Separating type hydraulic rail straightening device
Patent Information
- Application Number
- CN202422413533.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-30
- Publication Date
- 2025-07-18
- Estimated Expiration
- 2034-09-30
AI Technical Summary
The existing hydraulic straight rail devices have large weight, small application range and damage to the rail head.
A separate hydraulic straight rail device is designed, including a body frame body, oil cylinder assembly, lock hook assembly and clearance adjustment component. The body frame body body and lock hook assembly are designed to be separated. The lock hook assembly is equipped with a third top block and abutting the bending part of the rail. The clearance adjustment component is used to fill the gap and increase the force range of the straight rail.
It reduces the labor intensity of operators, expands the scope of application, avoids local deformation and damage to the rail head, and improves the efficiency and accuracy of the straight rail.
Smart Images

Figure CN223118771U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of railway maintenance appliances, and particularly to a separable hydraulic rail straightener. Background Art
[0002] Rail is the most fundamental and important component of a railway track, and the condition of the rail affects the running safety of trains. During the production, transportation, and construction processes of rails, problems such as distortion and hard bend may occur. If the rails with problems are laid on the line, it will cause harm such as gauge over-tolerance and installation difficulties.
[0003] Currently, the problems existing in the above-mentioned rails are mainly repaired by using a track hydraulic rail straightener. The existing hydraulic rail straighteners are mainly divided into two categories.
[0004] The first category: an integral hydraulic rail straightener, that is, the body frame and the top block for straightening the rail are integrally arranged. Since different types of rails require different top blocks, the versatility of the integral hydraulic rail straightener is poor. At the same time, the weight of the straightener corresponding to heavy rails is also large. It is difficult for operators to install and operate the machine, increasing the labor intensity.
[0005] The second category: a separable hydraulic rail straightener, that is, the underframe assembly and the locking hook assembly are separated. However, the assembly position of the locking hook and the underframe of the existing separable hydraulic rail straightener is fixed and non-adjustable, and the range of the straightening force is small, and its practicability for heavy-haul railways is poor. During operation, its acting force contacts the side surface of the rail head, and only local deformation of the rail head can be achieved. As the train passes, the local deformation will disappear, and new damage will also be caused to the working surface of the rail head. Summary of the Utility Model
[0006] In view of this, the purpose of the present application is to provide a separable hydraulic rail straightener to solve the problems of large weight, small applicable range, and damage to the rail head of the existing hydraulic rail straighteners.
[0007] According to the present utility model, a separable hydraulic rail straightener is provided, wherein the separable hydraulic rail straightener includes: a body frame main body, a first top block is installed at a first end of the body frame main body, and the first top block is used to abut against the web of the rail; an oil cylinder assembly, which is arranged at a second end of the body frame main body, the oil cylinder assembly is installed with a second top block, the second top block is used to abut against the web of the rail, and the oil cylinder assembly can drive the second top block to apply pressure to the web of the rail; a locking hook assembly, the locking hook assembly can be installed on the body frame main body, the locking hook assembly is provided with a third top block, when the locking hook assembly is installed on the body frame main body, the body frame main body and the rail are clamped inside the locking hook assembly, and the third top block abuts against the lower jaw of the rail head and the upper surface of the rail bottom at the bent part of the rail; and a gap adjustment assembly, which is movably installed on the body frame main body, when the locking hook assembly is installed on the body frame main body, the gap adjustment assembly is clamped between the locking hook assembly and the body frame main body, and is used to fill the gap between the locking hook assembly and the body frame main body.
[0008] Preferably, the locking hook assembly includes a locking hook main body, the locking hook main body is formed in a U shape, and the third top block is arranged inside the locking hook main body.
[0009] Preferably, the gap adjustment assembly includes: an adjustment assembly main body, the bottom side of which is formed as an open side, the bottom side of the adjustment assembly main body is clamped on the body frame main body, the adjustment assembly main body can move along the length direction of the body frame main body, the top side of the adjustment assembly main body is provided with an inclined surface, and the inclined surface extends in the length direction of the body frame main body; a fixing bolt, which penetrates through the body frame main body, a strip-shaped groove extending along the length direction of the body frame main body is opened on the adjustment assembly main body, and the fixing bolt penetrates through the strip-shaped groove; and a plurality of locking nuts, which are installed on the fixing bolt, and the plurality of locking nuts are respectively arranged on both sides of the adjustment assembly main body.
[0010] Preferably, a straight section is arranged in the middle of the body frame main body, the gap adjustment assembly is installed on the straight section, and the adjustment assembly main body can move on the straight section.
[0011] Preferably, the oil cylinder assembly includes: an oil tank; a cylinder block connected to the oil tank; a piston cylinder connected to the cylinder block, the piston cylinder being installed at the second end of the main body of the fuselage frame; a piston rod disposed in the piston cylinder, the piston rod being connected to the third top block; a plunger pump core assembly installed in the cylinder block. When the plunger pump core assembly moves in the first direction, the pressurized oil in the oil tank enters the cylinder block. When the plunger pump core assembly moves in the second direction, the pressurized oil in the cylinder block enters the piston cylinder to drive the piston rod to extend; and a swing rod assembly pivotally installed on the main body of the fuselage frame, the swing rod assembly being connected to the plunger pump core assembly, and the swing rod assembly being capable of driving the plunger pump core assembly to move in the first direction or the second direction during the swinging process.
[0012] Preferably, a sleeve portion is provided at the second end of the main body of the fuselage frame, and the piston cylinder is installed in the sleeve portion.
[0013] Preferably, the swing rod assembly includes: a connecting member, the first end of the connecting member being pivotally connected to the sleeve portion; a pressure oil connecting sleeve pivotally connected to the second end of the connecting member, the middle of the pressure oil connecting sleeve being pivotally connected to the plunger pump core assembly; and a lever, a hand-held portion being provided at the first end of the lever, and the second end of the lever being capable of being inserted into the pressure oil connecting sleeve.
[0014] Preferably, the split-type hydraulic straightening device for rails further includes a measuring assembly, and the measuring assembly includes: a power supply box body detachably installed on the main body of the fuselage frame; a power switch installed on the power supply box body; a distance measuring assembly connected to the power supply box body through a wire; a display screen provided on the power supply box body, the display screen being capable of displaying the measured value of the distance measuring assembly; a threaded pipe provided at the bottom of the distance measuring assembly; and a telescopic support leg frame installed on the threaded pipe, the telescopic support leg frame extending out of the bottom end of the threaded pipe.
[0015] Preferably, a plurality of traveling assemblies for traveling along the rail are provided on the main body of the fuselage frame, and the traveling assemblies include traveling wheels.
[0016] Preferably, a fixed connecting sleeve is provided in the middle of the main body of the fuselage frame, and the second end of the lever is capable of being inserted into the fixed connecting sleeve.
[0017] The split hydraulic rail straightener according to the embodiment of the present utility model has a first top block installed at the first end of the main body of the body frame. The first top block is used to abut against the web of the rail. The oil cylinder assembly is arranged at the second end of the main body of the body frame. The oil cylinder assembly is installed with a second top block, and the second top block is used to abut against the web of the rail. The oil cylinder assembly can drive the second top block to apply pressure to the web of the rail. The locking hook assembly is used to be installed on the main body of the body frame. The split design of the locking hook assembly and the main body of the body frame can avoid the overall weight of the rail straightener being too heavy, making it easy for the operator to install and operate. The locking hook assembly is provided with a third top block. When the locking hook assembly is installed on the main body of the body frame, the main body of the body frame and the rail are clamped inside the locking hook assembly, and the third top block abuts against the lower jaw of the rail head and the upper surface of the rail bottom at the bent part of the rail to prevent local deformation of the rail head. The third top block, the first top block and the second top block are respectively located on both sides of the rail, thus forming a lever structure. The first top block can be used as a fulcrum. When the third top block presses against the bent part of the rail, applying pressure to the web of the rail by the second top block can enable the third top block to apply a rail straightening force to the bent part of the rail. The gap adjustment assembly is movably installed on the main body of the body frame. When the locking hook assembly is installed on the main body of the body frame, the gap adjustment assembly is clamped between the locking hook assembly and the main body of the body frame, and is used to fill the gap between the locking hook assembly and the main body of the body frame, so that the locking hook assembly can be flexibly installed at multiple parts of the main body of the body frame, thereby increasing the range within which the rail straightening force can be applied. In this way, the problems of the existing hydraulic rail straightener, such as large weight, small applicable range and damage to the rail head, can be effectively solved.
[0018] To make the above objects, features and advantages of the present application more obvious and understandable, the following specifically enumerates preferred embodiments and, in conjunction with the accompanying drawings, makes the following detailed description. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] To more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings required in the embodiments. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be regarded as limiting the scope. For those of ordinary skill in the art, without creative efforts, other related drawings can also be obtained based on these drawings.
[0020] Figure 1 is a schematic diagram of the split hydraulic rail straightener and the rail according to the present utility model.
[0021] Figure 2 is a schematic diagram of the split hydraulic rail straightener according to the present utility model.
[0022] Figure 3 is a schematic diagram of the locking hook assembly of the split hydraulic rail straightener according to the present utility model.
[0023] Figure 4It is a partial structural schematic diagram of the separable hydraulic rail straightener according to the present utility model.
[0024] Figure 5 It is a schematic diagram of the oil cylinder assembly of the separable hydraulic rail straightener according to the present utility model.
[0025] Figure 6 It is a schematic diagram of the oil cylinder assembly of the separable hydraulic rail straightener from another angle.
[0026] Figure 7 It is a schematic diagram of the steel rail according to the present utility model.
[0027] Reference numerals: 1 - main body of the fuselage frame; 10 - first top block; 11 - straight section; 12 - sleeve part; 13 - fixed connection sleeve; 2 - oil cylinder assembly; 20 - second top block; 21 - fuel tank; 22 - cylinder block; 23 - piston cylinder; 231 - piston rod; 24 - plunger pump core assembly; 251 - connecting piece; 252 - pressure oil connection sleeve; 253 - lever; 2530 - hand - holding part; 26 - oil return valve; 27 - spare oil return valve; 28 - overflow valve; 3 - hook assembly; 30 - third top block; 31 - hook main body; 4 - clearance adjustment assembly; 40 - main body of the adjustment assembly; 400 - inclined plane; 401 - strip - shaped groove; 41 - fixing bolt; 42 - lock nut; 5 - measuring assembly; 50 - wire; 51 - power supply box body; 52 - power switch; 53 - distance - measuring assembly; 54 - display screen; 55 - threaded pipe; 56 - telescopic support frame; 6 - traveling assembly; 7 - steel rail; 71 - rail head; 710 - lower jaw of the rail head; 72 - rail web; 730 - upper surface of the rail base. Detailed implementation manners
[0028] The following detailed implementation manners are provided to help the reader obtain a comprehensive understanding of the methods, devices, and / or systems described herein. However, after understanding the disclosure of the present application, various changes, modifications, and equivalents of the methods, devices, and / or systems described herein will be apparent. For example, the order of operations described herein is merely exemplary and is not limited to the order set forth herein. Rather, changes that will be apparent after understanding the disclosure of the present application can be made, except for operations that must occur in a specific order. In addition, descriptions of features known in the art may be omitted for the sake of clarity and conciseness.
[0029] The features described herein may be implemented in different forms and should not be construed as limited to the examples described herein. Rather, the examples described herein are provided only to illustrate some of the many possible ways of implementing the methods, devices, and / or systems described herein that will be apparent after understanding the disclosure of the present application.
[0030] Throughout the specification, when an element (such as, a layer, a region, or a substrate) is described as being "on" another element, "connected to" another element, "coupled to" another element, "above" another element, or "covering" another element, it can be directly "on" another element, "connected to" another element, "coupled to" another element, "above" another element, or "covering" another element, or there can be one or more other elements intervening therebetween. In contrast, when an element is described as being "directly on" another element, "directly connected to" another element, "directly coupled to" another element, "directly above" another element, or "directly covering" another element, there can be no other elements intervening therebetween.
[0031] As used herein, the term "and / or" includes any one of the listed related items and any combination of any two or more of them.
[0032] Although terms such as "first", "second", and "third" may be used herein to describe various components, elements, regions, layers, or parts, these components, elements, regions, layers, or parts are not limited by these terms. Rather, these terms are only used to distinguish one component, element, region, layer, or part from another. Thus, a first component, element, region, layer, or part described in the examples herein may also be referred to as a second component, element, region, layer, or part without departing from the teachings of the examples.
[0033] For ease of description, spatial relationship terms such as "above", "upper", "below", and "lower" may be used herein to describe the relationship of one element to another as shown in the figures. Such spatial relationship terms are intended to include different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, an element described as "above" or "upper" relative to another element will then be "below" or "lower" relative to the other element. Thus, the term "above" includes both the orientations of "above" and "below" depending on the spatial orientation of the device. The device may also be positioned in other ways (e.g., rotated 90 degrees or in other orientations), and the spatial relationship terms used herein will be interpreted accordingly.
[0034] The terms used herein are for the purpose of describing various examples only and are not intended to limit the examples. Unless the context clearly indicates otherwise, the singular forms are also intended to include the plural forms. The terms "comprising", "including" and "having" enumerate the stated features, quantities, operations, components, elements and / or combinations thereof that exist, but do not preclude the existence or addition of one or more other features, quantities, operations, components, elements and / or combinations thereof.
[0035] Due to manufacturing techniques and / or tolerances, variations in the shapes shown in the drawings may occur. Accordingly, the examples described herein are not limited to the specific shapes shown in the drawings, but include changes in shape that occur during manufacturing.
[0036] The features of the examples described herein can be combined in various ways that will be apparent after understanding the disclosure of the present application. In addition, although the examples described herein have various configurations, other configurations are possible, as will be apparent after understanding the disclosure of the present application.
[0037] As Figures 1 to 7 shown, according to a first aspect of the present utility model, a separable hydraulic rail straightener is provided, which includes a body frame main body 1, an oil cylinder assembly 2, a locking hook assembly 3, and a clearance adjustment assembly 4.
[0038] In the following description, reference will be made to Figures 1 to 7 specifically describe the specific structures of the above components of the separable hydraulic rail straightener and the connection relationships of the above components.
[0039] As Figures 1 to 7 shown, in an embodiment, a first top block 10 may be installed at the first end (which may be the right end as Figure 2 shown) of the body frame main body 1. The first top block 10 is used to abut against the web 72 of the rail 7. The oil cylinder assembly 2 may be disposed at the second end (which may be as Figure 2The left end shown). The oil cylinder assembly 2 may be installed with a second top block 20. The second top block 20 is used to abut against the web 72 of the rail 7, and the oil cylinder assembly 2 can drive the second top block 20 to apply pressure to the web 72 of the rail 7. The locking hook assembly 3 can be installed on the main body 1 of the fuselage frame. The separable design of the locking hook assembly 3 and the main body 1 of the fuselage frame can prevent the overall weight of the separable hydraulic rail straightener from being too large, making it easy for the operator to disassemble and transport. The locking hook assembly 3 may be provided with a third top block 30. When the locking hook assembly 3 is installed on the main body 1 of the fuselage frame, the main body 1 of the fuselage frame and the rail 7 are clamped inside the locking hook assembly 3. The third top block 30 abuts against the lower jaw 710 of the rail head and the upper surface 730 of the rail bottom at the bent part of the rail 7 to prevent local deformation of the rail head 71. The third top block 30, the first top block 10, and the second top block 20 may be located on both sides of the rail 7 respectively, thus forming a lever structure. The first top block 10 may serve as a fulcrum. When the third top block 30 presses against the bent part of the rail 7, applying pressure to the web 72 of the rail 7 by the second top block 20 can enable the third top block 30 to apply a rail straightening force to the bent part of the rail 7. The gap adjustment assembly 4 can be movably installed on the main body 1 of the fuselage frame. When the locking hook assembly 3 is installed on the main body 1 of the fuselage frame, the gap adjustment assembly 4 is clamped between the locking hook assembly 3 and the main body 1 of the fuselage frame to fill the gap between the locking hook assembly 3 and the main body 1 of the fuselage frame, enabling the locking hook assembly 3 to be flexibly installed at multiple parts of the main body 1 of the fuselage frame to increase the range within which the rail straightening force can be applied.
[0040] Preferably, as Figures 1 to 3 shown, in the embodiment, the main body 1 of the fuselage frame can be approximately strip-shaped. When in use, the main body 1 of the fuselage frame can be arranged along the length direction of the rail 7. The main body 1 of the fuselage frame is arranged on one side of the rail 7. The locking hook assembly 3 is separately arranged from the main body 1 of the fuselage frame. During transportation, the operator can transport the locking hook assembly 3 and the main body 1 of the fuselage frame separately and then install them together when in use. The locking hook assembly 3 may include a locking hook main body 31. Preferably, the locking hook main body 31 can be a U-shaped plate member. The third top block 30 can be arranged inside the locking hook main body 31, that is, inside the opening of the locking hook main body 31. The third top block 30 can be bolted to the locking hook main body 31. When the locking hook assembly 3 is installed on the main body 1 of the fuselage frame, the third top block 30 and the main body 1 of the fuselage frame are located on opposite sides of the rail 7 respectively.
[0041] In addition, preferably, as Figure 1 and Figure 2 and Figure 7As shown, in the embodiment, the first top block 10, the second top block 20, and the third top block 30 can be plate-shaped components. The sides of the first top block 10 and the second top block 20 are in contact with the web 72. The side of the third top block 30 is in contact with the lower jaw 710 of the rail head and the upper surface 730 of the rail base of the rail 7. With such a setting, it can not only protect the rail head 71 from damage, but also straighten the bent part of the rail 7 and prevent local deformation of the rail head 71.
[0042] Preferably, as Figures 1 to 3 shown, in the embodiment, the gap adjustment assembly 4 and the first top block 10 and the second top block 20 can be respectively arranged on both sides of the fuselage frame main body 1. The gap adjustment assembly 4 can include an adjustment assembly main body 40, a fixing bolt 41, and a locking nut 42. Among them, the bottom side of the adjustment assembly main body 40 (i.e., the side facing the side part of the fuselage frame main body 1 as shown in Figure 2 can be formed as an open side. The bottom side of the adjustment assembly main body 40 can be clamped on the fuselage frame main body 1, that is, the plate part of the fuselage frame main body 1 is inserted into the open side of the adjustment assembly main body 40. The adjustment assembly main body 40 can move along the length direction of the fuselage frame main body 1. On the top side of the adjustment assembly main body 40 (i.e., the side facing the hook assembly 3 as shown in Figure 1 ), an inclined surface 400 can be provided, and the inclined surface 400 extends in the length direction of the fuselage frame main body 1. By moving the adjustment assembly main body 40, the gap between the hook assembly 3 and the fuselage frame main body 1 can be adjusted, so that the hook assembly 3 can remain stable during operation. In addition, the adjustment assembly main body 40 can move following the installation position of the hook assembly 3, so that the range of the straightening force of the rail can be adjusted. The fixing bolt 41 can pass through the plate part of the fuselage frame main body 1. A strip-shaped groove 401 extending along the length direction of the fuselage frame main body 1 can be formed on the adjustment assembly main body 40. The fixing bolt 41 also passes through the strip-shaped groove 401. Preferably, the number of the fixing bolts 41 can be multiple. A plurality of the locking nuts 42 can be installed on the plurality of the fixing bolts 41. The plurality of the locking nuts 42 can be respectively arranged on both sides of the adjustment assembly main body 40, and then the adjustment assembly main body 40 is locked and fixed to the fuselage frame main body 1.
[0043] More preferably, as Figure 1 and Figure 2 shown, in the embodiment, the middle part of the fuselage frame main body 1 can be formed as a plate part, and the plate part is formed with a straight section 11. The gap adjustment assembly 4 can be installed on the straight section 11. The adjustment assembly main body 40 can move on the straight section 11 to adapt to the installation position of the hook assembly 3.
[0044] Preferably, as Figures 1 to 5As shown, in the embodiment, the oil cylinder assembly 2 may include an oil tank 21, a cylinder block 22, a piston cylinder 23, a piston rod 231, a plunger pump core assembly 24, and a swing rod assembly. Among them, the oil tank 21 may be formed in a cylindrical shape, and pressure oil is stored inside the oil tank 21. The cylinder block 22 may be connected to the end of the oil tank 21. The piston cylinder 23 is connected to the cylinder block 22. The piston cylinder 23 is fixedly installed at the second end of the fuselage frame main body 1. The piston rod 231 is disposed inside the piston cylinder 23. The piston rod 231 may be connected to the third top block 30 to drive the third top block 30 to move. The plunger pump core assembly 24 may be installed outside the cylinder block 22. When the plunger pump core assembly 24 moves in the first direction, the pressure oil in the oil tank 21 can enter the cylinder block 22, and the first direction may be the upward direction as shown in Figure 4 , that is, lifting the plunger pump core assembly 24. When the plunger pump core assembly 24 moves in the second direction, the pressure oil in the cylinder block 22 can enter the piston cylinder 23, and the second direction may be the downward direction as shown in Figure 4 , that is, pressing down the plunger pump core assembly 24. After the pressure oil enters the piston cylinder 23, it can drive the piston rod 231 to extend, and then drive the third top block 30 to apply pressure to the rail 7. The swing rod assembly is swingably installed on the fuselage frame main body 1. The swing rod assembly may be connected to the plunger pump core assembly 24. During the swinging process of the swing rod assembly, it can drive the plunger pump core assembly 24 to move in the first direction or the second direction.
[0045] Specifically, as shown in Figures 2 to 5 , in the embodiment, a cylindrical sleeve portion 12 may be provided at the second end of the fuselage frame main body 1. The piston cylinder 23 may be snap-fitted and installed inside the sleeve portion 12. The swing rod assembly may include a connecting member 251, a pressure oil connecting sleeve 252, and a lever 253. Among them, the connecting member 251 may be a strip-shaped plate member. The first end of the connecting member 251 (which may be the lower end as shown in Figure 4 ) is pivotally connected to the sleeve portion 12. The end of the pressure oil connecting sleeve 252 may be pivotally connected to the second end of the connecting member 251 (which may be the upper end as shown in Figure 4 ). The middle of the pressure oil connecting sleeve 252 may be pivotally connected to the plunger pump core assembly 24. During the pivotal swinging process of the pressure oil connecting sleeve 252, the plunger pump core assembly 24 moves with the pressure oil connecting sleeve 252. The first end of the lever 253 may be provided with a handgrip portion 2530 to facilitate the operator's grasping. The second end of the lever 253 may be inserted into the pressure oil connecting sleeve 252, and the lever 253 may be threadedly connected to the pressure oil connecting sleeve 252. The operator can drive the pressure oil connecting sleeve 252 to swing by manipulating the lever 253.
[0046] More preferably, the oil cylinder assembly 2 may further include an oil return valve 26, a spare oil return valve 27, and an overflow valve 28. The oil return valve 26, the spare oil return valve 27, and the overflow valve 28 may be installed on the cylinder block 22. During use, the lever 253 is inserted into the pressure oil connection sleeve 252. When the pressure oil connection sleeve 252 is lifted, the plunger pump core assembly 24 is driven to move upward, and the pressurized oil in the fuel tank 21 enters the cylinder block 22 through the filter and the oil suction valve. When the pressure oil connection sleeve 252 is pressed down, the plunger pump core assembly 24 is driven to move downward, and the pressurized oil then enters the piston cylinder 23 to push the piston rod 231 to work. After the work is completed, the oil return valve 26 is opened, and the pressurized oil in the piston cylinder 23 pushes open the steel ball and returns to the fuel tank 21, and the piston rod 231 is reset by the return spring.
[0047] In addition, preferably, as Figure 1 and Figure 2 shown, in the embodiment, a plurality of traveling components 6 for traveling along the rail 7 may be further provided on the main body 1 of the fuselage frame. Preferably, the traveling component 6 may include a traveling wheel and a bracket for installing the traveling wheel, and the bracket may be bolted to the main body 1 of the fuselage frame. The traveling component 6 may be installed on one side of the main body 1 of the fuselage frame where the gap adjustment component 4 is provided. Preferably, two traveling components 6 may be respectively provided at both ends in the length direction of the main body 1 of the fuselage frame. With such a setting, the split hydraulic straightening device can travel along the rail 7 to reduce the handling labor intensity of the operator.
[0048] More preferably, as Figure 1 and Figure 2 shown, in the embodiment, an inclined fixed connection sleeve 13 may be provided on the plate surface in the middle of the main body 1 of the fuselage frame. Specifically, the first end of the fixed connection sleeve 13 may be integrally formed with the main body 1 of the fuselage frame, and a circular opening may be formed at the second end of the fixed connection sleeve 13. The fixed connection sleeve 13 may be inclined from the first end to the second end in the direction close to the first end of the main body 1 of the fuselage frame. The second end of the lever 253 can be inserted into the second end of the fixed connection sleeve 13 to facilitate the operator to push the split hydraulic straightening device to travel along the rail 7.
[0049] In addition, preferably, the separable hydraulic straightening device for rails may further include a measuring assembly 5, and the measuring assembly may include a power supply box body 51, a power switch 52, a distance measuring assembly 53, a display screen 54, a threaded pipe 55 and a telescopic support leg frame 56. Among them, the power supply box body 51 is detachably mounted in the middle of the main body of the fuselage frame 1. Specifically, it can be bolted. The power switch 52 can be mounted on the power supply box body for turning on or off the power supply. The distance measuring assembly 53 can be connected to the power supply box body 51 through a wire 50, and the wire 50 can be inserted and connected to the power supply box body 51. Specifically, the distance measuring assembly 53 can be a distance measuring device such as a laser displacement sensor, an eddy current sensor or a rangefinder. A display screen 54 can be arranged on the power supply box body 51, and the display screen 54 can display the measured value of the distance measuring assembly 53. The threaded pipe 55 can be arranged at the bottom of the distance measuring assembly 53. Preferably, the distance measuring assembly 53 can be bolted to the top end of the threaded pipe 55. The telescopic support leg frame 56 can be mounted on the threaded pipe 55. The top end of the telescopic support leg frame 56 can be threadedly connected to the threaded pipe 55, and the bottom end of the telescopic support leg frame 56 can extend out of the bottom end of the threaded pipe 55 for supporting on the ground. The bottom end of the telescopic support leg frame 56 can be formed into a disc shape.
[0050] When the measuring assembly 5 is working, first record the straightening amount required for straightening the rail 7, and place the separable hydraulic straightening device for rails at the designated working position. After installation, align the distance measuring assembly 53 with the rail to be straightened, turn on the power switch 52, record the initial value (or zero) of the display screen 54, and then perform the hydraulic pressure application for straightening the rail. When the data difference (or the displayed data) on the display screen 54 is the same as the straightening amount required for straightening (within the allowable error range), the pressure application can be stopped and the pressure can be maintained for two minutes. The measuring assembly 5 can accurately control the straightening amount, greatly improving the straightening efficiency and accuracy.
[0051] During the use of the separable hydraulic rail straightener, first, the bent part of the rail 7 is detected to measure the straightening amount value. Then, the sleeper fasteners on both sides of the bent part of the rail 7 are loosened. The separable hydraulic rail straightener is placed on the opposite side of the direction where the rail 7 needs to be straightened, and a top block adapted to the rail shape is installed. Then, the third top block 30 of the hook assembly 3 is abutted against the part to be straightened, and the first top block 10 and the second top block 20 are abutted against the rail web 72. The gap adjustment assembly 4 is adjusted until the hook assembly 3 is fixed. The distance measuring assembly 53 of the measuring assembly 5 is placed in the direction where the rail 7 needs to be straightened and is collinear with the third top block 30. Subsequently, the oil return valve 26 and the spare oil return valve 27 are tightened, and then the lever 253 is inserted into the oil pressing connecting sleeve 252. The swing of the lever 253 can extend the piston rod 231. The lever 253 is swung multiple times until the required straightening amount is reached, and then the pressure is maintained for 2 minutes to achieve the purpose of straightening the rail 7. After the work is completed, the oil return valve 26 is loosened, and the piston rod 231 can automatically reset. The operator can remove the separable hydraulic rail straightener from the track to perform the next cycle of operation.
[0052] Finally, it should be noted that the above embodiments are only specific embodiments of the present application, which are used to illustrate the technical solutions of the present application, rather than limiting them. The protection scope of the present application is not limited thereto. Although the present application has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: any person skilled in the art within the technical scope disclosed in the present application can still modify the technical solutions recorded in the foregoing embodiments, or can easily think of changes, or perform equivalent replacements for some of the technical features; and these modifications, changes or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present application, and should all be covered by the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.
Claims
1. A separable hydraulic straight rail aligner, characterized in that, The separable hydraulic rail straightener includes: A main body of the frame. A first top block is installed at the first end of the main body of the frame, and the first top block is used to abut against the web of the rail. An oil cylinder assembly is arranged at the second end of the main body of the frame. A second top block is installed on the oil cylinder assembly, and the second top block is used to abut against the web of the rail. The oil cylinder assembly can drive the second top block to apply pressure to the web of the rail. A locking hook assembly. The locking hook assembly can be installed on the main body of the frame. The locking hook assembly is provided with a third top block. When the locking hook assembly is installed on the main body of the frame, the main body of the frame and the rail are clamped inside the locking hook assembly, and the third top block abuts against the lower jaw of the rail head and the upper surface of the rail bottom at the bent part of the rail; and A gap adjustment component is movably installed on the main body of the frame. When the locking hook assembly is installed on the main body of the frame, the gap adjustment component is clamped between the locking hook assembly and the main body of the frame and is used to fill the gap between the locking hook assembly and the main body of the frame.
2. The separable hydraulic straight rail bender according to claim 1, wherein, The locking hook assembly includes a locking hook main body, and the locking hook main body is formed in a U shape, and the third top block is arranged inside the locking hook main body.
3. The separable hydraulic straight rail bender according to claim 2, wherein The gap adjustment component includes: A main body of the adjustment component. The bottom side of the main body of the adjustment component is formed as an open side. The bottom side of the main body of the adjustment component is clamped on the main body of the frame. The main body of the adjustment component can move along the length direction of the main body of the frame. A slope is arranged on the top side of the main body of the adjustment component, and the slope extends in the length direction of the main body of the frame; A fixing bolt is passed through the main body of the frame. A strip-shaped groove extending along the length direction of the main body of the frame is formed on the main body of the adjustment component, and the fixing bolt is passed through the strip-shaped groove; and A plurality of locking nuts are installed on the fixing bolt, and the plurality of locking nuts are respectively arranged on both sides of the main body of the adjustment component.
4. The separable hydraulic straight rail bender according to claim 3, characterized in that, A straight section is arranged in the middle of the main body of the frame, and the gap adjustment component is installed on the straight section, and the main body of the adjustment component can move on the straight section.
5. The separable hydraulic straightening tool according to claim 1, characterized in that, The oil cylinder assembly includes: An oil tank; A cylinder body is connected to the oil tank; A piston cylinder is connected to the cylinder body, and the piston cylinder is installed at the second end of the main body of the frame; A piston rod is arranged inside the piston cylinder, and the piston rod is connected to the third top block; A plunger pump core assembly is installed in the cylinder body. When the plunger pump core assembly moves in the first direction, the pressurized oil in the oil tank enters the cylinder body. When the plunger pump core assembly moves in the second direction, the pressurized oil in the cylinder body enters the piston cylinder to drive the piston rod to extend; and A swing rod assembly is swingably installed on the main body of the frame. The swing rod assembly is connected to the plunger pump core assembly, and the swing rod assembly can drive the plunger pump core assembly to move in the first direction or the second direction during the swinging process.
6. The separable hydraulic straight rail bender according to claim 5, characterized in that, A sleeve part is arranged at the second end of the main body of the frame, and the piston cylinder is installed inside the sleeve part.
7. The separable hydraulic straight rail bender according to claim 6, characterized in that, The swing rod assembly includes: A connecting piece. The first end of the connecting piece is pivotally connected to the sleeve part; An oil pressing connecting sleeve, pivotally connected to the second end of the connecting member, and the middle part of the oil pressing connecting sleeve is pivotally connected to the plunger pump core assembly; and A lever, with a handgrip portion provided at the first end of the lever, and the second end of the lever can be inserted into the oil pressing connecting sleeve.
8. The separable hydraulic straight rail bender according to claim 1, characterized in that, The separable hydraulic straight rail aligner further includes a measuring assembly, and the measuring assembly includes:[[]]END]] A power supply box body, detachably installed on the main body of the machine frame; A power switch, installed on the power supply box body; A distance measuring assembly, connected to the power supply box body through a wire; A display screen, arranged on the power supply box body, and the display screen can display the measured value of the distance measuring assembly; A threaded pipe, arranged at the bottom of the distance measuring assembly; and A telescopic support leg frame, installed on the threaded pipe, and the telescopic support leg frame extends out of the bottom end of the threaded pipe.
9. The separable hydraulic straight rail bender according to claim 7, wherein, A plurality of traveling assemblies for traveling along the rail are arranged on the main body of the machine frame, and the traveling assemblies include traveling wheels.
10. The separable hydraulic straightening device according to claim 9, characterized in that, A fixed connecting sleeve is arranged in the middle of the main body of the machine frame, and the second end of the lever can be inserted into the fixed connecting sleeve.