Quick release instrument module mounting rack structure for aircraft mockup cockpit

Abstract

The utility model discloses a quick detachable instrument module mounting rack structure for aircraft simulation cabin, electromagnet utilizes electromagnetic attraction, adsorbs metal block to fix electronic instrument panel main part, provides stable holding force for module, and power button controls the circuit on-off between battery and electromagnet, is the control component of operator active trigger electromagnet power supply or power off, realizes manual intervention to module fixed state, utilizes the magnetic force of electromagnet energization, through metal block adsorption electronic instrument panel main part, provides stable and reliable fixing force, lets instrument module run in simulation cabin, when needing to detach instrument module, control electromagnet power off, and magnetic force disappears, makes electronic instrument panel main part and installation groove stable separation, provides trigger condition for module dismounting, through the component of the device installation utilizes electromagnet characteristics to fix electronic instrument panel, fixes and unlocks instrument panel quickly, reduces dismounting time, improves overall operation and maintenance efficiency.

Description

Technical Field

[0001] This utility model relates to the field of aircraft simulator cockpit technology, specifically to a quick-release instrument module mounting rack structure for aircraft simulator cockpits. Background Technology

[0002] The quick-release instrument module mounting structure for aircraft simulator cockpits has several significant advantages. Aircraft simulator cockpits are devices that highly replicate the environment of a real aircraft cockpit or cabin, reproducing the flight status and environment of an aircraft and creating a near-real flight experience for users. The quick-release instrument module mounting structure is a dedicated mounting structure designed for instrument modules in aircraft simulator cockpits, which facilitates the removal of instrument panels by staff.

[0003] However, the device lacks components that utilize the properties of electromagnets to secure the electronic instrument panel, making it impossible to quickly fix and unlock the panel. This increases disassembly time and reduces overall maintenance efficiency. Utility Model Content

[0004] The purpose of this invention is to provide a quick-release instrument module mounting bracket structure for aircraft simulator cockpits, in order to solve the problems mentioned in the background art.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a quick-release instrument module mounting frame structure for an aircraft simulator cockpit, including a flight simulator cockpit. The outer surface of the flight simulator cockpit has multiple mounting slots, and multiple electromagnets are fixedly installed inside the mounting slots. A metal block is attached to the outer surface of the electromagnet, and an electronic instrument panel body is fixedly installed at the other end of the metal block. A battery is fixedly installed on the rear side of the upper surface of the flight simulator cockpit, and a power supply button is fixedly installed on the upper surface of the flight simulator cockpit.

[0006] According to the above technical solution, multiple slide rails are fixedly installed inside the mounting groove, and multiple slide grooves are opened on the outer surface of the electronic instrument panel body.

[0007] According to the above technical solution, a cable connector is fixedly installed in the middle of the mounting groove, and a cable interface is fixedly installed on the outer surface of the electronic instrument panel body.

[0008] According to the above technical solution, the front center of the flight simulator cockpit contains a mechanical instrument panel, and the front right side of the flight simulator cockpit contains a radio.

[0009] According to the above technical solution, the front left side of the flight simulator cockpit includes a switch control board, and the front lower left corner of the flight simulator cockpit includes a navigation control board.

[0010] According to the above technical solution, multiple engine control levers are fixedly installed at the lower middle front side of the flight simulator cockpit.

[0011] According to the above technical solution, the front outer surface of the flight simulator cockpit is provided with multiple driving control levers.

[0012] According to the above technical solution, a power interface is provided on the rear outer surface of the flight simulator cockpit.

[0013] Compared with existing technologies, the beneficial effects achieved by this utility model are as follows: The electromagnet uses electromagnetic attraction to attract a metal block to fix the main body of the electronic instrument panel, providing a stable holding force for the module. The power supply button controls the circuit connection between the battery and the electromagnet, which is a control component that allows the operator to actively trigger the electromagnet to power on or off, realizing manual intervention in the fixed state of the module. Utilizing the magnetic force generated by the energized electromagnet, the main body of the electronic instrument panel is attracted by the metal block, providing a stable and reliable fixing force, allowing the instrument module to operate in the simulated cockpit. When it is necessary to disassemble the instrument module, the electromagnet is de-energized, the magnetic force disappears, and the main body of the electronic instrument panel is smoothly separated from the mounting slot, providing the trigger condition for module disassembly. By installing a component that uses the characteristics of an electromagnet to fix the electronic instrument panel in this device, the instrument panel can be quickly fixed and unlocked, reducing disassembly time and improving overall operation and maintenance efficiency. Attached Figure Description

[0014] The accompanying drawings are provided to further illustrate the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention, but do not constitute a limitation thereof. In the drawings: Figure 1 This is a front three-dimensional structural diagram of the present invention; Figure 2 This is a schematic diagram of the docking component structure of this utility model; Figure 3 This is a schematic diagram of the display component structure of this utility model; Figure 4 This is a front view structural diagram of this utility model; Figure 5 This is a schematic diagram of the rear three-dimensional structure of this utility model.

[0015] The diagram shows the following markings: 1. Flight simulator cockpit; 2. Mounting slot; 3. Electromagnet; 4. Metal block; 5. Electronic instrument panel body; 6. Battery; 7. Power button; 8. Slide rail; 9. Slide groove; 10. Cable connector; 11. Cable interface; 12. Mechanical instrument panel; 13. Radio; 14. Switch control board; 15. Navigation control board; 16. Engine control stick; 17. Pilot control stick; 18. Power interface. Detailed Implementation

[0016] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0017] Please see Figure 1 , 2 3 and 5 are quick-release instrument module mounting rack structures for flight simulator cockpits, including a flight simulator console 1. Multiple mounting slots 2 are formed on the outer surface of the flight simulator console 1. Multiple electromagnets 3 are fixedly installed inside the mounting slots 2. Metal blocks 4 are attached to the outer surface of the electromagnets 3. The electronic instrument panel body 5 is fixedly installed at the other end of the metal blocks 4. A battery 6 is fixedly installed on the rear side of the upper surface of the flight simulator console 1. A power button 7 is fixedly installed on the upper surface of the flight simulator console 1. The flight simulator console 1 serves as the basic carrier for the installation and integration of the entire instrument module, providing physical installation space and an electrical connection platform for the flight instrument panel body, simulating the layout and functional logic of a real flight simulator console. The mounting slots 2 provide presets for the electronic instrument panel. The installation space serves as a physical positioning and limiting element, ensuring precise installation of each component and stable positioning of the module after installation. It employs a combination of electromagnet 3, metal block 4, and electronic instrument panel body 5. Electromagnet 3 uses electromagnetic attraction to attract metal block 4 to fix the electronic instrument panel body 5, providing a stable holding force for the module. By switching between power on and off, the module's fixation and release can be achieved, making it the core component for the quick disassembly function. Metal block 4 acts as the object of the electromagnet's attraction, transmitting electromagnetic force to fix the electronic instrument panel body 5. The electronic instrument panel body 5 simulates the functions of a real aircraft instrument panel, displaying flight parameters and providing a data interaction interface for simulated flight training and experience, allowing users to obtain flight-related information and make operational decisions.

[0018] The circuit of battery 6 is electrically connected to electromagnet 3 via a cable, providing electromagnet 3 with an independent and continuous power supply. When the main body of the electronic instrument panel 5 needs to be independently debugged, battery 6 can still work normally, maintaining the module's fixation or enabling quick disassembly. The power button 7 is located between the circuit of electromagnet 3 and battery 6, thereby controlling the on / off of the circuit between battery 6 and electromagnet 3. It is a control component that allows the operator to actively trigger the electromagnet to power on or off, realizing manual intervention in the module's fixation state. Utilizing the magnetic force generated by the energized electromagnet 3, the main body of the electronic instrument panel 5 is attracted by the metal block 4, providing a stable and reliable fixing force, allowing the instrument module to operate in the simulated cockpit. When the instrument module needs to be disassembled, the electromagnet is de-energized, the magnetic force disappears, and the main body of the electronic instrument panel 5 is smoothly separated from the mounting slot 2, providing the trigger condition for module disassembly. By installing a component that uses the characteristics of electromagnets to fix the electronic instrument panel in this device, the instrument panel can be quickly fixed and unlocked, reducing disassembly time and improving overall operation and maintenance efficiency.

[0019] Please see Figure 2-3 Multiple slide rails 8 are fixedly installed inside the mounting slot 2, and multiple slide grooves 9 are opened on the outer surface of the electronic instrument panel body 5. The slide rails 8 provide a guide rail for the electronic instrument panel body 5 to slide in a straight line, so that it can move along a fixed direction during installation and disassembly. The slide grooves 9 cooperate with the slide rails 8 inside the mounting slot 2 to form a sliding connection structure, so that the electronic instrument panel body 5 can move smoothly along the slide rails 8, ensuring the correct installation position and improving reliability.

[0020] Please see Figure 2 and 3 A cable connector 10 is fixedly installed in the middle of the mounting slot 2, and a cable interface 11 is fixedly installed on the outer surface of the electronic instrument panel body 5. The cable connector 10 serves as a fixed-end electrical interface and connects with the cable interface 11 when the electronic instrument panel body 5 enters the mounting slot 2, thereby realizing the electrical connection between the instrument panel and the simulated cockpit system. The cable interface 11 corresponds to the cable connector 10 inside the mounting slot 2 and serves as the electrical connection port of the electronic instrument panel body 5, receiving power and data signals, driving the instrument display function, and feeding back the operation signals to the simulation system.

[0021] Please see Figure 1 and 4 The front center of the flight simulator cockpit 1 contains a mechanical instrument panel 12, and the front right side of the flight simulator cockpit 1 contains a radio 13. The mechanical instrument panel 12 contains a barometric altimeter, an airspeed indicator, and a magnetic compass, which are used to simulate traditional mechanical instruments and present flight parameters intuitively through the physical display of mechanical pointers and dials. The radio 13 simulates the communication radio function of the aircraft and is used to train pilots in the voice communication process with the control tower and other aircraft.

[0022] Please see Figure 4 The front left side of the flight simulator cockpit 1 contains a switch control board 14, and the front lower left corner of the flight simulator cockpit 1 contains a navigation control board 15. The switch control board 14 integrates various system switches of the aircraft and simulates the switching operation of real equipment through physical buttons and knobs to control the state switching of the simulation system. The navigation control board 15 simulates the control interface of the aircraft navigation system and is used to set navigation parameters.

[0023] Please see Figure 1 and 4 Multiple engine control levers 16 are fixedly installed at the lower center of the front side of the flight simulator cockpit 1. The engine control levers 16 simulate the engine throttle lever, thrust lever and other control devices of the aircraft. By pushing, pulling and rotating, the power and thrust output of the simulated engine are adjusted, and the flight speed and climb rate are controlled.

[0024] Please see Figure 1 Multiple control sticks 17 are installed on the front outer surface of the flight simulator cockpit 1. The control sticks 17 simulate the control sticks of an aircraft and are used to control the pitch and roll attitude of the aircraft. They are the core input devices for flight control.

[0025] Please see Figure 5 A power interface 18 is provided on the rear outer surface of the flight simulator cockpit 1. The power interface 18 serves as the external power input port of the simulator cockpit, connecting to an external power supply system to provide power support for the electrical equipment in the device.

[0026] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0027] Finally, it should be noted that the above are merely preferred embodiments of this utility model and are not intended to limit the utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A quick-release instrument module mounting structure for an aircraft simulator cockpit, comprising a flight simulator cockpit (1), characterized in that: The outer surface of the flight simulator (1) is provided with multiple mounting slots (2), and multiple electromagnets (3) are fixedly installed inside the mounting slots (2). A metal block (4) is attached to the outer surface of the electromagnet (3), and an electronic instrument panel body (5) is fixedly installed at the other end of the metal block (4). A battery (6) is fixedly installed on the rear side of the upper surface of the flight simulator (1), and a power supply button (7) is fixedly installed on the upper surface of the flight simulator (1).

2. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: Multiple slide rails (8) are fixedly installed inside the mounting groove (2), and multiple slide grooves (9) are opened on the outer surface of the electronic instrument panel body (5).

3. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: A cable connector (10) is fixedly installed in the middle of the mounting slot (2), and a cable interface (11) is fixedly installed on the outer surface of the electronic instrument panel body (5).

4. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: The front center of the flight simulator (1) contains a mechanical instrument panel (12), and the front right side of the flight simulator (1) contains a radio (13).

5. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: The flight simulator (1) has a switch control board (14) on the front left side and a navigation control board (15) on the front lower left corner.

6. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: Multiple engine control levers (16) are fixedly installed at the lower middle front side of the flight simulator cockpit (1).

7. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: The flight simulator cockpit (1) has multiple control levers (17) on its front outer surface.

8. The quick-release instrument module mounting bracket structure for an aircraft simulator cockpit according to claim 1, characterized in that: A power interface (18) is provided on the rear outer surface of the flight simulator cockpit (1).

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