A multifunctional spiral drilling pile testing machine

Through a multi-functional auger drilling pile measuring machine that integrates the fuselage platform and pile testing columns, the problem of high inspection costs in the existing technology is solved, and the sharing of drilling and pile pressing inspection is realized, reducing equipment costs.

CN113047284BActive Publication Date: 2025-09-02CHANGSHA TIANWEI ENG MASCH MANUFACUTURE CO LTD
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Patent Information

Application Number
CN202110449634.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2021-04-25
Publication Date
2025-09-02
Estimated Expiration
2041-04-25

AI Technical Summary

Technical Problem

The existing auger piles need to be equipped with special equipment for inspection after pile pressing, resulting in high inspection costs and inability to share with existing equipment.

Method used

A multi-functional auger drill pile measuring machine is designed, integrating the fuselage platform, walking mechanism, auger drilling mechanism and pile measuring column. After disassembling the auger drilling mechanism, the pile measuring column is pressed on the engineering pile, and the counterweight is gradually increased to detect the maximum bearing capacity, achieving multi-purpose one machine.

Benefits of technology

The sharing of drilling and pile pressing inspection is achieved, the inspection cost is reduced, and the utilization efficiency and economicality of the equipment are improved.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention discloses a multifunctional spiral drilling pile measuring machine, comprising a body platform, a traveling mechanism, a spiral drilling mechanism, and a counterweight. The traveling mechanism is mounted on the lower side of the body platform, and the counterweight is stacked on the upper side of the body platform. The spiral drilling mechanism is detachably mounted on the body platform, and a pile measuring column for pressing onto a prefabricated pile is mounted on the lower side of the body platform. The body platform of the present invention can accommodate the installation of the spiral drilling mechanism and the counterweight. When the spiral drilling mechanism is mounted on the body platform, pile holes can be drilled. After the engineering pile is pressed, the spiral drilling mechanism can be disassembled, the body platform is moved to the position of the engineering pile, the pile measuring column is pressed onto the engineering pile, and the counterweight is gradually added to the body platform. The maximum bearing capacity of the engineering pile can be measured to achieve the purpose of measurement. The main structures such as the body platform and the traveling mechanism can be shared, thereby achieving multiple uses of one machine, greatly saving costs.
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Description

Technical Field

[0001] The present invention relates to the technical field of engineering machinery, in particular to a multifunctional spiral drilling pile testing machine. Background Art

[0002] At present, most existing spiral pile drilling machines usually only have the function of drilling pile holes, and some spiral pile drilling machines are integrated with pile driving devices, which can realize drilling and pile driving in one.

[0003] However, after driving the pile, it's often necessary to test the maximum bearing capacity of the pile. Currently, this is typically done by applying pressure to the pile. This involves removing the driving device after driving, then applying a certain amount of pressure to the pile to determine whether the pile moves within a certain timeframe under the set maximum bearing capacity. This method requires specialized testing equipment, has a limited function, and cannot be used with existing auger pile drivers. Furthermore, the testing costs are relatively high. Summary of the Invention

[0004] The technical problem to be solved by the present invention is to overcome the deficiencies in the prior art and provide a multifunctional spiral drilling pile testing machine.

[0005] In order to solve the above technical problems, the technical solution proposed by the present invention is:

[0006] A multifunctional auger pile testing machine comprises a body platform, a traveling mechanism, an auger drilling mechanism and a counterweight. The traveling mechanism is mounted on the lower side of the body platform, the counterweight is stacked on the upper side of the body platform, the auger drilling mechanism is detachably mounted on the body platform, and a pile testing column for pressing on an engineering pile is mounted on the lower side of the body platform.

[0007] Furthermore, a fuselage plane for stacking the counterweight is provided on the upper side of the fuselage platform, and a platform hole for the spiral drill of the spiral drilling mechanism to pass through is provided on the fuselage plane.

[0008] Furthermore, a slide groove is provided on the lower side of the fuselage platform, and the upper end of the measuring pile column is slidably connected to the slide groove.

[0009] Furthermore, the slide groove is a T-shaped slide groove, and one end of the measuring pile column is provided with a T-shaped sliding end portion.

[0010] Furthermore, the walking mechanism includes a hydraulic lifting leg and a support boat, the upper end of the hydraulic lifting leg is connected to the fuselage platform, and the lower end is slidably connected to the slide rail on the support boat.

[0011] Furthermore, a lifting leg driving cylinder for driving the hydraulic lifting legs to slide is installed on the support vessel, and a piston rod of the lifting leg driving cylinder is hinged to the hydraulic lifting legs.

[0012] Furthermore, it also includes an operating room, which is installed on one side of the fuselage platform in a manner that it can be raised and lowered on the upper and lower sides of the fuselage platform.

[0013] Furthermore, a support platform is provided on one side of the fuselage platform extending outward, an operating room lifting cylinder is vertically installed on the fuselage platform, the piston rod of the operating room lifting cylinder is installed with an operating room mounting platform, and the operating room is installed on the operating room mounting platform.

[0014] Furthermore, a flip bracket is installed on one side of the fuselage platform, and a generator set for supplying power to the spiral drilling mechanism and the operating room is installed above the flip bracket.

[0015] Compared with the prior art, the advantages of the present invention are:

[0016] The fuselage platform of the present invention can accommodate the installation of an auger drilling mechanism and a counterweight. When the auger drilling mechanism is installed on the fuselage platform, pile holes can be drilled. After the pile is driven, the auger drilling mechanism is removed, the fuselage platform is moved to the location of the pile, the pile test column is pressed onto the pile, and the counterweight is gradually added to the fuselage platform to test the maximum load-bearing capacity of the pile. The main structure, including the fuselage platform and the traveling mechanism, can be shared, thus achieving multiple uses of the machine and significantly saving costs. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 1 is a schematic front view of a multifunctional auger pile drilling machine disclosed in a preferred embodiment of the invention (the short boat and the short boat legs are not shown);

[0018] Figure 2 yes Figure 1 A magnified schematic diagram of point A;

[0019] Figure 3 It is a schematic front view of the multifunctional auger pile drilling machine disclosed in the preferred embodiment of the invention (with the longboat hidden);

[0020] Figure 4 It is a left side schematic diagram of the multifunctional spiral drilling pile testing machine disclosed in the preferred embodiment of the invention;

[0021] Figure 5 It is a top view schematic diagram of the multifunctional auger pile testing machine disclosed in the preferred embodiment of the invention (without the auger drilling mechanism and counterweight installed).

[0022] Legend:

[0023] 1. Fuselage platform; 11. Fuselage plane; 12. Platform hole; 13. Slide; 15. Support platform; 16. Operator cab lifting cylinder; 17. Operator cab mounting platform; 18. Flip bracket; 2. Travel mechanism; 21. Hydraulic lifting legs; 22. Support boat; 221. Slide rail; 222. Long boat; 223. Short boat; 23. Lifting leg drive cylinder; 3. Auger drilling mechanism; 31. Auger; 4. Counterweight; 5. Measurement pile column; 51. T-shaped sliding end; 6. Operator cab; 7. Generator set. DETAILED DESCRIPTION

[0024] To facilitate understanding of the present invention, the present invention will be described in more comprehensive and detailed form below in conjunction with the accompanying drawings and preferred embodiments. However, the protection scope of the present invention is not limited to the following specific embodiments.

[0025] like Figure 1-5 As shown, this embodiment discloses a multifunctional auger pile testing machine, including a body platform 1, a traveling mechanism 2, an auger drilling mechanism 3 and a counterweight 4. The traveling mechanism 2 is mounted on the lower side of the body platform 1, and the counterweight 4 is stacked on the upper side of the body platform 1. The auger drilling mechanism 3 is detachably mounted on the body platform 1. A pile testing column 5 for pressing on an engineering pile (the engineering pile includes a prefabricated pile prefabricated in a factory, a prefabricated pile pressed in on site, and a cast-in-place pile directly cast on site) is mounted on the lower side of the body platform 1. Thus, the body platform 1 can accommodate the installation of the auger drilling mechanism 3 and the counterweight 4. When the auger drilling mechanism 3 is mounted on the body platform 1, pile holes can be drilled. After the pile is pressed, the auger drilling mechanism 3 is disassembled, the body platform 1 is moved to the position of the engineering pile, the pile testing column 5 is pressed on the engineering pile, and the counterweight is gradually added to the body platform 1. Then, the maximum bearing capacity of the engineering pile is detected to achieve the purpose. The main structures such as the body platform 1 and the traveling mechanism 2 can be shared, thereby greatly saving costs.

[0026] In this embodiment, a fuselage plane 11 for stacking counterweights 4 is provided on the upper side of the fuselage platform 1. The plane structure can be better used for stacking counterweights. A platform hole 12 for the spiral drill 31 of the spiral drilling mechanism 3 to pass through is provided on the fuselage plane 11. The platform hole 12 deviates from the center of gravity position of the platform hole 12 and is used for the spiral drill 31 to penetrate the fuselage plane 11 to drill pile holes.

[0027] In this embodiment, a slide groove 13 is provided on the underside of the fuselage platform 1, with the upper end of the pile column 5 slidingly engaged with the slide groove 13. Specifically, the slide groove 13 is a T-shaped slide groove, and one end of the pile column 5 is provided with a T-shaped sliding end 51. This facilitates quick removal and installation of the pile column 5 and also facilitates adjustment of the pile column 5 to align with the precast pile.

[0028] In this embodiment, the walking mechanism 2 includes a hydraulic lifting leg 21 and a support boat 22. The support boat 22 includes long boats 222 on both sides of the transverse direction and short boats 223 on both sides of the longitudinal direction. The long boat 222 and the short boat 223 are both provided with a slide rail 221. The upper end of the hydraulic lifting leg 21 is connected to the fuselage platform 1, and the lower end is slidably connected to the slide rail 221 on the support boat 22. Specifically, a lifting leg driving cylinder 23 for driving the hydraulic lifting leg 21 to slide is installed on the support boat 22. The piston rod of the lifting leg driving cylinder 23 is hinged to the hydraulic lifting leg 21, so that Figure 4 The fuselage platform 1 can move left and right relative to the long ship 222 and longitudinally relative to the short ship 223, thereby accurately aligning the pile column 5 with the precast pile.

[0029] In this embodiment, in order to simultaneously monitor the working conditions on the upper and lower sides of the fuselage platform 1, ensuring rapid and safe construction, an operator's cab 6 is also included. The operator's cab 6 is mounted on one side of the fuselage platform 1 so that it can be raised and lowered. Specifically, a support platform 15 is provided extending outward from one side of the fuselage platform 1. An operator's cab lifting cylinder 16 is vertically mounted on the fuselage platform 1. The operator's cab lifting cylinder 16 can be connected in parallel with the hydraulic system of the fuselage platform 1. The piston rod of the operator's cab lifting cylinder 16 is mounted to an operator's cab mounting platform 17, and the operator's cab 6 is mounted on the operator's cab mounting platform 17.

[0030] In this embodiment, a flip bracket 18 is installed on one side of the fuselage platform 1. The flip bracket 18 is cantilevered relative to the fuselage platform 1 and does not occupy the space for stacking counterweights. A generator set 7 for powering the spiral drilling mechanism 3 and the operating room 6 is installed above the flip bracket 18, that is, the generator set 7 is a common power supply center. The generator set 7 can be easily disassembled and will not interfere with the stacking measurement of the counterweight 4.

[0031] Although the present invention has been disclosed above with reference to preferred embodiments, this is not intended to limit the present invention. Any person skilled in the art can, without departing from the scope of the technical solution of the present invention, utilize the technical content disclosed above to make many possible changes and modifications to the technical solution of the present invention, or modify it into an equivalent embodiment with equivalent changes. Therefore, any simple modification, equivalent change, and modification made to the above embodiments based on the technical essence of the present invention without departing from the content of the technical solution of the present invention shall fall within the scope of protection of the technical solution of the present invention.

Claims

1. A multifunctional auger pile testing machine, characterized in that: The invention comprises a fuselage platform (1), a walking mechanism (2), a spiral drilling mechanism (3) and a counterweight (4), wherein the walking mechanism (2) is mounted on the lower side of the fuselage platform (1), the counterweight (4) is stacked on the upper side of the fuselage platform (1), the spiral drilling mechanism (3) is detachably mounted on the fuselage platform (1), and a measuring pile column (5) for pressing on an engineering pile is mounted on the lower side of the fuselage platform (1); a slide groove (13) is provided on the lower side of the fuselage platform (1), and the upper end of the measuring pile column (5) is slidably connected to the slide groove (13); the slide groove (13) ) is a T-shaped slide groove, and one end of the measuring pile column (5) is provided with a T-shaped sliding end portion (51); the upper side of the fuselage platform (1) is provided with a fuselage plane (11) for stacking the counterweight (4), and the fuselage plane (11) is provided with a platform hole (12) for the spiral drill (31) of the spiral drilling mechanism (3) to pass through; the walking mechanism (2) includes a hydraulic lifting leg (21) and a support ship (22), the upper end of the hydraulic lifting leg (21) is connected to the fuselage platform (1), and the lower end is slidably connected to the slide rail (221) on the support ship (22).

2. The multifunctional auger pile testing machine according to claim 1, characterized in that: A lifting leg driving oil cylinder (23) for driving the hydraulic lifting leg (21) to slide is installed on the support vessel (22), and a piston rod of the lifting leg driving oil cylinder (23) is hinged to the hydraulic lifting leg (21).

3. The multifunctional auger pile testing machine according to any one of claims 1-2, characterized in that: It also includes an operating room (6), which is installed on one side of the fuselage platform (1) in a manner that it can be raised and lowered on the upper and lower sides of the fuselage platform (1).

4. The multifunctional auger pile testing machine according to claim 3, characterized in that: A support platform (15) is provided on one side of the fuselage platform (1) extending outward, an operating room lifting oil cylinder (16) is vertically mounted on the fuselage platform (1), a piston rod of the operating room lifting oil cylinder (16) is mounted on an operating room mounting platform (17), and the operating room (6) is mounted on the operating room mounting platform (17).

5. The multifunctional auger pile testing machine according to claim 3, characterized in that: A flip bracket (18) is installed on one side of the fuselage platform (1), and a generator set (7) for supplying power to the spiral drilling mechanism (3) and the operating room (6) is installed above the flip bracket (18).

Citation Information

Patent Citations

  • Novel walking type static test platform machine

    CN108331036A

  • Multifunctional spiral pile drilling machine

    CN211849421U

  • Multifunctional twist drill pile measuring machine

    CN215329881U