embodiment.
Description of the drawings
Structure diagram when Fig. 1 is the working condition of the utility model;
Fig. 2 is the structure diagram of the utility model.
Specific embodiment
In the description of the present invention, it is to be appreciated that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ", The orientation or position relationship of the instructions such as "front", "rear", "left", "right", " hard straight ", " level ", " top ", " bottom ", " interior ", " outer " are Based on orientation shown in the drawings or position relationship, it is for only for ease of description the utility model and simplifies description rather than instruction Or imply that signified device or element there must be specific orientation, with specific azimuth configuration and operation, therefore be not understood that For the limitation to the utility model.In the description of the present invention, unless otherwise indicated, " multiple " are meant that two or two More than a.
Please refer to Fig. 1 and Fig. 2, the quick filling tailing axle of this case by the device 3 of army cap lubricant grease, including by up to Under a sequentially connected grease tank 310, a greasing cylinder 320, one driving 330 and one linkage air cylinder 340 of cylinder, the grease tank 310 bottoms connect fixation, the cylinder bottom concatenation driving cylinder 330 of the greasing cylinder 320, institute with 320 top of greasing cylinder by connecting rod It states driving 330 bottom of cylinder and fixation is connected by connecting rod with 340 top of linkage air cylinder.The inner cavity of the greasing cylinder 320 and The inner cavity connection of cylinder 330 is driven, and first work shared is provided in the inner cavity of the greasing cylinder 320 and driving cylinder 330 Plug assembly 380;The inner cavity of the driving cylinder 330 is connected with the inner cavity of linkage air cylinder 340, and the driving cylinder 330 and linkage Shared second piston component 390 is provided in the inner cavity of cylinder 340.It lives the bottom of the first piston component 380 and second The top of plug assembly 390 concatenation one, and can synchronize make in the greasing cylinder 320, driving cylinder 330 and linkage air cylinder 340 it is past Multiple movement.
The grease tank 310, inside can hold lubricant grease 311, an exhaust cover board is provided in the grease tank 310 312, the exhaust cover board 312 is covered on lubricant grease 311 when holding lubricant grease 311 in grease tank 310, the exhaust cover board 312 center is vertically provided with an exhaust manifolds 313, which connects the inner cavity of grease tank 310, the exhaust manifolds A rubber plug 314 is provided in 313.In actual use, when which presses on the top surface of lubricant grease 311, grease The air inside air and grease in 310 inner cavities of bucket is discharged by exhaust manifolds 313 outside grease tank 310, blocks up tight rubber plug 314 just Extraneous air can be prevented to enter in grease tank 310 by exhaust manifolds 313.
The greasing cylinder 320, top are provided with a grease entrance 321 and a grease outlets 322, the grease entrance 321 The grease tank 310 is connected to by a first check-valve 7, which is connected to general by a second check-valve 8 Cap pouring orifice 21.The cylinder bottom center of the greasing cylinder 320 is provided with a First piston bar pilot hole 325 and the driving cylinder 330 Connection, the First piston bar pilot hole 325 are used to install the piston rod of first piston component 380.The First piston bar assembling One first driving stomata 326 is provided on the cylinder bottom of 325 side of hole, which is also connected to driving cylinder 330, which is used in driving cylinder 330 inject or discharge compressed air, to drive described first to live Plug assembly 380 moves back and forth.The bottom end of the casing wall of the greasing cylinder 320 is provided with a greasing cylinder stomata 327, the greasing cylinder stomata 327 are connected in the inner cavity of the greasing cylinder 320, when the first piston component 380 moves back and forth, inside the greasing cylinder 320 Air is sucked or is discharged by the greasing cylinder stomata 327.
The cylinder bottom of the driving cylinder 330, top and the greasing cylinder 320 concatenates, in the cylinder bottom of the driving cylinder 330 Centre is provided with a second piston bar pilot hole 335 for installing the piston rod of second piston component 390.The second piston bar is assembled One second driving stomata 336 is provided on the cylinder bottom of 335 side of hole to be connected in the inner cavity of driving cylinder 330.The driving cylinder One is provided on 330 outer wall and manually drives reversal valve 337, which includes three-way connection, the three-way connection The first driving stomata 326 is connected by the first driving tracheae 331, second drive is connected by the second driving tracheae 332 Take offence hole 336, by third drive tracheae 333 connect compressed air air source.In the present embodiment, which wraps The three-way connection included such as third driving tracheae 333 connection the first driving tracheae 331, then second drives tracheae in handover operation 332 connection extraneous airs;If third driving tracheae 333 connection second drives tracheae 332, then the first driving tracheae 331 connects outer Portion's air.
The linkage air cylinder 340 is fixed by connecting rod and the driving connection of cylinder 330, in the cylinder top of the linkage air cylinder 340 Centre is provided with a third piston rod pilot hole 345 for installing the piston rod of second piston component 390, the First piston bar dress Distribution 325, second piston bar pilot hole 335 and third piston rod pilot hole 345 are coaxial and aperture is identical, and First piston bar and Second piston bar is coaxial and Matching installation is lived in First piston bar pilot hole 325, second piston bar pilot hole 335 and third respectively In stopper rod pilot hole 345.345 side of third piston rod pilot hole is provided with one first on the cylinder top of linkage air cylinder 340 Link stomata 346, which is connected in the inner cavity of linkage air cylinder 340;It is set in the cylinder bottom of linkage air cylinder 340 It is equipped with one second linkage stomata 348 and first and links stomata 346 relatively, which is also connected to linkage air cylinder In 340 inner cavity.Manually linkage reversing valve 347, the linkage reversing valve 347 are provided on the outer wall of the linkage air cylinder 340 Including three-way connection, which connects the first linkage stomata 346, by second by the first linkage tracheae 341 Pipe 342 of taking offence connects the second linkage stomata 348, the tracheae 343 that linked by third is connected to army cap exhaust outlet 22.It is described Linkage reversing valve 347 connects the driving reversal valve 337 by a linkage reversing handle 349 so that the linkage reversing valve 347 It is synchronous in handover operation with the driving reversal valve 337.In the present embodiment, three-way connection which includes In handover operation, if third linkage tracheae 343 connects the first linkage tracheae 341, then the second linkage tracheae 342 connects external sky Gas;If third linkage tracheae 343 connects the second linkage tracheae 342, then the first linkage tracheae 341 connects extraneous air.
The first piston component 380, including the first piston being mounted vertically in the First piston bar pilot hole Bar 381,381 upper end of First piston bar are located in the inner cavity of the greasing cylinder 320 and lower end and are located at the driving cylinder 330 In inner cavity, which is fixedly installed first piston head, which fixes and set It is equipped with second piston head.The first piston head by the bore seal of the greasing cylinder 320 be isolated into top the first cavity A and Second cavity B of lower part;The bore seal of the driving cylinder 330 is isolated into the third cavity on top by the second piston head C and the 4th cavity D of lower part.The second cavity B connects the greasing cylinder stomata 327;The third cavity C passes through described One driving stomata 326, the first driving tracheae 331 are connected to the driving reversal valve 337;4th cavity D passes through institute State the second driving stomata 336, the second driving tracheae 332 is connected to the driving reversal valve 337.
The second piston component 390, including being mounted vertically in the second piston bar pilot hole 335 and third piston Second piston bar 391 in bar pilot hole 345.391 upper end of second piston bar is located at the described 4th of the driving cylinder 330 Cavity D is interior and lower end is located in the inner cavity of the linkage air cylinder 340.391 upper end of second piston bar is fixedly installed third Piston head, 391 lower end of second piston bar are fixedly installed the 4th piston head.The third piston head and first piston component The second piston head on 380 is fixedly connected so that the first piston component 380 and the second piston component 390 It moves back and forth and synchronizes;4th piston head by the bore seal of the linkage air cylinder 340 be isolated into top the 5th cavity E and 6th cavity F of lower part.The 5th cavity E is connected by the described first linkage stomata 346, the first linkage tracheae 341 To the linkage reversing valve 347;The 6th cavity F passes through the described second linkage stomata 348, the second linkage tracheae 342 It is connected to the linkage reversing valve 347.
The quick filling tailing axle of this case is as follows by the grease injecting principle of the device of army cap lubricant grease:
The first step:Third driving tracheae is connected to the air source of compressed air, third linkage tracheae is connected and is vented army cap Mouthful, second check-valve is connected to by oil fuel tube by army cap pouring orifice;
Second step:Operations linkage reversing handle causes compressed air by third driving tracheae, the second driving tracheae, second Driving stomata enters in the 4th cavity and first piston component and second piston component is driven gradually to go upward to highest stroke, this When, the air in the first cavity is discharged by second check-valve, the air in third cavity passes through the first driving stomata, first drives Air in pipe of taking offence discharge, the 5th cavity is discharged by the first linkage stomata, the first linkage tracheae.Meanwhile in grease tank Fill grease, and pass through be vented cover board, exhaust manifolds exclude grease tank inside air;
Third walks:Operations linkage reversing handle causes compressed air by third driving tracheae, the first driving tracheae, first Driving stomata enters in third cavity and first piston component and second piston component is driven gradually to come downwards to minimum stroke, this When, the air in the second cavity is discharged by the greasing cylinder stomata, the air in the 4th cavity passes through the second driving stomata, the Air in two driving tracheae discharges, the 6th cavity is discharged by the second linkage stomata, the second linkage tracheae.Meanwhile grease tank Interior grease is inhaled into first cavity, and army cap inner cavity is also sucked to form certain vacuum degree;
4th step:Operations linkage reversing handle causes compressed air by third driving tracheae, the second driving tracheae, second Driving stomata enters in the 4th cavity and first piston component and second piston component is driven gradually to go upward to highest stroke, this When, first check-valve is closed, second check-valve is opened, and the grease in the first cavity is injected by oil fuel tube will be in army cap.And And at this time by, since third step forms certain vacuum degree, while second piston component uplink, third links in army cap inner cavity Tracheae, the second linkage tracheae, the second linkage stomata connect the 6th cavity, and the low-pressure air in army cap inner cavity is sucked once more Into the 6th cavity, certain suction is formed, is injected so as to accelerate grease from the first cavity by the speed in army cap.Link gas Cylinder 340 is so that the injection efficiency of grease greatly promotes;
5th step:Operation switching linkage reversing handle repeatedly, repeats second step to the 4th step, by grease in by army cap Until filling or until the grease in grease tank exhausts.
It, can be in this quick filling tailing axle general since 1 end of marine rear shaft is huge by 2 shape of army cap in the present embodiment Fixed frame 4 is built in 3 one side of device of cap lubricant grease, and 2 one side of army cap is being built operating platform 5, and pacify on operating platform 5 Peephole 6 is filled, is observed by peephole 6 by the injection rate of grease in army cap 2, avoids causing to waste due to grease spilling.Together When, it connects third linkage tracheae and can be laid with the pipeline between army cap 2 along operating platform 5, avoid making due to pipeline bending It is obstructed into gas circuit.
The utility model is not limited to the above embodiment, if the various changes or deformation to the utility model do not take off Spirit and scope from the utility model, if these changes and deformation belong to the claims and equivalents of the utility model Within the scope of, then the utility model is also intended to comprising these changes and deformation.

Claims (10)

1. a kind of quick filling tailing axle is by the device of army cap lubricant grease, which is characterized in that including sequentially connected from top to bottom One grease tank, a greasing cylinder, a driving cylinder and a linkage air cylinder, the grease bottom of the barrel and greasing cylinder top are connected by connecting rod Fixation is connect, the cylinder bottom concatenation driving cylinder of the greasing cylinder, the driving cylinder bottom and linkage air cylinder top pass through company Bar connection is fixed;The inner cavity of the greasing cylinder is connected with the inner cavity of driving cylinder, and in the inner cavity of the greasing cylinder and driving cylinder It is provided with a shared first piston component;The inner cavity of the driving cylinder connects, and the driving gas with the inner cavity of linkage air cylinder A shared second piston component is provided in the inner cavity of cylinder and linkage air cylinder;It lives the bottom of the first piston component and second Concatenation one at the top of plug assembly, and can synchronize reciprocating in the greasing cylinder, driving cylinder and linkage air cylinder.
2. a kind of quick filling tailing axle as described in claim 1 is by the device of army cap lubricant grease, it is characterised in that:The note A grease entrance and a grease outlets are provided at the top of fat cylinder, which is connected to the oil by a first check-valve Fat bucket, the grease outlets are connected to by a second check-valve by army cap pouring orifice;The cylinder bottom center of the greasing cylinder is provided with one First piston bar pilot hole is connected with the driving cylinder, and the First piston bar pilot hole side is provided with one first driving gas Hole, the first driving stomata are also connected to driving cylinder, and the bottom end of the casing wall of the greasing cylinder is provided with a greasing cylinder stomata, the note Fat cylinder stomata is connected to the inner cavity of greasing cylinder.
3. a kind of quick filling tailing axle as claimed in claim 2 is by the device of army cap lubricant grease, it is characterised in that:The drive The take offence cylinder bottom center of cylinder is provided with a second piston bar pilot hole, which is provided with one second drive Take offence hole be connected to driving cylinder inner cavity;One, which is provided with, on the outer wall of the driving cylinder manually drives reversal valve, the driving Reversal valve includes three-way connection, which connects the first driving stomata by the first driving tracheae, driven by second Pipe of taking offence connection the second driving stomata, the air source that tracheae connection compressed air is driven by third.
4. a kind of quick filling tailing axle as claimed in claim 3 is by the device of army cap lubricant grease, it is characterised in that:It is described The take offence cylinder top center of cylinder is provided with a third piston rod pilot hole, and the third piston rod pilot hole side is provided with one first Link stomata, which is connected in the inner cavity of linkage air cylinder;The cylinder bottom of linkage air cylinder is provided with one second Taking offence, hole is opposite with the first linkage stomata, which is also connected in the inner cavity of linkage air cylinder;The linkage air cylinder A manually linkage reversing valve is provided on outer wall, which includes three-way connection, which passes through first Pipe of taking offence connection the first linkage stomata connects the second linkage stomata by the second linkage tracheae, is linked by third Tracheae is connected to army cap exhaust outlet.
5. a kind of quick filling tailing axle as claimed in claim 4 is by the device of army cap lubricant grease, it is characterised in that:Described One piston component, including the First piston bar in the First piston bar pilot hole, First piston bar upper end position In the inner cavity of the greasing cylinder and lower end be located at it is described driving cylinder inner cavity in;The First piston bar upper end is fixedly installed There is first piston head, which is fixedly installed second piston head;The first piston head is by the greasing The bore seal of cylinder is isolated into first cavity on top and the second cavity of lower part, and the second piston head is by the driving cylinder Bore seal be isolated into the third cavity on top and the 4th cavity of lower part;Second cavity connects the greasing cylinder gas Hole;The third cavity is connected to the driving reversal valve by the described first driving stomata, the first driving tracheae;It is described 4th cavity is connected to the driving reversal valve by the described second driving stomata, the second driving tracheae.
6. a kind of quick filling tailing axle as claimed in claim 5 is by the device of army cap lubricant grease, it is characterised in that:Described Two piston components, the second piston being mounted on including one in the second piston bar pilot hole and third piston rod pilot hole Bar;The second piston bar upper end is located in the 4th cavity and lower end is located in the inner cavity of the linkage air cylinder;Second work Stopper rod upper end is fixedly installed third piston head, which is fixedly installed the 4th piston head;Described At the top of three piston heads fixation is connect with the second piston head bottom;4th piston head is close by the inner cavity of the linkage air cylinder Envelope is isolated into the 5th cavity on top and the 6th cavity of lower part;5th cavity passes through the described first linkage stomata, described First linkage tracheae is connected to the linkage reversing valve, and the 6th cavity passes through the described second linkage stomata, described second Pipe of taking offence is connected to the linkage reversing valve.
7. a kind of quick filling tailing axle as claimed in claim 6 is by the device of army cap lubricant grease, it is characterised in that:The oil An exhaust cover board is provided in fat bucket, the center of the exhaust cover board is vertically provided with an exhaust manifolds, exhaust manifolds connection oil The inner cavity of fat bucket is provided with a rubber plug in the exhaust manifolds.
8. a kind of quick filling tailing axle as claimed in claim 6 is by the device of army cap lubricant grease, it is characterised in that:It is described Dynamic reversal valve connects the driving reversal valve by a linkage reversing handle.
9. a kind of quick filling tailing axle as claimed in claim 6 is by the device of army cap lubricant grease, it is characterised in that:Described One piston rod pilot hole, second piston bar pilot hole and third piston rod pilot hole is coaxial and aperture is identical.
10. a kind of quick filling tailing axle as claimed in claim 6 is by the device of army cap lubricant grease, it is characterised in that:It is described First piston bar and second piston bar it is coaxial and respectively Matching installation First piston bar pilot hole, second piston bar pilot hole and In third piston rod pilot hole.
CN201721540855.9U 2017-11-17 2017-11-17 A kind of quick filling tailing axle is by the device of army cap lubricant grease Withdrawn - After Issue CN207471096U (en)

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Application Number Priority Date Filing Date Title
CN201721540855.9U CN207471096U (en) 2017-11-17 2017-11-17 A kind of quick filling tailing axle is by the device of army cap lubricant grease

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Application Number Priority Date Filing Date Title
CN201721540855.9U CN207471096U (en) 2017-11-17 2017-11-17 A kind of quick filling tailing axle is by the device of army cap lubricant grease

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CN207471096U true CN207471096U (en) 2018-06-08

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CN201721540855.9U Withdrawn - After Issue CN207471096U (en) 2017-11-17 2017-11-17 A kind of quick filling tailing axle is by the device of army cap lubricant grease

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107747673A (en) * 2017-11-17 2018-03-02 广州中船文冲船坞有限公司 A kind of quick filling tailing axle is by the device of army cap lubricant grease

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107747673A (en) * 2017-11-17 2018-03-02 广州中船文冲船坞有限公司 A kind of quick filling tailing axle is by the device of army cap lubricant grease

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Effective date of registration: 20200102

Address after: 511462 building 6, No. 2, No. 10, QIHANG Road, Nansha District, Guangzhou City, Guangdong Province (production management building and auxiliary building of electromechanical comprehensive workshop) (office only)

Patentee after: Guangzhou Wenchong Shipbuilding Co.,Ltd.

Address before: 511462 No. 10, sailing Road, Nansha District, Guangdong, China, No. 1, 4 (office building), written by myself, Guangzhou

Patentee before: CSSC GUANGZHOU WENCHONG DOCKYARD CO.,LTD.

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Granted publication date: 20180608

Effective date of abandoning: 20230124

AV01 Patent right actively abandoned
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