Remote magnetic control switch
Through magnetic control of magnetic steel combination and dry spring combination, the problem of wear of mechanical components of remote magnetron switches is solved, and high reliability and low resistance switches are achieved, excessive refueling accidents are avoided, and suitable for high-frequency and flammable environment.
Patent Information
- Application Number
- CN202421198304.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-29
- Publication Date
- 2025-01-07
- Estimated Expiration
- 2034-05-29
AI Technical Summary
Existing remote magnetron switch mechanical components are prone to wear, loose contact points, damage or oxidation, which reduces trigger sensitivity and electrical connection quality, affects the reliability and life of the switch, and is prone to excessive refueling accidents.
Using a combination of magnetic steel and a dry spring combination combining spring and pressure plate, the magnetic control switch avoids wear and oxidation problems of traditional contactors, and long-distance control is achieved using a combination of spiral wires and aerospace plugs.
Improves the accuracy and reliability of the switch, extends life, ensures fast response time and low contact resistance, is suitable for high-frequency and high-speed operations, avoids excessive refueling accidents, and is suitable for explosion-proof and flammable environments.
Smart Images

Figure CN222320091U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to a remote magnetically controlled switch and belongs to the field of remote control. Background Art
[0002] The remote magnetic control switch of the aircraft refueling truck is a switch device used for remote control of the refueling truck. It uses magnetic control technology to achieve remote control of the start and stop of refueling, as well as unmanned flow cut-off protection, and other equipment configurations to ensure that the pressure at the end of the hose at the aircraft tank port does not exceed the standard, providing a more convenient and safe refueling operation. The bottom of the remote magnetic control switch of the aircraft refueling truck is fixedly connected to a spiral wire. By utilizing the retractability of the spiral wire, the staff can hold the remote magnetic control switch and pull the spiral wire to patrol around the refueling truck while the refueling truck is refueling the aircraft. The existing remote magnetic control switches are mostly button-type. In long-term use, the mechanical parts of the existing conventional magnetic control switches are very easy to wear, and the contact points will be loose, damaged, worn or oxidized, which reduces the trigger sensitivity and the quality of the electrical connection, thereby affecting the reliability and life of the switch, and it is easy to cause over-refueling accidents.
[0003] Therefore, it is urgent to propose a new type of remote magnetically controlled switch to solve the above technical problems. Utility Model Content
[0004] The purpose of the research and development of this utility model is to solve the problems that the mechanical parts of the existing remote magnetic control are very easy to wear, the contact points are loose, damaged, worn or oxidized, and the trigger sensitivity and electrical connection quality are reduced, thereby affecting the reliability and life of the switch, and the problem of over-refueling accidents is prone to occur. A brief overview of the utility model is given below to provide a basic understanding of certain aspects of the utility model. It should be understood that this overview is not an exhaustive overview of the utility model. It is not intended to determine the key or important parts of the utility model, nor is it intended to limit the scope of the utility model.
[0005] The technical solution of this utility model:
[0006] A remote magnetically controlled switch comprises a handle body, a pressure plate, a spring, a pressure rod, a magnetic steel combination, a reed combination, a spiral wire combination and an aviation plug combination. One side of the pressure plate is rotatably connected to the handle body through a rotating shaft. A sliding groove is provided on the handle body. The spring is arranged in the sliding groove, and one end of the spring is fixedly connected to the bottom of the sliding groove, the other end of the spring is fixedly connected to the pressure rod, the top of the pressure rod is in contact with the inner wall of the pressure plate, a magnetic steel combination is fixedly installed on the other side of the pressure plate, a reed combination is built into the handle body, one end of the spiral wire combination is fixedly connected to the handle body, and at the same time penetrates into the handle body to be electrically connected to the reed combination, and the other end of the spiral wire combination is fixedly connected to the aviation plug combination.
[0007] Preferably, the magnetic steel combination comprises a magnetic steel sheet and a magnetic steel frame, and the magnetic steel sheet is fixedly mounted on the inner wall of the pressure plate on the side away from the rotating shaft through the magnetic steel frame.
[0008] Preferably: the spiral wire combination includes a wire outlet nozzle, a cable protective sleeve, a spiral wire, a terminal block and a sealing ring, one side of the wire outlet nozzle is threadedly connected to the end of the handle body, and a sealing ring is arranged between the wire outlet nozzle and the handle body, the other side of the wire outlet nozzle is fixedly installed with a cable protective sleeve, and the inside of the handle body is fixedly installed with a terminal block, the end of the spiral wire passes through the cable protective sleeve and the wire outlet nozzle and enters the inside of the handle body, and is fixedly connected to the terminal block, and the spiral wire is electrically connected to the reed combination through the terminal block.
[0009] Preferably: the aviation plug combination includes a detachable plug and socket, the plug includes a small lock nut, a plug sleeve, a retaining ring, a first cover plate, a plug frame, a pin and a large lock nut, one side of the plug sleeve is fixedly connected to the spiral wire through the small lock nut, the end of the spiral wire is inserted into the plug sleeve and fixedly connected to the retaining ring, a large lock nut is installed on the other side of the plug sleeve, a plug frame is fixedly installed in the plug sleeve, a first cover plate is fixedly installed on one side of the plug frame, a pin is fixedly installed on the other side of the plug frame, and the spiral wire is electrically connected to the pin.
[0010] Preferably: the socket comprises a socket sleeve, a conductive tube assembly, a second cover plate, a socket frame and a rubber pad, the socket frame is fixedly installed in the socket sleeve, the conductive tube assembly is installed on one side of the socket frame, and the second cover plate is installed on the other side of the socket frame, the pin is inserted in the conductive tube assembly, the socket sleeve is inserted in the large lock nut, and a rubber pad is arranged between the plug frame and the socket frame.
[0011] Preferably, an O-ring is provided between the inner wall of the small lock nut and the outer wall of the spiral wire.
[0012] Preferably, an arc-shaped slider is arranged on the top of the pressure rod.
[0013] The utility model has the following beneficial effects:
[0014] 1. The utility model combines springs and pressure plates, and cleverly utilizes the magnetic control switch of the magnetic steel combination and the reed combination, which has very high precision and reliability. Because its operation does not rely on traditional contactors, there is no contact wear and oxidation problem, so it has a long life and is reliable. At the same time, it has a fast switching speed and a short response time. It is suitable for high-frequency and high-speed operations, and avoids the phenomenon of over-fueling accidents;
[0015] 2. The contact resistance between the magnetic steel combination and the reed combination of the utility model is very low, ensuring good electrical connection and signal transmission, and no sparks will be generated during the switching process because there is no collision and separation of the contactor, which is suitable for explosion-proof and flammable environments such as aircraft refueling;
[0016] 3. The utility model is light and flexible, small in size, light in weight, resistant to pulling, stable on and off, and has a long switch life; the spiral wire has good resilience and is wear-resistant, and the aviation plug combination can also be configured according to different user requirements, with strong flexibility. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 It is a schematic diagram of the structure of a remote magnetically controlled switch;
[0018] Figure 2 It is a schematic diagram of the structure of the handle body;
[0019] Figure 3 It is a structural diagram of the aviation plug assembly;
[0020] Figure 4 It is a schematic diagram of the structure of the plug;
[0021] Figure 5 It is a schematic diagram of the structure of the socket;
[0022] Figure 6 is a side view of the pressure plate.
[0023] In the figure: 1-handle body, 2-pressure plate, 3-spring, 4-pressure rod, 5-magnetic steel combination, 6-reed combination, 7-spiral wire combination, 8-aviation plug combination, 9-rotating shaft, 10-slideway, 41-arc slider, 51-magnetic steel sheet, 52-magnetic steel frame, 71-outlet nozzle, 72-cable protective sleeve, 73-spiral wire, 74-terminal seat, 75-sealing ring, 81-plug, 82-socket, 811-small lock nut, 812-plug cover, 813-blocking ring, 814-first cover plate, 815-plug frame, 816-pin, 817-large lock nut, 821-socket cover, 822-conductive tube combination, 823-second cover plate, 824-socket frame, 825-rubber pad. DETAILED DESCRIPTION
[0024] In order to make the purpose, technical solution and advantages of the utility model clearer, the utility model is described below by specific embodiments shown in the accompanying drawings. However, it should be understood that these descriptions are only exemplary and are not intended to limit the scope of the utility model. In addition, in the following description, the description of well-known structures and technologies is omitted to avoid unnecessary confusion of the concept of the utility model.
[0025] The connection mentioned in the present invention is divided into fixed connection and detachable connection. The fixed connection is a non-detachable connection, including but not limited to conventional fixed connection methods such as folding connection, rivet connection, bonding connection and welding connection. The detachable connection includes but is not limited to conventional detachable methods such as threaded connection, snap connection, pin connection and hinge connection. When the specific connection method is not clearly defined, it is assumed that at least one connection method can always be found in the existing connection methods to achieve the function. Those skilled in the art can choose according to their needs. For example: choose welding connection for fixed connection and hinge connection for detachable connection.
[0026] Specific implementation method 1: Combination Figure 1-Figure 6 The present embodiment is described. The remote magnetically controlled switch of the present embodiment comprises a handle body 1, a pressure plate 2, a spring 3, a pressure rod 4, a magnetic steel combination 5, a reed combination 6, a spiral wire combination 7 and an aviation plug combination 8. One side of the pressure plate 2 is rotatably connected to the handle body 1 through a rotating shaft 9. A slide groove 10 is provided on the handle body 1. The spring 3 is arranged in the slide groove 10, and one end of the spring 3 is fixedly connected to the bottom of the slide groove 10, the other end of the spring 3 is fixedly connected to the pressure rod 4, the top of the pressure rod 4 is in contact with the inner wall of the pressure plate 2, the other side of the pressure plate 2 is fixedly installed with a magnetic steel combination 5, the handle body 1 has a built-in reed combination 6, one end of the spiral wire combination 7 is fixedly connected to the handle body 1, and at the same time penetrates into the handle body 1 to be electrically connected to the reed combination 6, and the other end of the spiral wire combination 7 is fixedly connected to the aviation plug combination 8.
[0027] The handle body 1 is a cylindrical handle body, the pressure plate 2 is an arc-shaped pressure plate, and the two sides of the arc-shaped pressure plate are rotatably hinged with the cylindrical handle body through a rotating shaft 9. A raised shift plate is processed on the top of the arc-shaped pressure plate close to the hinged rotating shaft 9 to limit the flipping angle of the pressure plate. The cylindrical handle body is also processed with a groove for accommodating a magnetic steel combination 5, and a reed combination 6 is embedded in the handle body directly below the recess, in order to shorten the distance between the magnetic steel combination 5 and the reed combination 6 and reduce the shielding thickness, thereby improving sensitivity.
[0028] The slide groove 10 is inclined, and the sliding direction of the slide groove 10 tends to be perpendicular to the pressing plate 2 .
[0029] The magnetic steel assembly 5 includes a magnetic steel sheet 51 and a magnetic steel frame 52 . The magnetic steel sheet 51 is fixedly mounted on the inner wall of the pressing plate 2 away from the rotating shaft 9 via the magnetic steel frame 52 .
[0030] The reed assembly 6 is triggered by the magnetic steel assembly 5. The reed assembly 6 has a switch function, but uses a magnetic steel sheet 51 made of magnetic material as a mechanism to trigger the switch. The reed assembly 6 is usually composed of two metal reeds, one of which is fixed in an insulating sleeve of magnetic material, called a reed, and the other is a magnetic material, called a trigger magnet or a magnetic nail. When the trigger magnetic steel sheet 51 approaches the reed inside the reed assembly 6, the reed will bend due to the action of the magnetic force, turning on the switch. When the trigger magnet leaves the reed, the reed rebounds and turns off the switch.
[0031] The spiral wire combination 7 includes a wire outlet nozzle 71, a cable protective sleeve 72, a spiral wire 73, a terminal block 74 and a sealing ring 75. One side of the wire outlet nozzle 71 is threadedly connected to the end of the handle body 1, and a sealing ring 75 is arranged between the wire outlet nozzle 71 and the handle body 1. The cable protective sleeve 72 is fixedly installed on the other side of the wire outlet nozzle 71, and the terminal block 74 is fixedly installed inside the handle body 1. The end of the spiral wire 73 passes through the cable protective sleeve 72 and the wire outlet nozzle 71 and then enters the handle body 1, and is fixedly connected to the terminal block 74. At the same time, the spiral wire 73 is electrically connected to the reed combination 6 through the terminal block 74.
[0032] The cable protection cover 72 is clamped at the outlet of the outlet nozzle 71 and is fixedly connected thereto via a top screw.
[0033] The aviation plug combination 8 includes a detachable plug 81 and a socket 82, and the plug includes a small lock nut 811, a plug sleeve 812, a retaining ring 813, a first cover plate 814, a plug frame 815, a pin 816 and a large lock nut 817. One side of the plug sleeve 812 is fixedly connected to the spiral wire 73 through the small lock nut 811, and the end of the spiral wire 73 is inserted into the plug sleeve 812 and fixedly connected to the retaining ring 813. A large lock nut 817 is installed on the other side of the plug sleeve 812, and a plug frame 815 is fixedly installed in the plug sleeve 812. The first cover plate 814 is fixedly installed on one side of the plug frame 815, and the pin 816 is fixedly installed on the other side of the plug frame 815. The spiral wire 73 is electrically connected to the pin 816.
[0034] The socket 82 includes a socket sleeve 821, a conductive tube assembly 822, a second cover plate 823, a socket frame 824 and a rubber pad 825. The socket frame 824 is fixedly installed in the socket sleeve 821, the conductive tube assembly 822 is installed on one side of the socket frame 824, and the second cover plate 823 is installed on the other side of the socket frame 824. When the plug pin 816 is inserted into the conductive tube assembly 822, the circuit is connected. The socket sleeve 821 is inserted into the large lock nut 817 for positioning. The rubber pad 825 is arranged between the plug frame 815 and the socket frame 824. An O-ring is arranged between the inner wall of the small lock nut 811 and the outer wall of the spiral wire 73.
[0035] An arc-shaped slider 41 is provided on the top of the pressing rod 4 to reduce the sliding resistance of the contact between the pressing rod 4 and the pressing plate 2 .
[0036] When in use, the socket 82 is prefabricated and installed on the refueling vehicle, and the plug 81 and the socket 82 are plugged and connected. The operator holds the handle body 1. When the switch needs to be controlled, the pressure plate 2 is manually pressed to tilt one end. Under the action of force, the pressure plate 2 is turned downward with the rotating shaft as the rotation center. While turning, the pressure rod 4 is pressed, and the spring 3 is squeezed and contracted. The magnetic steel combination 5 on the pressure plate 2 is close to the reed combination 6, and the reed combination 6 is triggered. The triggered switch signal is transmitted to the magnetic control refueling program controller of the refueling vehicle through the spiral wire combination 7 and the aviation plug combination 8, so as to realize the remote control of refueling and unmanned flow interruption protection, and other equipment configurations are used to ensure that the pressure at the end of the hose at the aircraft fuel tank port does not exceed the standard. When the hand is released, the spring 3 resets and rebounds, driving the pressure plate 2 to turn upward with the rotating shaft as the rotation center. While turning, the magnetic steel combination 5 on the pressure plate 2 is in line with the reed combination 6, and the reed combination 6 is closed.
[0037] It should be noted that in the above embodiments, as long as the technical solutions are not contradictory, they can be arranged and combined, and those skilled in the art can exhaust all possibilities based on the mathematical knowledge of arrangement and combination. Therefore, the present utility model will no longer describe the technical solutions after arrangement and combination one by one, but it should be understood that the technical solutions after arrangement and combination have been disclosed by the present utility model.
[0038] The above description is only the preferred embodiment of the utility model, and is not intended to limit the utility model. For those skilled in the art, the utility model can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.
Claims
1. Remote magnetic switch, characterized by: The utility model comprises a handle body (1), a pressure plate (2), a spring (3), a pressure rod (4), a magnetic steel assembly (5), a dry reed assembly (6), a spiral wire assembly (7) and an aviation plug assembly (8). One side of the pressure plate (2) is rotatably connected to the handle body (1) through a rotating shaft (9). A sliding groove (10) is provided on the handle body (1). The spring (3) is arranged in the sliding groove (10). One end of the spring (3) is fixedly connected to the bottom of the sliding groove (10). The other end of the spring (3) is fixedly connected to the pressure rod (4). The top of the pressure rod (4) is in contact with the inner wall of the pressure plate (2). The other side of the pressure plate (2) is fixedly installed with a magnetic steel assembly (5). The handle body (1) is internally provided with a dry reed assembly (6). One end of the spiral wire assembly (7) is fixedly connected to the handle body (1) and simultaneously penetrates into the handle body (1) to be electrically connected to the dry reed assembly (6). The other end of the spiral wire assembly (7) is fixedly connected to the aviation plug assembly (8).
2. The remote magnetically controlled switch according to claim 1, characterized in that: The magnetic steel assembly (5) comprises a magnetic steel sheet (51) and a magnetic steel frame (52), and the magnetic steel sheet (51) is fixedly mounted on the inner wall of the pressing plate (2) on a side away from the rotating shaft (9) via the magnetic steel frame (52).
3. The remote magnetically controlled switch according to claim 2, characterized in that: The spiral wire assembly (7) comprises a wire outlet nozzle (71), a cable protective sleeve (72), a spiral wire (73), a terminal block (74) and a sealing ring (75); one side of the wire outlet nozzle (71) is threadedly connected to the end of the handle body (1), and a sealing ring (75) is provided between the wire outlet nozzle (71) and the handle body (1); the other side of the wire outlet nozzle (71) is fixedly installed with a cable protective sleeve (72); the handle body (1) is fixedly installed with a terminal block (74); the end of the spiral wire (73) passes through the cable protective sleeve (72) and the wire outlet nozzle (71) and then enters the handle body (1) and is fixedly connected to the terminal block (74); and the spiral wire (73) is electrically connected to the reed assembly (6) through the terminal block (74).
4. The remote magnetically controlled switch according to claim 3, characterized in that: The aviation plug assembly (8) comprises a detachable plug (81) and a socket (82), wherein the plug comprises a small lock nut (811), a plug sleeve (812), a retaining ring (813), a first cover plate (814), a plug frame (815), a plug pin (816) and a large lock nut (817); one side of the plug sleeve (812) is fixedly connected to the spiral wire (73) through the small lock nut (811); the end of the spiral wire (73) is inserted into the plug sleeve (812) and fixedly connected to the retaining ring (813); the other side of the plug sleeve (812) is provided with a large lock nut (817); the plug frame (815) is fixedly installed in the plug sleeve (812); the first cover plate (814) is fixedly installed on one side of the plug frame (815); the plug pin (816) is fixedly installed on the other side of the plug frame (815); and the spiral wire (73) is electrically connected to the plug pin (816).
5. The remote magnetically controlled switch according to claim 4, characterized in that: The socket (82) comprises a socket sleeve (821), a conductive tube assembly (822), a second cover plate (823), a socket frame (824) and a rubber pad (825); the socket sleeve (821) is fixedly mounted with the socket frame (824); the conductive tube assembly (822) is mounted on one side of the socket frame (824); the second cover plate (823) is mounted on the other side of the socket frame (824); the plug pin (816) is inserted into the conductive tube assembly (822); the socket sleeve (821) is inserted into the large lock nut (817); and a rubber pad (825) is arranged between the plug frame (815) and the socket frame (824).
6. The remote magnetically controlled switch according to claim 5, characterized in that: An O-type sealing ring is provided between the inner wall of the small lock nut (811) and the outer wall of the spiral wire (73).
7. The remote magnetically controlled switch according to claim 6, characterized in that: The top of the pressure rod (4) is provided with an arc-shaped slider (41).