Electromagnetic release for aircraft simulator

By using the design of plastic shell, moving iron core, tie rod and magnetic flux mechanism in the aircraft simulator, the switch is connected or disconnected by pressing/separating the limit switch and sleeve, the complex structure of the circuit breaker device for existing aircraft simulators is solved, simplifying the equipment structure and reducing costs.

CN223092807UActive Publication Date: 2025-07-11ADVENTURER INTELLIGENT TECH (SHANGHAI) CO LTD
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Patent Information

Application Number
CN202421128185.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-22
Publication Date
2025-07-11
Estimated Expiration
2034-05-22

AI Technical Summary

Technical Problem

The circuit breaker used in existing aircraft simulators has a complex structure and high production cost.

Method used

It adopts a plastic shell, moving iron core, tie rod and magnetic flux mechanism design, and the switch is connected or disconnected by pressing/separating the limit switch and sleeve, eliminating contacts, springs, isolation rings and other components.

Benefits of technology

Simplify the equipment structure, reduce the number of components, improve the applicability and flexibility of the equipment, and reduce production costs.

✦ Generated by Eureka AI based on patent content.

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    Figure CN223092807U_ABST
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Abstract

The utility model discloses an electromagnetic release for an aircraft simulator. The electromagnetic release comprises a plastic shell, a movable iron core, a magnetic flux mechanism and the like, the movable iron core is sleeved with a main spring. One end of the movable iron core and one end of the pull rod are mutually fixed, the fixed position of the movable iron core and the pull rod is located in the magnetic flux mechanism, one end of the movable iron core is arranged in the button reset mechanism, the other end of the pull rod is fixedly connected into the sleeve, and a secondary spring is fixedly installed between the bottom of the sleeve and the plastic shell; limiting switches are fixedly installed in the plastic shell and located on the two sides of the sleeve, and switch buttons are arranged on the tops of the limiting switches. When the sleeve is in a pressed state, the sleeve can be in contact with the switch button, and the switch button is pressed; when the sleeve rebounds, the sleeve and the switch button are in a separated state. According to the utility model, the signal copper sheet can be switched on by manually pressing the button, and the signal copper sheet can be switched off by manually pulling out the button or electrifying, so that compared with the existing design, the structure is simpler, and more functions can be realized.
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Description

Technical Field

[0001] The utility model relates to the technical field of aircraft simulator analog open circuit technology, and particularly relates to an electromagnetic release for an aircraft simulator. Background Technique

[0002] An aircraft simulator is a highly precise flight training device that can simulate the flight environment and operations of a real aircraft, providing pilots with an almost real flight experience. This device plays a crucial role in pilot training, aircraft R & D, flight performance testing, and flight accident investigation, and provides pilots with a test and training device with similar operating loads, vision, hearing, and kinesthetic sensations; the open circuit device in the aircraft simulator is an important component.

[0003] The previously publicly disclosed Chinese authorized patent CN219534392U, an open circuit device for an aircraft simulator, includes a magnetic flux mechanism, a moving iron core, and a pull rod. One end of the moving iron core and the pull rod are fixedly connected to each other, and the connection point is located inside the magnetic flux mechanism; the other end of the moving iron core is connected to a button reset mechanism, and the other end of the pull rod is connected to a wiring mechanism. Through the above scheme, the utility model achieves the purpose of a compact overall product structure and reasonable layout. Although this patent solves the problems in the prior art that the existing open circuit device for an aircraft simulator has a complex structure and extremely high production costs, the structure of the above device is still complex, so the existing device needs to be further improved. Content of the Utility Model

[0004] Aiming at the deficiencies of the prior art, the utility model provides an electromagnetic release for an aircraft simulator to solve the problem of the complex structure of the existing open circuit device for an aircraft simulator.

[0005] To solve the above problems, the utility model provides the following technical scheme: an electromagnetic release for an aircraft simulator, including a plastic shell, a moving iron core, a pull rod, and a magnetic flux mechanism; a main spring is sleeved on the moving iron core; one end of the moving iron core and the pull rod are fixedly connected to each other, and the connection point is located inside the magnetic flux mechanism. One end of the moving iron core is placed inside the button reset mechanism, and the other end of the pull rod is fixedly connected inside a sleeve. A secondary spring is fixedly installed between the bottom of the sleeve and the plastic shell; limit switches are fixedly installed on both sides of the sleeve inside the plastic shell, and a switch button is arranged on the top of the limit switch; when the sleeve is in a pressed state, the sleeve can contact and press the switch button; when the sleeve rebounds, the sleeve is in a separated state from the switch button.

[0006] Preferably: two connecting pressure pieces are symmetrically arranged at one end of the sleeve; the sleeve presses and opens or separates and closes the switch button through the two connecting pressure pieces.

[0007] Preferably, there are three pins provided on the limit switch.

[0008] Preferably, for the two wires coming out of the magnetic flux coil in the magnetic flux mechanism, one is directly connected to the copper sheet, and the other is connected to another connecting copper sheet through the limit switch; the limit switch is respectively connected to the signal copper sheet I and the signal copper sheet II.

[0009] Preferably, the button reset mechanism includes a button upper cover and a button lower cover which are connected to each other.

[0010] Compared with the prior art, the technical solution of this application has the following beneficial effects:

[0011] 1. From a structural perspective, in this utility model, the other end of the pull rod is fixedly connected inside the sleeve, and limit switches are fixedly installed on both sides of the sleeve inside the plastic housing. The switch button at the top of the limit switch realizes the connection or disconnection of the switch through the pressing / separation of the sleeve; compared with the existing structure, it omits components such as contacts, spring pieces, isolation rings, and spring mounting seats, thus reducing the addition of components and making the structure of the entire device simpler.

[0012] 2. From a functional perspective, this utility model can achieve the following functions: the button can be manually pressed (the signal copper sheet is conducted); the button can be manually pulled out (the signal copper sheet is disconnected); it can pop out when powered on. It can be flexibly adjusted according to the actual situation, and the applicability of this utility model is strong. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 is a schematic structural diagram of this utility model;

[0014] Figure 2 is of this utility model Figure 1 the schematic cross-sectional structure diagram of A-A in;

[0015] Figure 3 is of this utility model Figure 1 structural sectional view;

[0016] Figure 4 is a three-dimensional view of the limit switch structure of this utility model;

[0017] Figure 5 is a three-dimensional view of the sleeve structure of this utility model.

[0018] In the figure: 1 plastic housing, 2 moving iron core, 3 pull rod, 4 main spring, 5 sleeve, 6 secondary spring, 7 limit switch, 71 switch button, 8 signal copper sheet I, 9 signal copper sheet II, 10 button upper cover, 11 button lower cover, 101 U-shaped frame, 102 magnet, 103 magnetic flux coil, 104 magnetic flux skeleton, 105 magnetic flux cover plate. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0019] The technical solutions in the embodiments of the present utility model will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0020] As Figures 1 to 5 shown, an electromagnetic release for an aircraft simulator of the present utility model includes a plastic shell 1, a moving iron core 2, a pull rod 3, and a magnetic flux mechanism; the magnetic flux mechanism in the present utility model is the same as that in the background art, and is also composed of components such as a U-shaped frame 101, a magnet 102, a magnetic flux coil 103, a magnetic flux skeleton 104, and a magnetic flux cover plate 105. Its principle is also the same as that in the background art, that is, an electromagnet with a coil and a magnet inside. When the coil is energized, the magnetic force generated plus the elastic force of the spring is greater than the suction force of the magnet, and the button part will pop out. Consistent with the original patent, a main spring 4 is sleeved on the moving iron core 2 of the present utility model; one end of the moving iron core 2 and the pull rod 3 are fixedly connected to each other, and the fixed part of the two is located inside the magnetic flux mechanism. One end of the moving iron core 2 is placed inside the button reset mechanism. Different from the original patent, the button reset mechanism includes a button upper cover 10 and a button lower cover 11 that are connected to each other, omitting components such as a button spring and a button pin. The other end of the pull rod 3 of the present utility model is fixedly connected to a sleeve 5, and a secondary spring 6 is fixedly installed between the bottom of the sleeve 5 and the plastic shell 1; limit switches 7 are fixedly installed inside the plastic shell 1 and on both sides of the sleeve 5, and a switch button 71 is provided on the top of the limit switch 7; when the sleeve 5 is in a pressed state, the sleeve 5 can contact and press the switch button 71; when the sleeve 5 rebounds, the sleeve 5 is in a separated state from the switch button 71.

[0021] As Figure 4 shown: Two connecting pressure pieces 51 are symmetrically provided at one end of the sleeve 5 of the present utility model; the sleeve 5 presses the switch button 71 to open or separates and closes it through the two connecting pressure pieces 51. As Figure 5 shown, three pins are provided on the limit switch 7 of the present utility model. Two wires coming out of the magnetic flux coil inside the magnetic flux mechanism, one is directly connected to a copper sheet, and the other is connected to another copper sheet through the limit switch 7; the limit switch 7 is respectively connected to a signal copper sheet I 8 and a signal copper sheet II 9, that is, the limit switch 7 on the left side of the pull rod 3 is connected to the signal copper sheet I 8, and the limit switch 7 on the right side of the pull rod 3 is connected to the signal copper sheet II 9.

[0022] The functions that the present utility model can achieve are: 1. The button can be manually pressed to conduct the signal copper sheet; 2. The button can be manually pulled out to disconnect the signal copper sheet; 3. It can be ejected by power on; the working principle to achieve the above is:

[0023] 1. The signal copper sheet can be conducted by manually pressing the button: When it is not powered on, manually press the upper button cover 10. While the upper button cover 10 drives the moving iron core 2, the pull rod 3 and the sleeve 5 to move downward, the main spring 4 and the secondary spring 6 are compressed until the moving iron core 2 is attracted by the magnet 102. At this time, the connecting tab 51 of the sleeve 5 contacts the switch button 71 of the limit switch 7, and the switch button 71 of the limit switch 7 is in a pressed state, so that the signal copper sheet is conducted;

[0024] 2. The signal copper sheet of the button can be disconnected by manually pulling it out: Select to manually pull the upper button cover 10 upward. When the applied force is greater than the adsorption force of the magnet 102, the sleeve 5 can also be driven to release the switch button 71 of the limit switch 7, resulting in power off.

[0025] 3. It can pop out when powered on: When the main spring 4 is compressed (at this time, the two connecting tabs 51 of the sleeve 5 press the switch button 71 of the limit switch 7), apply 24V or 28V power to it, and the whole composed of the upper button cover 10, the lower button cover 11, the moving iron core 2, and the pull rod 3 will pop out. Under the action of the secondary spring 6, the sleeve 5 will also move forward, so that the switch button 71 of the limit switch 7 is released, and all things are powered off.

[0026] In addition, the limit switch 7 is connected to the signal copper sheet I 8 and the signal copper sheet II 9. When the sleeve 5 pops out, the electrical signals of the signal copper sheet I 8 and the signal copper sheet II 9 are disconnected, and vice versa. In the case of all disconnections, press the button, the pull rod 3 pushes the sleeve 5, the secondary spring 6 is compressed, the sleeve 5 squeezes the switch button 71 of the limit switch 7, and the circuit (two wiring copper sheets) and the electrical signal (two signal copper sheets) are both conducted. Finally, it should be noted that the limit switch of the present utility model has three pins, one is normally open, and the other is normally closed. As long as the pin for feedback electrical signal (connecting the signal copper sheet and the limit switch) is changed, the electrical signal can be reversed, that is, in the popped state, the electrical signal is conducted, and when pressed, it is disconnected.

[0027] It should be noted that in this text, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprising", "including" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device comprising a series of elements not only includes those elements, but also includes other elements not expressly listed, or further includes elements inherent to such process, method, article or device. Without further limitation, an element defined by the statement "comprising an..." does not exclude the existence of additional identical elements in the process, method, article or device comprising the said element.

[0028] Although the embodiments of the present invention have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An electromagnetic release for an aircraft simulator, comprising a plastic housing (1), a moving iron core (2), a pull rod (3) and a magnetic flux mechanism; a main spring (4) is sleeved on the moving iron core (2); one end of the moving iron core (2) and the pull rod (3) are fixedly connected to each other, and the connection position is located within the magnetic flux mechanism, and one end of the moving iron core (2) is placed within a button reset mechanism, characterized in that: The other end of the pull rod (3) is fixedly connected inside the sleeve (5), and a secondary spring (6) is fixedly installed between the bottom of the sleeve (5) and the plastic housing (1); inside the plastic housing (1) and on both sides of the sleeve (5), limit switches (7) are fixedly installed, and a switch button (71) is arranged on the top of the limit switch (7); when the sleeve (5) is in a pressed state, the sleeve (5) can contact the switch button (71) and press the switch button (71); when the sleeve (5) rebounds, the sleeve (5) is in a separated state from the switch button (71).

2. The electromagnetic release for aircraft simulators according to claim 1, wherein: Two connecting pressure plates (51) are symmetrically arranged at one end of the sleeve (5); the sleeve (5) presses the switch button (71) to turn it on or separates and closes it through the two connecting pressure plates (51).

3. The electromagnetic release for aircraft simulators according to claim 1, wherein: The limit switch (7) is provided with three pins.

4. The electromagnetic release for aircraft simulator according to claim 3, characterized in that: For the two wires coming out of the magnetic flux coil in the magnetic flux mechanism, one is directly connected to the copper sheet, and the other is connected to another connecting copper sheet through the limit switch (7); the limit switch (7) is respectively connected to the signal copper sheet I (8) and the signal copper sheet II (9).

5. The electromagnetic release for aircraft simulators according to any one of claims 1 to 4, characterized in that: The button reset mechanism includes a button upper cover (10) and a button lower cover (11) which are connected to each other.

Citation Information

Patent Citations

  • Circuit breaking device for aircraft simulator

    CN219534392U