Oil injection device and oil filling device for turnout rotator
By integrating a container and a one-way valve structure into the turnout rotator oil injection device, convenient connection and air pressure balance between the container and the oil injection pipeline are achieved, solving the problems of container tilting and replacement waiting time, and improving oil injection efficiency and convenience.
Patent Information
- Application Number
- CN202520812608.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-27
- Publication Date
- 2026-01-23
- Estimated Expiration
- 2035-04-27
AI Technical Summary
When maintenance personnel use the lubrication device, they need to carry aviation fuel storage containers, which makes the containers prone to tipping over, affecting the lubrication operation. Furthermore, when changing the container, they need to wait for the fuel to be replenished, which reduces the lubrication efficiency of the turnout rotator.
A turnout rotator oil injection device is designed, which integrates a container for storing aviation fuel into the housing of the oil injection device. A one-way valve structure enables communication between the container and the oil injection pipeline. Multiple containers are provided for quick replacement. An oil pump is used to drive the oil injection, maintain air pressure balance, and improve the oil injection efficiency.
The oiling operation can be carried out without placing the container on the ground, and the container can be replaced quickly, which improves the oiling efficiency and ease of operation of the turnout turner.
Smart Images

Figure CN223826040U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to railway turnout rotator oil injection technical field especially relates to a turnout rotator oil injection device and oil filling device. BACKGROUND
[0002] Railway turnout is an important component of railway track structure, and the turnout rotator is used to drive the track to turn. The turnout rotator needs to be injected with oil regularly. Generally, maintenance personnel inject aviation oil into the turnout rotator by using an oil injection device so that the aviation oil level in the oil tank of the turnout rotator is kept in the middle of the oil scale. At present, when the maintenance personnel use the oil injection device, they need to carry an aviation oil storage container, put the oil suction pipe of the oil injection device into the aviation oil storage container, and then inject the aviation oil into the oil tank of the turnout rotator after the oil injection device sucks the aviation oil. However, the maintenance personnel need to place the aviation oil storage container on the ground when they operate the oil injection device to inject oil, which may cause the aviation oil storage container to be easily tilted by the oil suction pipe of the oil injection device and affect the oil injection operation. SUMMARY
[0003] The utility model aims at solving one of the technical problems in the prior art. To this end, the utility model provides a turnout rotator oil injection device and oil filling device. The container for storing aviation oil is combined into the shell of the oil injection device, so that the oil injection operation is not affected by the placement of the container on the ground. Moreover, when the aviation oil in the container is consumed, the oil injection device can continue to work by replacing another container full of aviation oil, thereby improving the oil injection efficiency of the turnout rotator.
[0004] According to the utility model first aspect embodiment's turnout rotator oil injection device, including:
[0005] The shell is internally provided with an inner cavity, and the side wall of the shell is inwardly recessed to form an installation cavity;
[0006] The oil injection pipeline is arranged in the inner cavity, and is provided with a joint and an oil injection hole. The joint is located in the installation cavity, and the oil injection hole is located at the bottom of the shell. The liquid in the oil injection pipeline is transported from the joint to the oil injection hole.
[0007] The container is provided with an interface at the bottom, and the interface is internally provided with a first one-way valve. The liquid in the container pushes the first one-way valve to move outward so as to close the interface. The top of the container is provided with an opening and a top cover which can detachably seal the opening. The top cover is provided with a second one-way valve, and the second one-way valve is connected from the outside to the inside of the container.
[0008] The container is detachably arranged in the installation cavity, the joint is inserted into the interface and pushes the first one-way valve to move to the inside of the container, so that the container is connected with the oil injection pipeline.
[0009] The turnout rotator oiling device according to the present invention has at least the following beneficial effects: Before using the oiling device, the container is removed from the mounting cavity on the side wall of the housing, the top cover of the container is opened, aviation oil is added to the container, and then the container filled with aviation oil is reinstalled into the mounting cavity of the housing. The connector of the mounting cavity is inserted into the interface at the bottom of the container, so that the connector pushes the first one-way valve to move into the container, thereby connecting the oiling pipeline and the container, so that the oiling pipeline can deliver the aviation oil in the container to the oiling hole. The maintenance personnel align the oiling hole with the oil tank filling port of the turnout rotator and inject aviation oil. The second one-way valve helps the outside air to enter the container and maintain the air pressure balance between the container and the outside. Therefore, the container storing aviation oil is combined with the housing of the oiling device, so that the container does not need to be placed on the ground to affect the oiling operation. When the aviation oil in the container is exhausted, the oiling device can continue to work by replacing another container filled with aviation oil, thereby improving the oiling efficiency of the turnout rotator.
[0010] According to some embodiments of this utility model, the length of the mounting cavity in the vertical direction is greater than the length of the container in the vertical direction, the connector is located on the bottom wall of the mounting cavity, the interface is located on the bottom wall of the container, the container is rotatably disposed in the mounting cavity, the inner side wall of the interface is provided with an internal thread, the outer side wall of the connector is provided with an external thread, and the internal thread and the external thread are engaged.
[0011] According to some embodiments of the present invention, the container is cylindrical, and a plurality of anti-slip grooves are provided on the outer side wall of the container, the plurality of anti-slip grooves being distributed at intervals along the circumference of the container.
[0012] According to some embodiments of the present invention, a stop block is provided on the periphery of the bottom of the mounting cavity, the distance from the top of the stop block to the top wall of the mounting cavity is greater than the length of the container in the vertical direction, and the stop block abuts against the outer wall of the container.
[0013] According to some embodiments of the present invention, the outer wall of the container protrudes outside the shell.
[0014] According to some embodiments of the present invention, the turnout rotator oil injection device further includes:
[0015] The power supply is located within the cavity.
[0016] An oil pump is installed in the oil injection pipeline. The oil pump is electrically connected to the power supply. Starting the oil pump causes the liquid in the oil injection pipeline to be transported from the joint to the oil injection hole.
[0017] According to some embodiments of the present invention, the top of the housing is provided with a vertically arranged handle, and the turnout rotator oil injection device further includes:
[0018] A controller is located on the handle and is electrically connected to the oil pump. The controller controls the start and stop of the oil pump.
[0019] According to some embodiments of the present invention, the sidewall of the container is transparent, and the outer sidewall of the container is provided with volume markings.
[0020] According to some embodiments of this utility model, the oil injection pipeline further includes:
[0021] A liquid inlet check valve is provided at the joint, and the liquid inlet check valve allows the oil injection pipeline to be opened from the outside to the inside of the oil injection pipeline.
[0022] A liquid outlet check valve is provided at the oil injection hole, and the liquid outlet check valve is open from the inside to the outside of the oil injection pipeline;
[0023] A piston cylinder, with both ends connected to the connector and the oil injection port, respectively;
[0024] The piston is movably disposed within the piston cylinder;
[0025] A piston rod is connected to the piston. The housing has a through-hole. The piston rod extends out of the housing through the through-hole. The piston rod moves along the through-hole to move the piston along the piston cylinder.
[0026] According to a second aspect of the present invention, an oil filling device is applied to a turnout rotary oil filling device as described in the above embodiment. The device has at least two containers, one of which is detachably disposed in the mounting cavity, and the oil filling device replenishes aviation oil to the other container.
[0027] The oil filling device according to the embodiment of the present utility model has at least the following beneficial effects: a container is installed in the mounting cavity of the oil filling device. When the maintenance personnel use the oil filling device to inject aviation oil into the oil tank of the turnout rotator, the oil filling device replenishes aviation oil to another container. When the aviation oil in the container of the oil filling device is exhausted, it can be used again after replacing the other container without waiting for the container to be replenished with aviation oil, thereby improving the oil filling efficiency of the turnout rotator. Attached Figure Description
[0028] Figure 1 This is a schematic diagram of the structure of a turnout rotator oil injection device according to an embodiment of the present invention;
[0029] Figure 2 This is an exploded view of a turnout rotator oil injection device according to an embodiment of the present invention;
[0030] Figure 3 This is an exploded view of the turnout rotator oil injection device according to another embodiment of the present invention.
[0031] Figure 4 This is a cross-sectional schematic diagram of a turnout rotator oil injection device according to an embodiment of the present invention, wherein the arrow indicates the direction of aviation oil flow.
[0032] Reference numerals: housing 100, inner cavity 110, mounting cavity 120, stop block 130, oil filling line 200, connector 210, oil filling hole 220, container 300, interface 310, first check valve 320, opening 330, top cover 340, second check valve 350, anti-slip groove 360, power supply 400, oil pump 500, handle 600, controller 700. Detailed Implementation
[0033] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.
[0034] In the description of this utility model, it should be understood that the terms front, back, up, down, axial, circumferential, etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.
[0035] In the description of this utility model, "multiple" means two or more; "greater than," "less than," and "exceeding" are understood to exclude the stated number; "above," "below," and "within" are understood to include the stated number. The use of "first" and "second" in the description is merely for distinguishing technical features and should not be construed as indicating or implying relative importance, or implicitly specifying the number of indicated technical features or their sequential relationship.
[0036] In the description of this utility model, it should be noted that terms such as "setting," "installing," and "connecting" should be interpreted broadly, and those skilled in the art can reasonably determine the specific meaning of the above terms in this utility model in conjunction with the specific content of the technical solution.
[0037] The technical solution of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the embodiments described below are some embodiments of this utility model, not all embodiments.
[0038] Reference Figures 1 to 4 As shown, this utility model provides a turnout rotator oil injection device.
[0039] ReferenceFigure 1 As shown, the turnout rotator oil injection device includes a housing 100, an oil injection pipeline 200, and a container 300.
[0040] The housing 100 has an inner cavity 110 inside, and the side wall of the housing 100 is recessed into the inner cavity 110, so that the side wall of the housing 100 forms an installation cavity 120 for accommodating the container 300.
[0041] The bottom of the housing 100 is provided with a connecting pipe that extends downwards. The outer wall of the connecting pipe is provided with external threads, which are used to connect to the oil tank threaded hole of the turnout turner.
[0042] The oil filling line 200 is installed in the inner cavity 110. The two ends of the oil filling line 200 are respectively provided with a connector 210 and an oil filling hole 220. The connector 210 is installed in the mounting cavity 120, and the oil filling hole 220 is installed in the connecting pipe at the bottom of the housing 100. The oil filling line 200 delivers the liquid from the connector 210 to the oil filling hole 220.
[0043] The container 300 is detachably disposed in the mounting cavity 120. For example, the container 300 is placed in the mounting cavity 120 and fixed by clamping the container 300 with the inner wall of the mounting cavity 120; or, the container 300 is cylindrical, with external threads on the bottom of its outer side wall, the shape of the mounting cavity 120 matches the shape of the container 300, and internal threads are provided on the bottom of its inner side wall, so that the container 300 is threadedly connected to the mounting cavity 120; or, the outer side wall of the container 300 has a snap-fit, and the inner side wall of the mounting cavity 120 has a snap fastener, so that the container 300 is inserted into the mounting cavity 120, and the snap fastener and snap-fit engage to detachably connect the container 300 to the mounting cavity 120.
[0044] The bottom of the container 300 is provided with an interface 310, the position of which corresponds to the position of the connector 210 in the mounting cavity 120. After the container 300 is placed in the mounting cavity 120, the interface 310 is directly opposite the connector 210. A first one-way valve 320 is provided in the interface 310. When the inside of the container 300 is filled with aviation oil, the aviation oil will push the first one-way valve 320 at the bottom to move outward of the container 300, causing the first one-way valve 320 to close the interface 310.
[0045] The top of the container 300 is provided with an opening 330 and a top cover 340. The top cover 340 is used to detachably seal the opening 330. A second one-way valve 350 is provided in the middle of the top cover 340. The conduction direction of the second one-way valve 350 is from the outside to the inside of the container 300.
[0046] When the container 300 is placed in the mounting cavity 120, the connector 210 is inserted into the interface 310. The connector 210 will push the first one-way valve 320 in the interface 310 to move into the interior of the container 300, so that the connector 210 of the oil injection line 200 is connected to the interface 310 of the container 300.
[0047] It is understood that the first one-way valve 320 includes a valve body, a spring, and a piston. The valve body has a through hole running along the axis inside. The first one-way valve 320 is installed in the interface 310 of the container 300. The top of the through hole is connected to the container 300, and the bottom of the through hole faces downwards from the container 300. The spring and piston are installed in the through hole. The spring connects the inner wall of the through hole to the piston. The spring pushes the piston downwards. The through hole is a stepped hole that is larger at the top and smaller at the bottom, that is, the through hole is divided into an upper section and a lower section. The diameter of the upper section is larger than that of the lower section. When the piston moves to the lower section of the through hole, the piston seals the lower section of the through hole. When the connector 210 is inserted into the interface 310, a plug is provided on the upper surface of the connector 210. The plug is vertically positioned upwards. The plug is inserted into the bottom of the through hole of the first one-way valve 320. The plug pushes the piston upwards to the upper section, and the upper and lower sections of the through hole are connected, realizing the connection between the interface 310 and the connector 210.
[0048] Understandably, the top cover 340 is provided with a vertically penetrating air inlet, and the second one-way valve 350 is disposed in the air inlet of the top cover 340. The second one-way valve 350 includes a valve body, a valve core, and a spring. The valve body is provided with a vertically penetrating through hole, and the valve core is slidably disposed in the through hole. An annular protrusion is disposed at the top of the through hole, and the spring is disposed in the through hole. The spring pushes the valve core upward to abut against the annular protrusion, thereby sealing the through hole. When the aviation fuel in the container 300 is delivered to the filling hole 220 by the filling pipeline 200, the pressure in the container 300 decreases, while the external air pressure is greater than the air pressure in the container 300. This causes the external air to push the valve core of the second one-way valve 350 downward against the spring force, thereby allowing external air to replenish the container 300, balancing the pressure between the container 300 and the external air pressure, and thus enabling the filling pipeline 200 to smoothly deliver the aviation fuel in the container 300.
[0049] Reference Figure 4 As shown, it can be understood that there are multiple ways in which the oil injection line 200 generates power to transport aviation oil.
[0050] For example, an inlet check valve is installed at connector 210, with the flow direction from the outside to the oil filling pipeline 200. An outlet check valve is installed at oil filling hole 220, with the flow direction from the inside of oil filling pipeline 200 to the outside. A piston cylinder is installed in oil filling pipeline 200, connecting connector 210 and oil filling hole 220. A piston is installed in the piston cylinder, with one end of the piston connected to a piston rod. The piston rod passes through the side wall of housing 100 and is located outside. The piston moves by pushing or pulling the piston rod. When the piston compresses the volume in the piston cylinder, the air pressure in the piston cylinder increases, causing the aviation oil in the piston cylinder to be output to the outside through the outlet check valve of oil filling hole 220. When the piston returns to its original position, the air pressure in the piston cylinder decreases. Since the oil filling hole 220 of oil filling pipeline 200 is closed by the outlet check valve, the liquid in container 300 is replenished into the piston cylinder through the inlet check valve to balance the air pressure in the piston cylinder.
[0051] Alternatively, an electric hydraulic pump can be installed in the oil filling line 200 to generate power to deliver oil from the connector 210 to the oil filling hole 220.
[0052] Before using the oil filling device, the container is removed from the mounting cavity 120 on the side wall of the housing 100. After opening the top cover 340 of the container 300, aviation oil is added to the container 300. Then, the container 300 filled with aviation oil is reinstalled into the mounting cavity 120 of the housing 100. The connector 210 of the mounting cavity 120 is inserted into the interface 310 at the bottom of the container 300, so that the connector 210 pushes the first one-way valve 320 to move into the container 300, thereby connecting the oil filling pipeline 200 and the container 300. This allows the oil filling pipeline 200 to deliver the aviation oil in the container 300 to the oil filling hole 220. The maintenance personnel align the oil filling hole 220 with the oil tank filling port of the turnout turner and inject aviation oil. Meanwhile, the second one-way valve 350 helps the outside air to enter the container 300, maintaining the air pressure balance between the container 300 and the outside.
[0053] The container 300 for storing aviation fuel is integrated into the housing 100 of the fuel injection device, eliminating the need to place the container 300 on the ground to avoid affecting the fuel injection operation. Furthermore, when the aviation fuel in the container 300 is depleted, the fuel injection device can continue to operate by replacing it with another container 300 filled with aviation fuel, thereby improving the fuel injection efficiency of the turnout rotator.
[0054] In some embodiments, refer to Figure 4As shown, the length of container 300 in the vertical direction is less than the length of mounting cavity 120 in the vertical direction. Interface 310 is set on the bottom wall of container 300, and connector 210 is set on the bottom wall of mounting cavity 120. Connector 210 is set vertically upward. There is a space between the outer wall of container 300 and the inner wall of mounting cavity 120. Container 300 can rotate around the vertical axis in mounting cavity 120. The outer wall of connector 210 is provided with external thread. Interface 310 is a round hole. The inner wall of interface 310 is provided with internal thread. The external thread of connector 210 and the internal thread of interface 310 are engaged.
[0055] The interface 310 of the container 300 is threadedly connected to the connector 210 of the oil filling line 200, which helps to improve the sealing performance, prevent the aviation oil in the container 300 from leaking from the interface 310, and the container 300 can be fixed in the mounting cavity 120.
[0056] The container 300 is easy to install and remove. Rotating the container 300 gradually moves it upwards, causing the second one-way valve 320 to return to its original position and seal the interface 310. After moving the container 300 upwards again, the interface 310 is disengaged from the connector 210. Then, the container 300 can be moved horizontally to detach it from the mounting cavity 120. When installing the container 300 in the mounting cavity 120, after offsetting the container 300 and connector 210 vertically, move the container 300 horizontally into the mounting cavity 120 so that the interface 310 and connector 210 are aligned. Then, move the container 300 downwards so that the connector 210 is inserted into the interface 310. Finally, rotate the container 300 to make the connector 210 and interface 310 threadedly engage.
[0057] In some embodiments, refer to Figures 1 to 3 As shown, the outer wall of the container 300 is cylindrical, and multiple anti-slip grooves 360 are provided on the outer wall of the container 300 at intervals along the circumference.
[0058] The anti-slip groove 360° allows the container 300 to be rotated more easily by maintenance personnel, and helps the interface 310 of the container 300 and the threaded engagement of the connector 210 to be tighter.
[0059] In some embodiments, refer to Figure 2 and Figure 4 As shown, a stop 130 is provided at the bottom of the mounting cavity 120. The stop 130 is located on the periphery of the container 300. When the container 300 is installed in the mounting cavity 120 and the connector 210 and the interface 310 are engaged, the stop 130 abuts against the outer wall of the container 300. The length of the container 300 in the vertical direction is less than the distance from the top of the stop 130 to the top wall of the mounting cavity 120, so that the container 300 can be inserted into the mounting cavity 120 from above the stop 130.
[0060] The container 300 is inserted into the mounting cavity 120 from above the stop 130. Then the container 300 moves downward along the side wall of the stop 130 toward the mounting cavity 120. Finally, the interface 310 and the connector 210 cooperate, so that the stop 130 can form a support around the container 300, preventing the container 300 from tilting or falling out of the mounting cavity 120 and causing the interface 310 and connector 210 to loosen.
[0061] In some embodiments, refer to Figure 1 and Figure 4 As shown, the outer wall of container 300 protrudes outside the shell 100.
[0062] The rotation of container 300 is achieved by rubbing the protruding outer wall of container 300.
[0063] In some embodiments, refer to Figures 1 to 4 As shown, the sidewall of container 300 is made of transparent material, and the outer sidewall of container 300 is provided with volume scale so that maintenance personnel can observe the remaining amount of aviation fuel in container 300 and replace container 300 in a timely manner.
[0064] In some embodiments, refer to Figure 4 As shown, the turnout rotator oil injection device also includes a power supply 400 and an oil pump 500.
[0065] Both the power supply 400 and the oil pump 500 are located in the inner cavity 110 of the housing 100. The power supply 400 supplies power to the oil pump 500. The oil pump 500 is connected to the oil filling line 200. After the oil pump 500 is started, it delivers aviation oil from the connector 210 to the oil filling hole 220 in the oil filling line 200.
[0066] The oil pump 500 drives the flow of aviation oil in the oil injection line 200, making the oil injection operation of the oil injection device more convenient.
[0067] In some embodiments, refer to Figure 4 As shown, the turnout rotator oil injection device also includes a handle 600 and a controller 700. The handle 600 is located on the top of the housing 100 and is vertically mounted on the top of the housing 100. The controller 700 is located inside the handle 600, and the button of the controller 700 extends out of the handle 600. The controller 700 is electrically connected to the oil pump 500 and controls the opening and closing of the oil pump 500. The electrical connection wire of the controller 700 is built into the inside of the handle 600 and extends downward into the inner cavity 110 of the housing 100.
[0068] Maintenance personnel operate the oil injection device by holding handle 600. By pressing the button on handle 600, the controller 700 controls the start and stop of the oil pump 500, making the oil injection operation of the oil injection device more convenient.
[0069] This utility model embodiment also provides an oil filling device, which is applied to the turnout rotary oil filling device as described in the above embodiment.
[0070] The turnout rotator oil filling device is equipped with multiple containers 300, at least one container 300 is detachably installed in the mounting cavity 120 of the housing 100, and at least one container 300 is replenished with aviation oil by an oil filling device.
[0071] One container 300 is installed in the mounting cavity 120 of the oiling device. When maintenance personnel use the oiling device to inject aviation oil into the oil tank of the turnout rotator, the top cover 340 of the other container 300 is opened and the oil filling device is used to replenish the aviation oil in the other container 300. When the aviation oil in the container 300 of the oiling device is exhausted, the other container 300 can be replaced and the device can continue to be used without waiting for the container to be replenished with aviation oil, thus improving the oiling efficiency of the turnout rotator.
[0072] The embodiments of the present utility model have been described in detail above with reference to the accompanying drawings. However, the present utility model is not limited to the above embodiments. Within the knowledge possessed by those skilled in the art, various changes can be made without departing from the spirit of the present utility model.
Claims
1. A turnout rotator oil injection device, characterized in that, include: The housing has an internal cavity, and the side wall of the housing is recessed inward to form an installation cavity; An oil filling pipeline is provided in the inner cavity. The oil filling pipeline is provided with a connector and an oil filling hole. The connector is located in the mounting cavity, and the oil filling hole is located at the bottom of the housing. The liquid in the oil filling pipeline is delivered from the connector to the oil filling hole. The container has an interface at the bottom, and a first one-way valve is provided inside the interface. The liquid inside the container squeezes the first one-way valve to move outward, causing the first one-way valve to close the interface. The top of the container has an opening and a top cover that can be detachably sealed to the opening. The top cover has a second one-way valve, which allows the liquid to flow from the outside to the inside of the container. The container is detachably installed in the mounting cavity. The connector is inserted into the interface and pushes the first one-way valve to move into the interior of the container, so that the container is connected to the oil injection pipeline.
2. The turnout rotator oil injection device according to claim 1, characterized in that, The length of the mounting cavity in the vertical direction is greater than that of the container in the vertical direction. The connector is located on the bottom wall of the mounting cavity, and the interface is located on the bottom wall of the container. The container is rotatably disposed in the mounting cavity. The inner side wall of the interface is provided with an internal thread, and the outer side wall of the connector is provided with an external thread. The internal thread and the external thread are engaged.
3. The turnout rotator oil injection device according to claim 2, characterized in that, The container is cylindrical, and multiple anti-slip grooves are provided on the outer side wall of the container, with the multiple anti-slip grooves distributed at intervals along the circumference of the container.
4. The turnout rotator oil injection device according to claim 2, characterized in that, A stop block is provided on the periphery of the bottom of the mounting cavity. The distance from the top of the stop block to the top wall of the mounting cavity is greater than the length of the container in the vertical direction. The stop block abuts against the outer wall of the container.
5. The turnout rotator oil injection device according to claim 2, characterized in that, The outer wall of the container protrudes outside the shell.
6. The turnout rotator oil injection device according to claim 1, characterized in that, The turnout rotator oil injection device also includes: The power supply is located within the cavity. An oil pump is installed in the oil injection pipeline. The oil pump is electrically connected to the power supply. Starting the oil pump causes the liquid in the oil injection pipeline to be transported from the joint to the oil injection hole.
7. The turnout rotator oil injection device according to claim 6, characterized in that, The top of the housing is provided with a vertically arranged handle, and the turnout rotator oil injection device further includes: A controller is located on the handle and is electrically connected to the oil pump. The controller controls the start and stop of the oil pump.
8. The turnout rotator oil injection device according to claim 1, characterized in that, The container has transparent sidewalls, and the outer sidewalls of the container are provided with volume markings.
9. The turnout rotator oil injection device according to claim 1, characterized in that, The oil injection pipeline also includes: A liquid inlet check valve is provided at the joint, and the liquid inlet check valve allows the oil injection pipeline to be opened from the outside to the inside of the oil injection pipeline. A liquid outlet check valve is provided at the oil injection hole, and the liquid outlet check valve is open from the inside to the outside of the oil injection pipeline; A piston cylinder, with both ends connected to the connector and the oil injection port, respectively; The piston is movably disposed within the piston cylinder; A piston rod is connected to the piston. The housing has a through-hole. The piston rod extends out of the housing through the through-hole. The piston rod moves along the through-hole to move the piston along the piston cylinder.
10. An oil-filling device, characterized in that, An oil filling device for a turnout rotator as described in any one of claims 1 to 9, wherein there are at least two containers, one of which is detachably disposed in the mounting cavity, and the oil filling device replenishes aviation oil to the other container.