CN207775861U - A kind of device of foundation - Google Patents

A kind of device of foundation Download PDF

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Publication number
CN207775861U
CN207775861U CN201721862838.7U CN201721862838U CN207775861U CN 207775861 U CN207775861 U CN 207775861U CN 201721862838 U CN201721862838 U CN 201721862838U CN 207775861 U CN207775861 U CN 207775861U
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CN
China
Prior art keywords
fuselage
rack
fixed
gear
long nut
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
CN201721862838.7U
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Chinese (zh)
Inventor
李明
袁建伟
蔡俊勇
郭腾翔
何晓悦
王美英
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Individual
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Individual
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Publication date
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Priority to CN201721862838.7U priority Critical patent/CN207775861U/en
Application granted granted Critical
Publication of CN207775861U publication Critical patent/CN207775861U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)

Abstract

A kind of device of foundation, the effective solution prior art cannot carry out smooth processing before being tamped to soil layer to soil layer, so that the soil layer intensity after compacting can be reduced, the problems such as low construction efficiency;Including tamping machine fuselage, front fuselage is internally provided with two rotating mechanisms, and rotating mechanism includes the long nut being mounted on fuselage, and long nut right end is connected with screw rod, screw rod right end is fixed with the T-type sliding block that can be slided in T-type slideway, T-type sliding block side is fixed with rack, is engaged with gear above rack, push plate is fixed on gear shaft, it is connected with driving wheel and driven wheel below fuselage, driving wheel and driven wheel outer surface are engaged with crawler belt, and motor is equipped in fuselage, hammer ram structure is connected on rear side of fuselage;By the way of threaded connection and rack and pinion engagement, before crawler belt over the ground face pressure reality, ground is first subjected to smooth and removal obstacle, compaction quality is ensure that and improves work efficiency, this is simple in structure, easy to operate, and securely and reliably, service efficiency is high.

Description

A kind of device of foundation
Technical field
The utility model is related to technical field of building construction, more particularly to a kind of device of foundation.
Background technology
Ground refers to the soil body or rock mass of supporting base below building, and the soil layer as building lot is divided into rock, broken Stone soil, sand, silt, cohesive soil and artificial earth fill, ground have two class of subsoil and artificial foundation, and subsoil is not need The natural soil layer that people reinforces, artificial foundation need people's consolidation process.
During artificial foundation is handled, need that soil layer and concrete layer compacting will be reinforced, in the prior art, generally All it is to drive hammer ram to tamp ground using tamping machine, or to soil layer or coagulation in such a way that crawler type rolls compacting Soil layer carries out forced ramming reinforcing, since soil layer or concrete layer upper surface are uneven, during hammer ram or crawler belt roll, no Compacting speed is reduced by only, and is needed again to the smooth processing of soil layer upper surface progress, so unavoidably after the completion of compacting processing The secured intensity of soil layer after tamping can be weakened, reduce construction efficiency.
Utility model content
For the above situation, to overcome the defect of the prior art, the purpose of the utility model to be just to provide a kind of reinforcing ground The device on base basis, the effective solution prior art cannot carry out smooth processing before being tamped to soil layer to soil layer, so that meeting The soil layer intensity after compacting is reduced, and the problems such as low construction efficiency.
Its technical solution solved is that the utility model includes tamping machine fuselage, and front fuselage inside front-rear direction is equipped with Two rotating mechanisms, rotating mechanism include the long nut being rotatably installed on fuselage, and long nut right end, which is threaded with, stretches into length The screw rod of nut interior, screw rod right end are fixed with the T-type sliding block that can be horizontally slipped in T-type slideway, and T-type sliding block side is fixed with Rack, rack top are engaged with the gear being rotatably connected on fuselage, are fixed with push plate on gear shaft, constitute the rotation of long nut The structure for driving push plate to rotate upwardly and downwardly, fuselage rotated down are connected with driving wheel and driven wheel, driving wheel and driven wheel outer surface It is engaged with crawler belt, motor is equipped in fuselage, hammer ram structure is connected on rear side of fuselage.
Compared with prior art, the utility model has the beneficial effects that:Using the side being threadedly coupled with rack and pinion engagement Ground is first carried out smooth and removal obstacle by formula before crawler belt over the ground face pressure reality, be ensure that compaction quality and is improved work effect Rate, this is simple in structure, easy to operate, and securely and reliably, service efficiency is high.
Description of the drawings
Fig. 1 is the local cutting front view of the utility model.
Fig. 2 is the enlarged drawing of A in the utility model Fig. 1.
Specific implementation mode
Specific embodiment of the present utility model is described in further detail below in conjunction with attached drawing.
It is provided by Fig. 1 to Fig. 2, the utility model includes tamping machine fuselage 1, and 1 front end of fuselage inside front-rear direction is equipped with two A rotating mechanism, rotating mechanism include the long nut 2 of rotational installation on the fuselage 1, and 2 right end of long nut, which is threaded with, stretches into length Screw rod 3 inside nut 2,3 right end of screw rod are fixed with the T-type sliding block 5 that can be horizontally slipped in T-type slideway 4,5 side of T-type sliding block It is fixed with rack 6,6 top of rack is engaged with the gear 7 of rotation connection on the fuselage 1, is fixed with push plate 8 on 7 axis of gear, constitutes The rotation of long nut 2 drives the structure that push plate 8 rotates upwardly and downwardly, 1 rotated down of fuselage to be connected with driving wheel 9 and driven wheel 10, main Driving wheel 9 and 10 outer surface of driven wheel are engaged with crawler belt 11, and motor 12 is equipped in fuselage 1, and 1 rear side of fuselage is connected with hammer ram structure.
2 left end of long nut is equipped with the handwheel 13 in driver's cabin 23.
1 front end of fuselage connects push plate 8 through torsional spring 14, and baffle 15 is fixed on the downside of 1 front end of fuselage.
6 both sides of rack and be respectively connected with support plate 16 positioned at the bottom of T-type sliding block 5,16 upper surface of support plate with The lower surface of rack 6 is concordant.
The gear 7 is a quarter gear 7, and the both sides of the gear teeth are plane 17, and plane 17 can be slided in support plate 16 It is dynamic.
The hammer ram structure includes babinet 18, and babinet 18 connects fuselage 1 through fixed frame 19, and bottom is equipped with hammer in babinet 18 Body 20,20 top of hammer body are equipped with multiple sensors 21, and 18 leading flank of babinet is equipped with controller 22, the minimum height in 18 lower surface of babinet Degree is higher than 11 lower surface 10cm-20cm of crawler belt.
When the utility model is used,
Driving wheel 9 and driven wheel 10 are connected in 1 rotated down of fuselage, crawler belt 11 is installed on driving wheel 9 and driven wheel 10, Make the rotation of driving wheel 9 that crawler belt 11 be driven to be rotated around driving wheel 9 and driven wheel 10, long spiral shell is rotatablely installed in 1 front interior of fuselage Mother 2,2 left end of long nut are positioned at the handwheel 13 in driver's cabin 23,2 right end of long nut and stretch into the screw rod 3 inside long nut 2 Connection, 3 right side of screw rod are fixed with T-type sliding block 5, and T-type sliding block 5 can horizontally slip in fixed T-type slideway 4 on the fuselage 1, T 5 side of type sliding block is fixed with the rack 6 in horizontal direction, and 6 both sides of rack are equipped with support plate 16,16 upper surface of support plate and rack 6 lower surface is concordant, and 6 top of rack is engageable a quarter gear 7 of rotation connection on the fuselage 1, a quarter gear 7 With under the engagement of rack 6, drive the push plate 8 being fixed on 7 axis of gear that can rotate 90 degree;Babinet 18 is connected through fixed frame 19 At 1 rear of fuselage, 18 lower surface minimum altitude of babinet is higher than 11 lower surface 10cm-20cm of crawler belt, and bottom is equipped with hammer in babinet 18 Body 20,20 top of hammer body are equipped with multiple sensors 21, and 18 leading flank of babinet is equipped with controller 22.
Motor 12 starts, and tamping machine is driven to the foundation region for needing to tamp, and rotates handwheel 13, and long nut 2 drives screw rod 3 It being moved to the left, while T-type sliding block 5 is moved to the left in T-type slideway 4 together with rack 6, this hour rack 6 is engaged with gear 7, Rack 6 is rotated clockwise with moving gear 7, and when the tooth of 6 rightmost side of rack is engaged with gear 7 to close to an end, plane 17 is supporting It is slided on plate 16, push plate 8 rotates clockwise 90 degree, due to the blocking of baffle 15 and the self-locking performance of screw thread so that push plate 8 is in perpendicular Straight position;When tamping machine moves forward, 8 front end of push plate pushes rugged ground to achieve the purpose that ground grading, simultaneously The obstacle on ground can also be removed, crawler belt 11 rolls ground, reinforcing compacting is carried out to ground, in controller 22 and sensor 21 Cooperation under, hammer ram tamps ground;After entire foundation region is compacted, handwheel 13 is rotated, long nut 2 drives screw rod 3 move right, while T-type sliding block 5 moves right in T-type slideway 4 together with rack 6, this hour rack 6 is engaged with gear 7, Rack 6 is rotated counterclockwise with moving gear 7, and when the tooth of 6 leftmost side of rack is engaged with gear 7 to close to an end, plane 17 is supporting It is slided on plate 16, push plate 8 rotates counterclockwise 90 degree, due to the pulling force of torsional spring 14 and the self-locking performance of screw thread so that push plate 8 is in water Prosposition is set and will not fall, and tamping machine can be driven out to foundation region, and entire Ramming operation is completed.
18 lower surface minimum altitude of babinet is higher than 11 lower surface 10cm-20cm of crawler belt, it is ensured that tamping machine on the way when driving, case Body 18 scrape along the ground or will not touch barrier.
Compared with prior art, the utility model has the beneficial effects that:Using the side being threadedly coupled with rack and pinion engagement Ground is first carried out smooth and removal obstacle by formula before crawler belt over the ground face pressure reality, be ensure that compaction quality and is improved work effect Rate, this is simple in structure, easy to operate, and securely and reliably, service efficiency is high.

Claims (6)

1. a kind of device of foundation, including tamping machine fuselage(1), which is characterized in that fuselage(1)Front and back inside front end It is set upwards there are two rotating mechanism, rotating mechanism includes being rotatably installed in fuselage(1)On long nut(2), long nut(2)Right end It is threaded with and stretches into long nut(2)Internal screw rod(3), screw rod(3)Right end is fixed with can be in T-type slideway(4)It slides interior left and right Dynamic T-type sliding block(5), T-type sliding block(5)Side is fixed with rack(6), rack(6)Top, which is engaged with, is rotatably connected on fuselage(1) On gear(7), gear(7)Push plate is fixed on axis(8), constitute long nut(2)Rotation drive push plate(8)It rotates upwardly and downwardly Structure, fuselage(1)Rotated down is connected with driving wheel(9)And driven wheel(10), driving wheel(9)And driven wheel(10)It nibbles outer surface Conjunction has crawler belt(11), fuselage(1)It is interior to be equipped with motor(12), fuselage(1)Rear side is connected with hammer ram structure.
2. a kind of device of foundation according to claim 1, which is characterized in that the long nut(2)It is left End is equipped with positioned at driver's cabin(23)Interior handwheel(13).
3. a kind of device of foundation according to claim 1, which is characterized in that the fuselage(1)Front end Through torsional spring(14)Connect push plate(8), fuselage(1)It is fixed with baffle on the downside of front end(15).
4. a kind of device of foundation according to claim 1, which is characterized in that the rack(6)Both sides And it is located at T-type sliding block(5)Bottom be respectively connected with support plate(16), support plate(16)Upper surface and rack(6)Lower surface it is flat Together.
5. a kind of device of foundation according to claim 1, which is characterized in that the gear(7)It is four / mono- gear(7), the both sides of the gear teeth are plane(17), plane(17)It can be in support plate(16)Upper sliding.
6. a kind of device of foundation according to claim 1, which is characterized in that the hammer ram structure includes Babinet(18), babinet(18)Through fixed frame(19)Connect fuselage(1), babinet(18)Interior bottom is equipped with hammer body(20), hammer body(20) Top is equipped with multiple sensors(21), babinet(18)Leading flank is equipped with controller(22), babinet(18)Lower surface minimum altitude Higher than crawler belt(11)Lower surface 10cm-20cm.
CN201721862838.7U 2017-12-27 2017-12-27 A kind of device of foundation Expired - Fee Related CN207775861U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721862838.7U CN207775861U (en) 2017-12-27 2017-12-27 A kind of device of foundation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721862838.7U CN207775861U (en) 2017-12-27 2017-12-27 A kind of device of foundation

Publications (1)

Publication Number Publication Date
CN207775861U true CN207775861U (en) 2018-08-28

Family

ID=63225289

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721862838.7U Expired - Fee Related CN207775861U (en) 2017-12-27 2017-12-27 A kind of device of foundation

Country Status (1)

Country Link
CN (1) CN207775861U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113174923A (en) * 2021-04-01 2021-07-27 机械工业第九设计研究院有限公司 Foundation tamping device for civil engineering construction and use method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113174923A (en) * 2021-04-01 2021-07-27 机械工业第九设计研究院有限公司 Foundation tamping device for civil engineering construction and use method thereof
CN113174923B (en) * 2021-04-01 2023-03-14 机械工业第九设计研究院股份有限公司 Foundation tamping device for civil engineering construction and use 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: 20180828

Termination date: 20201227