CN206941537U - A kind of check gate aileron structure - Google Patents

A kind of check gate aileron structure Download PDF

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Publication number
CN206941537U
CN206941537U CN201720917515.7U CN201720917515U CN206941537U CN 206941537 U CN206941537 U CN 206941537U CN 201720917515 U CN201720917515 U CN 201720917515U CN 206941537 U CN206941537 U CN 206941537U
Authority
CN
China
Prior art keywords
aileron
shoulder guard
check gate
structure according
upstream face
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.)
Expired - Fee Related
Application number
CN201720917515.7U
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Chinese (zh)
Inventor
薛亮
祁凯
葛万明
孟怡凯
秦景言
薛莲
江沆
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.)
Wuxi Water Conservancy Design Institute Co Ltd
Original Assignee
Wuxi Water Conservancy Design Institute 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
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Priority to CN201720917515.7U priority Critical patent/CN206941537U/en
Application granted granted Critical
Publication of CN206941537U publication Critical patent/CN206941537U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A30/00Adapting or protecting infrastructure or their operation
    • Y02A30/30Adapting or protecting infrastructure or their operation in transportation, e.g. on roads, waterways or railways

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  • Lining And Supports For Tunnels (AREA)

Abstract

It the utility model is related to check gate field, more particularly to a kind of check gate aileron structure, including aileron body, the aileron body includes upstream face and meets native face, the upstream face is outer covered with one layer of shoulder guard, fixing hole is provided with the upstream face, the expansion bolt of fixed protection steel plate is equipped with the fixing hole.By above-mentioned setting, shoulder guard is blocked before upstream face, prior to aileron body and the ship collision passed through; aileron body construction is protected; and shoulder guard directly contacts aileron body, and effect of impact power is undertaken together by aileron body caused by collision, avoids shoulder guard from deforming.When shoulder guard is damaged, expansion bolt can be unclamped, is changed, then expansion bolt is tightened and is continuing with, it is convenient to change, and saves labour, only need to change shoulder guard, cost is relatively low.

Description

A kind of check gate aileron structure
Technical field
Check gate field is the utility model is related to, more particularly to a kind of check gate aileron structure.
Background technology
Publication No. CN203603164U Chinese patent discloses a kind of steel guard timber aileron, belongs to hydraulic engineering technology neck Domain.It includes concrete aileron, and the concrete aileron front is provided with coated steel plate, and the coated steel plate front is along vertical side To more bar steel guard timbers are arranged with parallel, the coated steel plate back side is evenly arranged with a plurality of coated steel plate joint bar, the clad can steel Plate is fixedly connected by coated steel plate joint bar with concrete aileron, and the steel guard timber section is in circular arc, and the steel guard timber is with covering Concrete is filled between the steel plate of face.
Although this aileron has preferable barrier propterty, during long-time use, the clad can on aileron surface Steel plate and steel guard timber can still be damaged under the collision of ship, and coated steel plate is to be fixed on by joint bar on aileron, more Cast concrete is re-started after coated steel plate is changed, it is necessary to destroy the upstream face of wall to fix joint bar, it has not been convenient to safeguard.
Utility model content
The purpose of this utility model is to provide a kind of check gate aileron structure, and it, which has, maintains easily advantage.
Above-mentioned technical purpose of the present utility model technical scheme is that:
A kind of check gate aileron structure, including aileron body, the aileron body includes upstream face and meets native face, described to meet The water surface is outer covered with one layer of shoulder guard, is provided with fixing hole on the upstream face, fixed protection steel is equipped with the fixing hole The expansion bolt of plate.
By using above-mentioned technical proposal, shoulder guard is blocked before upstream face, prior to aileron body and the ship passed through Collision, is protected, and shoulder guard directly contacts aileron body, effect of impact caused by collision to aileron body construction Power is undertaken together by aileron body, avoids shoulder guard from deforming., can in installation process using expansion bolt fixed protection steel plate Carry out opening up fixing hole in upstream face with directly, being re-filled with high-pressure medium after expansion bolt insertion carries out expansion fastening installation side Just.When shoulder guard is damaged, expansion bolt can be unclamped, is changed, then expansion bolt is tightened and is continuing with, It is convenient to change, and saves labour, only need to change shoulder guard, cost is relatively low.Even if expansion bolt damages, one can also be changed Expansion bolt, and the perforate again on aileron body and shoulder guard, change position and be fixed.
Further set:The installation counterbore penetrated for expansion bolt, the installation counterbore are offered on the aileron body Place is provided with connection heavy cup, and the connection heavy cup includes cup and cup edge, and the cup installs counterbore through shoulder guard insertion Interior, the cup edge contradicts with shoulder guard.
By using above-mentioned technical proposal, expansion bolt is located at installation counterbore, be ensure that the smooth of surface of wall, is kept away Exempt from expansion bolt and protrude a gun body surface, ship by when be scratched, or even cause danger.Utilize the cup edge pressure for connecting heavy cup Tight steel plate, contact area is big, and active force is more scattered, more stable to the compression of steel plate;And it can allow to connect heavy cup circle The concentricity of the heart and the hole heart of the mounting hole on shoulder guard has larger error, easy for installation, prevents in the case of different temperatures Shield steel plate expands with heat and contract with cold and can still keep good fixation;And connect heavy cup and prevent external force to the direct of expansion bolt Collide, effectively prevent destruction of the shearing force to expansion bolt as caused by collision.
Further set:The expansion bolt includes the expansion tube and bolt head being welded to each other, and is opened up on the bolt head There is an oilhole for leading to expansion tube, what the expansion tube passed aileron body meets native face.
By using above-mentioned technical proposal, after collided gudgeon is inserted in aileron body through shoulder guard, pass through oil Hydraulic oil is injected in hole into expansion tube, and expansion tube expands in the presence of hydraulic oil, is firmly connected with aileron body.Expansion tube is stretched Go out aileron body one end because soil resistance is less than coagulation soil resistance, dilation dimension is larger, more than the diameter of fixing hole, to expansion The abjection of bolt produces stop, improves the bonding strength of expansion bolt.When needing to change, first to the hydraulic oil in expansion bolt Dismantled again after being discharged.
Further set:Fixing groove is offered on the upstream face of the aileron body, the lower end of the shoulder guard has The fixation edge of embedded fixing groove.
By using above-mentioned technical proposal, in traditional steel plate protection, tilting occurs along position is most normal to steel plate lower The damage mode seen, lower fixation avoid shoulder guard lower end from being turned up in collision process tilting, carried along embedded fixing groove The high service life of shoulder guard.
Further set:The shoulder guard positive and negative scribbles antirust paint.
By using above-mentioned technical proposal, shoulder guard often contacts with river, and easily corrosion, antirust paint enhance protection The antiseptic property of steel plate, avoid shoulder guard that corrosion of rotting occurs.
Further set:Spilled water hole is provided with the aileron body, the spilled water hole from soil is met lead to downwards by inclination Upstream face.
By using above-mentioned technical proposal, spilled water hole can release the water met and infiltrated outside native face inside soil naturally, The stability of soil is ensured, avoiding soil, immersion is collapsed for a long time by water, ensures the safety of aileron.
Further set:The aileron structure also includes the aileron base being wholely set with aileron body, the aileron bottom Some floors are connected between seat and aileron body.
By using above-mentioned technical proposal, the setting of connect base reduces the overall center of gravity of aileron structure so that aileron Structural stability is stronger, and the setting of floor enhances the stability of aileron body, avoids effect of the aileron body in hydraulic pressure Lower run-off the straight.
Further set:Reinforcing prop is connected between the adjacent floor.
By using above-mentioned technical proposal, being connected with each other between floor for reinforcing prop, local ribs stress is avoided The excessive situation for bending or wrecking, improve the stability of rib structure.
Further set:The lower section of the aileron base sets concrete bed course of being always or usually as specified.
By using above-mentioned technical proposal, plain concrete bed course is laid on ground in advance, is formed flat surface, is easy to above Assembling reinforcement, while ground can also be protected.
Further set:The aileron base stretches out the upstream face of aileron body towards river side.
By using above-mentioned technical proposal, aileron base stretches into river lower end, aileron base can be produced and pushed in river Active force so that the position of aileron base is stable, improves the stability of aileron structure.
In summary, the utility model has the advantages that:
1st, aileron body is protected by shoulder guard, avoids ship collision from causing to damage to aileron, shoulder guard It is fixed by countersunk head expansion bolt, impact surfaces are smooth, are connected firmly;
2nd, aileron base and aileron body are wholely set, and reduce the center of aileron so that aileron is in soil and hydraulic pressure Effect is lower to keep stable, improves the stability of aileron structure.
Brief description of the drawings
Fig. 1 is the structural representation of embodiment;
Fig. 2 is enlarged drawing at A in Fig. 1.
In figure, 1, aileron body;2nd, upstream face;3rd, native face is met;4th, shoulder guard;5th, expansion bolt;6th, heavy cup is connected;7、 Cup;8th, cup edge;9th, expansion tube;10th, bolt head;11st, oilhole;12nd, fixed edge;13rd, spilled water hole;14th, aileron base;15th, rib Plate;16th, reinforcing prop;17th, plain concrete bed course.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
Embodiment:
A kind of check gate aileron structure, reference picture 1, including horizontal aileron base 14 and the wing perpendicular to aileron base 14 Concrete bed course 17 of being always or usually as specified is laid in wall body 1, the lower section of aileron base 14.Aileron body 1 includes upstream face 2 and meets native face 3, aileron body 1 meet is connected with vertical floor 15 between native face 3 and aileron base 14, horizontal reinforcing prop 16 is connected between adjacent floor 15 Floor 15 is supported.
Referring to Figures 1 and 2, shoulder guard 4 is stamped in the upside of aileron body 1, and the positive and negative of shoulder guard 4 scribbles antirust Paint, the upper end of shoulder guard 4 is hooked on aileron body 1.Aileron body 1 offers fixing hole from upstream face 2 to native face 3 is met, Gu Determine hole and be provided with the installation counterbore coaxial with fixing hole towards the native side of face 3 is met, install at counterbore embedded with connection heavy cup 6.Connection is heavy Cup 6 includes cup 7 and cup edge 8, and after cup 7 passes through shoulder guard 4, cup edge 8 contradicts with shoulder guard 4.The bottom of cup 7 is worn There is expansion bolt 5, expansion bolt 5 is penetrated in fixing hole through after connecting heavy cup 6.Expansion bolt 5 divides for bolt head 10 and expansion Pipe 9, bolt head 10 are provided with the oilhole 11 for leading to expansion tube 9, and expansion tube 9 passes from fixing hole, in the soil of insertion outside.Aileron The position of the lower end of face shoulder guard 4 of body 1 is provided with fixing groove, and the lower end of shoulder guard 4 has consolidating for embedded fixing groove Determine along 12.
Reference picture 2, aileron body 1 are provided with spilled water hole 13 in the fixed lower section along 12, and spilled water hole 13 is downward from native face 3 is met Pass-out upstream face 2 is tilted, spilled water hole 13 is reserved pipe fitting when pouring aileron body 1 and is made.
When building aileron, first plain soil padding is laid and completed, aileron base 14 and aileron body are poured on plain soil padding 1, then floor 15 and reinforcing prop 16 are poured.The installation of shoulder guard 4 is carried out again, first by shoulder guard 4 from top hook Onto aileron body 1, counterbore is installed in the hole alignment that cup edge 8 passes through on connecting plate, is made fixed along consolidating on 12 insertion aileron bodies 1 Determine groove, connection heavy cup 6 is then embedded in installation counterbore, cup edge 8 contradicts with shoulder guard 4.Expansion bolt 5 is inserted into, is expanded Native face 3 is met in the stretching of pipe 9, and pad is provided between the lower end of bolt head 10 of expansion bolt 5 and connection heavy cup 6.By expansion bolt 5 The bottom of connection heavy cup 6 is pressed on, 150Mpa hydraulic oils are passed through into oilhole 11 so that expansion bolt 5 fixes aileron body 1 On.
Shoulder guard 4 be damaged need change when, unclamp expansion bolt 5, changed, then by expansion bolt 5 Tighten and be continuing with, it is convenient to change, and saves labour, only need to change shoulder guard 4, cost is relatively low.Even if expansion bolt 5 damages It is bad, an expansion bolt 5, and the perforate again on aileron body 1 and shoulder guard 4 can also be changed, position is changed and is consolidated It is fixed.
The above embodiments are only that it is not to limitation of the present utility model, ability to explanation of the present utility model Field technique personnel can make the modification of no creative contribution to the present embodiment as needed after this specification is read, but As long as all protected in right of the present utility model by Patent Law.

Claims (10)

1. a kind of check gate aileron structure, including aileron body (1), it is characterised in that:The aileron body (1) includes upstream face (2) and native face (3) is met, the upstream face (2) is provided with fixation outside covered with one layer of shoulder guard (4) on the upstream face (2) Hole, the expansion bolt (5) of fixed protection steel plate (4) is equipped with the fixing hole.
A kind of 2. check gate aileron structure according to claim 1, it is characterised in that:Opened up on the aileron body (1) There is the installation counterbore penetrated for expansion bolt (5), connection heavy cup (6), the connection heavy cup (6) are provided with the installation counterbore Including cup (7) and cup edge (8), the cup (7) is installed in counterbore through shoulder guard (4) is embedded, and the cup edge (8) is with preventing Steel plate (4) is protected to contradict.
A kind of 3. check gate aileron structure according to claim 1 or 2, it is characterised in that:The expansion bolt (5) includes The expansion tube (9) and bolt head (10) being welded to each other, the oilhole for leading to expansion tube (9) is offered on the bolt head (10) (11) what, the expansion tube (9) passed aileron body (1) meets native face (3).
A kind of 4. check gate aileron structure according to claim 1, it is characterised in that:Aileron body (1) meets water Fixing groove is offered on face (2), the lower end of the shoulder guard (4) has the fixed along (12) of embedded fixing groove.
A kind of 5. check gate aileron structure according to claim 1, it is characterised in that:Shoulder guard (4) positive and negative Scribble antirust paint.
A kind of 6. check gate aileron structure according to claim 1, it is characterised in that:Set on the aileron body (1) There is spilled water hole (13), the spilled water hole (13) is met native face (3) and tilted down certainly leads to upstream face (2).
A kind of 7. check gate aileron structure according to claim 1, it is characterised in that:The aileron structure also includes and the wing The aileron base (14) that wall body (1) is wholely set, some ribs are connected between the aileron base (14) and aileron body (1) Plate (15).
A kind of 8. check gate aileron structure according to claim 7, it is characterised in that:Connect between the adjacent floor (15) It is connected to reinforcing prop (16).
A kind of 9. check gate aileron structure according to claim 7, it is characterised in that:The lower section of the aileron base (14) Setting is always or usually as specified concrete bed course (17).
A kind of 10. check gate aileron structure according to claim 7, it is characterised in that:Aileron base (14) direction The upstream face (2) of aileron body (1) is stretched out in river side.
CN201720917515.7U 2017-07-26 2017-07-26 A kind of check gate aileron structure Expired - Fee Related CN206941537U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720917515.7U CN206941537U (en) 2017-07-26 2017-07-26 A kind of check gate aileron structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720917515.7U CN206941537U (en) 2017-07-26 2017-07-26 A kind of check gate aileron structure

Publications (1)

Publication Number Publication Date
CN206941537U true CN206941537U (en) 2018-01-30

Family

ID=61370242

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720917515.7U Expired - Fee Related CN206941537U (en) 2017-07-26 2017-07-26 A kind of check gate aileron structure

Country Status (1)

Country Link
CN (1) CN206941537U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108442352A (en) * 2018-04-23 2018-08-24 南通航运职业技术学院 A kind of Retaining Wall of Shiplock protective device and its method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108442352A (en) * 2018-04-23 2018-08-24 南通航运职业技术学院 A kind of Retaining Wall of Shiplock protective device and its method
CN108442352B (en) * 2018-04-23 2023-05-26 南通航运职业技术学院 Ship lock wall protection device and method thereof

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180130

Termination date: 20190726