CN203334282U - Whole loading and transporting type hydraulic static pile driver - Google Patents
Whole loading and transporting type hydraulic static pile driver Download PDFInfo
- Publication number
- CN203334282U CN203334282U CN2013204249936U CN201320424993U CN203334282U CN 203334282 U CN203334282 U CN 203334282U CN 2013204249936 U CN2013204249936 U CN 2013204249936U CN 201320424993 U CN201320424993 U CN 201320424993U CN 203334282 U CN203334282 U CN 203334282U
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- supporting leg
- fuselage
- free bearing
- oil cylinder
- hydraulic static
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Abstract
The utility model relates to a whole loading and transporting type hydraulic static pile driver which comprises a driver body, a short ship mechanism, a long ship mechanism, a corner pile mechanism and a crane mechanism with a crane. The driver body is provided with a driver body main body, the driver body main body is provided with a driver body supporting leg hinged support, and the driver body supporting leg hinged support is provided with a driver body supporting leg with a supporting leg telescopic oil cylinder. The whole loading and transporting type hydraulic static pile driver is characterized in that the driver body supporting leg can slide inside the driver body supporting leg hinged support under the effect of the supporting leg telescopic oil cylinder. Therefore, the long ship mechanism, the short ship mechanism, the driver body supporting leg and the like are not required to be disassembled in the whole transition loading and transporting process of the pile driver, the whole loading and transporting can be achieved, the crane is not required to be additionally arranged, the cost for assembling and disassembling the crane is reduced, the labor amount for assembling and disassembling the crane is reduced, the whole loading and transporting type hydraulic static pile driver is particularly suitable for small construction sites and construction sites where the crane cannot reach, the applicability of the pile driver is improved, and the pile driver is simple in structure and easy and convenient to manufacture, assemble, disassemble and maintain.
Description
Technical field
The utility model relates to a kind of hydraulic static pile pressing machine, espespecially a kind of hydraulic static pile pressing machine that can whole shipment.
Background technology
The static pressure construction of preformed pile is to utilize static pressure preformed pile to be pressed into reposefully to a kind of novel environment friendly pile foundation construction method of ground.To the eighties, along with the development of piling machinery and the enhancing of environmental consciousness progressively are promoted.The silent piling construction method generally adopts in pile foundation construction at home at present, and, except preformed pile is used silent piling, H Section-steel Piles and other special-shaped piling bar have also generally adopted the silent piling construction method.Hydraulic static construction, place is clean, noiselessness, shockproof, without sewage, smoke dust, operation in the suitable urban district environment being had to specific (special) requirements; Piling speed is fast, efficiency is high, and hydraulic static pile pressing machine is the ideal equipment of static pressure construction, and the scope of application is more and more wider.
During hydraulic static pile pressing machine transition at present, after all needing the complete machine dismounting is disintegrated, transported, dismounting is cumbersome, the especially long ship of dismounting mechanism, short ship mechanism, supporting leg etc., and workload is large, labour intensity is high, need please the loop wheel machine cooperation just can complete the machine of tearing open and installation in addition, in addition in narrower and small building site, loop wheel machine also is difficult to arrive, some area or country ask the expense of loop wheel machine very expensive, increase construction cost.
Summary of the invention
Technical problem to be solved in the utility model is: for the cumbersome deficiency of hydraulic static pile pressing machine transition dismounting in above-mentioned prior art, and provide a kind of whole shipment formula hydraulic static pile pressing machine.
In order to solve the problems of the technologies described above, the technical scheme that the utility model adopts is: a kind of whole shipment formula hydraulic static pile pressing machine, the loop wheel machine mechanism that it comprises fuselage, short ship mechanism, long ship mechanism, corner stake mechanism and is provided with loop wheel machine, this fuselage has the fuselage main body, this fuselage main body is provided with fuselage supporting leg free bearing, this fuselage supporting leg free bearing is provided with the fuselage supporting leg of tool support oil cylinder, is characterized in, described fuselage supporting leg can slide in this fuselage supporting leg free bearing.
Described fuselage supporting leg free bearing is located at the two ends of this fuselage main body, the centre of this fuselage supporting leg free bearing is provided with dividing plate, this dividing plate bilateral symmetry is fixed with the oil cylinder that the landing leg stretching oil cylinder is installed free bearing is installed, these fuselage supporting leg free bearing both sides have respectively the first accommodation space, and this fuselage supporting leg major part is placed in this first accommodation space.
Described fuselage supporting leg has the second accommodation space, be provided with the free bearing fixed head in this second accommodation space, be fixed with oil cylinder supporting leg on this free bearing fixed head free bearing is installed, it is hinged that one end of this landing leg stretching oil cylinder and this oil cylinder are installed free bearing, and the other end enters in the second accommodation space hinged with this oil cylinder supporting leg installation free bearing through the fuselage supporting leg.
The framework of described fuselage supporting leg is respectively equipped with first and second dowel hole in front and back end, and on the supporting plate up and down of this fuselage supporting leg free bearing, correspondence is provided with the 3rd dowel hole, the misalignment of this first, second and third dowel hole and fuselage supporting leg free bearing, when pile press work or transportation, insert in the 3rd dowel hole and the second dowel hole or, in the 3rd dowel hole and the first dowel hole, this fuselage supporting leg and this fuselage supporting leg free bearing fixed by alignment pin.
Described fuselage supporting leg free bearing two ends are provided with anchor ear.The framework of described fuselage supporting leg is provided with the antifriction plate on four sides.
Described corner stake mechanism has corner stake section, and this corner stake section and this fuselage main body are wholely set, and Zhuan Bu end, this corner is provided with the U-shaped opening.
Described long ship mechanism and short ship mechanism are narrow flat shape.The long outboard side of described long ship mechanism is provided with chamfering.
Compared with prior art, the beneficial effects of the utility model are: the whole transition transportation of this integral body shipment formula hydraulic static pile pressing machine does not need to tear open long ship mechanism, short ship mechanism and fuselage supporting leg etc., can realize whole Transporting; Do not need separately to ask loop wheel machine, reduce the cost of tearing the machine installation open, reduced the amount of labour of tearing the machine installation open, be particularly useful for little building site, the building site that loop wheel machine can not arrive, improve the pile press applicability; This pile press is simple in structure, production, installation and removal, convenience easy to maintenance.
Below in conjunction with drawings and Examples, the utility model is described in further detail.
The accompanying drawing explanation
Fig. 1 is complete machine structure schematic diagram of the present utility model.
Fig. 2 is the airframe structure schematic diagram.
Fig. 3 is the schematic diagram of fuselage supporting leg.
Fig. 4 is the scheme of installation of landing leg stretching oil cylinder.
Fig. 5 is the structural representation of long ship mechanism.
Fig. 6 is the structural representation of short ship mechanism.
Fig. 7 is pile press travel position schematic diagram.
The specific embodiment
As shown in Figures 1 and 2, the utility model is a kind of whole shipment formula hydraulic static pile pressing machine, and it comprises fuselage 1, short ship mechanism 2, long ship mechanism 3, cross beam and upright post 4, pile clamping box 5, corner stake mechanism 6, loop wheel machine mechanism 7, hydraulic system 8, electrical system 9 etc.This fuselage 1 is body structure, there is fuselage main body 11, this fuselage main body 11 is provided with fuselage supporting leg free bearing 12, this fuselage supporting leg free bearing 12 is provided with fuselage supporting leg 13, the support oil cylinder 131 that this fuselage supporting leg 13 arranges adopts inverted structures, and the bulb 1311 of support oil cylinder 131 is supported on the walking dolly 31 of long ship mechanism 3; The loop wheel machine seat 71 that one side of this fuselage main body 11 is loop wheel machine mechanism 7, be equipped with loop wheel machine 72 on this loop wheel machine seat 71, the corner stake section 61 that opposite side is corner stake mechanism 6, and this corner stake section 61 is wholely set with this fuselage main body 11, forms whole corner pilework; Be respectively equipped with the column free bearing 10 that cross beam and upright post 4 is installed in this fuselage main body 11 and corner stake section 61; This fuselage 1 flexibly connects by central axis and short ship mechanism 2.This short ship mechanism 2 realizes laterally stake machine walking and turns to, and long ship mechanism 3 realizes that a machine vertically walks.Those structures are all prior art, and this is no longer going to repeat them, now with regard to improvements of the present utility model, are described as follows:
Continuation is referring to Fig. 2, the two ends of this fuselage main body 11 are welded with this fuselage supporting leg free bearing 12, the centre of this fuselage supporting leg free bearing 12 is welded with dividing plate 14, these dividing plate 14 bilateral symmetry are welded with the oil cylinder that landing leg stretching oil cylinder 15 is installed free bearing 16 are installed, these fuselage supporting leg free bearing 12 both sides have respectively the first accommodation space 17, and these fuselage supporting leg 13 major parts are placed in this first accommodation space 17; These fuselage supporting leg free bearing 12 two ends are designed with anchor ear 18, to increase the rigidity of fuselage supporting leg free bearing 12 ends.
In a preferred embodiment, the end of the corner stake section 61 of this corner stake mechanism 6 is designed with U-shaped opening 62, can reduce the corner pilespacing from.
Referring to Fig. 3 and Fig. 4, the framework of this fuselage supporting leg 13 is welded with antifriction plate 132 on four sides, this fuselage supporting leg 13 has the second accommodation space 133, this support oil cylinder 131 is arranged at the end of this fuselage supporting leg 13, be provided with free bearing fixed head 134 in this second accommodation space 133, be welded with oil cylinder supporting leg on this free bearing fixed head 134 free bearing 135 is installed, it is hinged that one end of this landing leg stretching oil cylinder 15 and this oil cylinder are installed free bearing 16, the other end enters in the second accommodation space 133 hinged with this oil cylinder supporting leg installation free bearing 135 through fuselage supporting leg 13, under the effect of landing leg stretching oil cylinder 15, this fuselage supporting leg 13 is in the 12 interior slips of fuselage supporting leg free bearing.The framework of this fuselage supporting leg 13 is respectively equipped with first and second dowel hole 136,137 in front and back end, and on the supporting plate 121 of this fuselage supporting leg free bearing 12, correspondence is provided with the 3rd dowel hole 122, the misalignment of this first, second and third dowel hole 136,137,122 and fuselage supporting leg free bearing 12, so that the installation of landing leg stretching oil cylinder 15; During pile press work, after this fuselage supporting leg 13 stretches out by landing leg stretching oil cylinder 15, insert the 3rd dowel hole 122 and the second dowel hole 137 with alignment pin 19, can pin fuselage supporting leg 13, make landing leg stretching oil cylinder 15 can not bear the power that fuselage supporting leg 13 transmits, and make fuselage supporting leg 13 be connected safety, reliable with fuselage supporting leg free bearing 12; During transhipment, after fuselage supporting leg 13 is retracted, by alignment pin 19, insert the 3rd dowel hole 122 and the first dowel hole 136, to pin fuselage supporting leg 13, install reliable while making to transport.
Referring to Fig. 5 and Fig. 6, this long ship mechanism 3 and short ship mechanism 2 are designed to narrow flat shape, and the height while making complete machine work reduces, and the height of whole Transporting reduces and width reduces, and facilitates whole Transporting.For reduce the angle pilespacing from, the chamfering 32 that the long outboard side of two long ship mechanisms is designed with large chamfering 32, two long ships is symmetrical set.
As shown in Figure 7, during the pile press transhipment, only need be by counterweight, counterweight beam and pile pressing beam hang away with loop wheel machine 72, by support oil cylinder 131 jackings, fuselage 1 and short ship mechanism 2 are by jack-up, when short ship mechanism 2 base plates during higher than haulage vehicle, haulage vehicle is steadily poured into, then support oil cylinder 131 is retracted, short ship mechanism 2 and fuselage 1 are fallen on haulage vehicle reposefully, continue retraction support oil cylinder 131, long ship mechanism 3 is raised, after the flat board 20 of long ship lower shoe higher than haulage vehicle, the piston rod of landing leg stretching oil cylinder 15 is retracted, fuselage supporting leg 13 and long ship mechanism 3 retract to fuselage 1, fuselage supporting leg 13 use alignment pin 19 are plugged to pinning, then support oil cylinder 131 is stretched out, long ship is placed on the flat board 20 of haulage vehicle, installation process process therewith is contrary, whole transition transportation does not need to tear open long ship mechanism 3, the structures such as short ship mechanism 2 and fuselage supporting leg 13, can realize whole Transporting, do not need separately to ask loop wheel machine, reduce the cost of tearing the machine installation open, reduced the amount of labour of tearing the machine installation open, be particularly useful for little building site, the building site that loop wheel machine can not arrive, improve the pile press applicability, this pile press is simple in structure, make, install, dismounting, convenience easy to maintenance.
Claims (9)
1. a whole shipment formula hydraulic static pile pressing machine, the loop wheel machine mechanism (7) that it comprises fuselage (1), short ship mechanism (2), long ship mechanism (3), corner stake mechanism (6) and is provided with loop wheel machine (72), this fuselage (1) has fuselage main body (11), this fuselage main body (11) is provided with fuselage supporting leg free bearing (12), this fuselage supporting leg free bearing (12) is provided with the fuselage supporting leg (13) of tool support oil cylinder (131), it is characterized in that, described fuselage supporting leg (13) can slide in this fuselage supporting leg free bearing (12).
2. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, it is characterized in that, described fuselage supporting leg free bearing (12) is located at the two ends of this fuselage main body (11), the centre of this fuselage supporting leg free bearing (12) is provided with dividing plate (14), this dividing plate (14) bilateral symmetry is fixed with the oil cylinder that landing leg stretching oil cylinder (15) is installed free bearing (16) is installed, these fuselage supporting leg free bearing (12) both sides have respectively the first accommodation space (17), and this fuselage supporting leg (13) major part is placed in this first accommodation space (17).
3. whole shipment formula hydraulic static pile pressing machine as claimed in claim 2, it is characterized in that, described fuselage supporting leg (13) has the second accommodation space (133), be provided with free bearing fixed head (134) in this second accommodation space (133), be fixed with oil cylinder supporting leg on this free bearing fixed head (134) free bearing (135) is installed, it is hinged that one end of this landing leg stretching oil cylinder (15) and this oil cylinder are installed free bearing (16), and the other end enters in the second accommodation space (133) hinged with this oil cylinder supporting leg installation free bearing (135) through fuselage supporting leg (13).
4. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, it is characterized in that, the framework of described fuselage supporting leg (13) is respectively equipped with first in front and back end, two dowel holes (136, 137), and the upper correspondence of the supporting plate (121) of this fuselage supporting leg free bearing (12) is provided with the 3rd dowel hole (122), this is first years old, two, three dowel holes (136, 137, 122) with the misalignment of fuselage supporting leg free bearing (12), when pile press work or transportation, by alignment pin (19), insert in the 3rd dowel hole (122) and the second dowel hole (137) or in the 3rd dowel hole (122) and the first dowel hole (136), make this fuselage supporting leg (13) and this fuselage supporting leg free bearing (12) fixing.
5. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, is characterized in that, described fuselage supporting leg free bearing (12) two ends are provided with anchor ear (18).
6. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, is characterized in that, the framework of described fuselage supporting leg (13) is provided with antifriction plate (132) on four sides.
7. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, it is characterized in that, described corner stake mechanism (6) has corner stake section (61), and this corner stake section (61) is wholely set with this fuselage main body (11), and the end of this corner stake section (61) is provided with U-shaped opening (62).
8. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, is characterized in that, described long ship mechanism (3) and short ship mechanism (2) are narrow flat shape.
9. whole shipment formula hydraulic static pile pressing machine as claimed in claim 1, is characterized in that, the long outboard side of described long ship mechanism (3) is provided with chamfering (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013204249936U CN203334282U (en) | 2013-07-17 | 2013-07-17 | Whole loading and transporting type hydraulic static pile driver |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013204249936U CN203334282U (en) | 2013-07-17 | 2013-07-17 | Whole loading and transporting type hydraulic static pile driver |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203334282U true CN203334282U (en) | 2013-12-11 |
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ID=49702963
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013204249936U Expired - Lifetime CN203334282U (en) | 2013-07-17 | 2013-07-17 | Whole loading and transporting type hydraulic static pile driver |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203334282U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104005412A (en) * | 2014-06-13 | 2014-08-27 | 湖南新天和工程设备有限公司 | Hydraulic static pile driver suitable for narrow construction site |
| CN108411750A (en) * | 2018-05-15 | 2018-08-17 | 河南省高远公路养护技术有限公司 | A kind of quick change locking device of road maintenance engineering vehicle and function module |
| CN114319357A (en) * | 2022-01-06 | 2022-04-12 | 上海中联重科桩工机械有限公司 | Static pile press |
-
2013
- 2013-07-17 CN CN2013204249936U patent/CN203334282U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104005412A (en) * | 2014-06-13 | 2014-08-27 | 湖南新天和工程设备有限公司 | Hydraulic static pile driver suitable for narrow construction site |
| CN108411750A (en) * | 2018-05-15 | 2018-08-17 | 河南省高远公路养护技术有限公司 | A kind of quick change locking device of road maintenance engineering vehicle and function module |
| CN108411750B (en) * | 2018-05-15 | 2023-09-08 | 河南省高远公路养护技术有限公司 | Quick-change locking device for highway maintenance engineering truck and functional module |
| CN114319357A (en) * | 2022-01-06 | 2022-04-12 | 上海中联重科桩工机械有限公司 | Static pile press |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20131211 |
|
| CX01 | Expiry of patent term |