Double aviation simulation training equipment

Abstract

The utility model relates to the technical field of aviation simulation driving devices, and provides double aviation simulation training equipment which comprises a simulation cabin which is arranged on a cabin base and comprises a front panel, a rocker unit is arranged on the front panel, a foot rudder unit is arranged on the cabin base below the rocker unit, and the rocker unit and the foot rudder unit are used for simulation training control; the rocker unit comprises a left rocker and a right rocker, and the left rocker and the right rocker are connected through a rocker linkage assembly and used for synchronous movement of the left rocker and the right rocker. The foot rudder unit comprises a left foot rudder and a right foot rudder, and the left foot rudder and the right foot rudder are connected through a foot rudder linkage assembly and used for synchronous action of the left foot rudder and the right foot rudder. The avionics system is arranged on the front panel and used for displaying real-time data of simulated flight; the control keys are arranged on the front panel and used for assisting in controlling the simulated flight state; and the visual display system is used for displaying the surrounding environment of the simulated flight. According to the utility model, a two-person driving type or a training plane can be simulated, so that an instructor can timely correct possible operation errors of trainees, and the efficiency and the quality of simulation training are improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation simulation driving devices, and particularly relates to a double-person aviation simulation training device. Background Art

[0002] Aviation simulation training devices are important tools for pilot training and skill improvement. Through a highly simulated environment, they provide pilots with an experience close to real flight without incurring the high costs and safety risks of actual flight. By combining software and hardware, aviation simulation training devices can simulate flight scenarios from simple to complex and are indispensable tools for pilot training and skill improvement.

[0003] Currently, common aviation simulation training devices are generally single-person aviation simulation training devices, which only allow one pilot or trainee to participate in the simulation training. They cannot truly simulate double-pilot aircraft models, such as two-seat models in general aviation, Airbus models, trainer aircraft, etc., nor can they complete tasks that require two-person cooperation. Single-person aviation simulation trainers are lacking in terms of the comprehensiveness and cooperation of simulated scenarios and tasks.

[0004] Therefore, in view of the above problems, a double-person aviation simulation training device is proposed to solve the above problems. Content of the Utility Model

[0005] Aiming at the deficiencies of the prior art, the utility model develops a double-person aviation simulation training device, which can simulate double-pilot aircraft models or trainer aircraft, enabling the instructor to promptly correct possible operation mistakes of the trainee and improving the efficiency and quality of simulation training.

[0006] To achieve the above object, the utility model is realized through the following technical solutions:

[0007] A double-person aviation simulation training device includes: a simulation cabin, arranged on a cabin base, including a front panel, on which a rocker unit is arranged, and a rudder pedal unit is arranged on the cabin base below the rocker unit. The rocker unit and the rudder pedal unit are used for simulation training control; the rocker unit includes a left rocker and a right rocker, and the left rocker and the right rocker are connected by a rocker linkage component for simultaneous rotation or forward and backward movement of the left rocker and the right rocker; the rudder pedal unit includes a left rudder pedal and a right rudder pedal, and the left rudder pedal and the right rudder pedal are connected by a rudder pedal linkage component for synchronous movement of the left rudder pedal and the right rudder pedal; an avionics system, arranged on the front panel, for displaying real-time data of simulated flight; operation buttons, arranged on the front panel, for assisting in controlling the simulated flight state; a visual display system, for displaying the surrounding environment of simulated flight.

[0008] Preferably, the left joystick includes a left handle and a left control lever. The left handle is provided at one end of the left control lever, and the other end of the left control lever penetrates through the front panel and is arranged in the simulation cabin to connect with the joystick linkage assembly; the right joystick includes a right handle and a right control lever. The right handle is provided at one end of the right control lever, and the other end of the right control lever penetrates through the front panel and is arranged in the simulation cabin to connect with the joystick linkage assembly; both the left handle and the right handle are located outside the simulation cabin, and the axes of the left control lever and the right control lever are parallel to each other.

[0009] Preferably, the joystick linkage assembly includes a translation mechanism and a rotation mechanism. The translation mechanism includes a slide rail, which is arranged in the simulation cabin, and the length direction of the slide rail is parallel to the axis of the left control lever. A slider is slidably arranged on the slide rail, and a translation plate is arranged on the slider. Both the left control lever and the right control lever are rotatably arranged on the translation plate, and both the left control lever and the right control lever are used to drive the translation plate to move along the length direction of the slide rail; the rotation mechanism includes a left gear disk and a right gear disk. The left gear disk is coaxially arranged at the end of the left control lever away from the left handle, and the right gear disk is coaxially arranged at the end of the right control lever away from the right handle. The left gear disk and the right gear disk are connected by chain drive for the synchronous and same-direction rotation of the left control lever and the right control lever.

[0010] Preferably, it further includes a centering unit, which includes a left-right centering assembly and a front-back centering assembly. The front-back centering assembly includes a front spring and a rear spring, which are sleeved on the left control lever and the right control lever. The two ends of the front spring are respectively connected to the inner wall of the front panel and the translation plate, and the two ends of the rear spring are respectively connected to the wall of the fixed plate in the simulation cabin and the translation plate. The front spring and the rear spring are located on both sides of the translation plate; the left-right centering assembly includes a middle position plate, which is arranged on the translation plate. Guide blocks are arranged on both sides of the middle position plate, and a left spring and a right spring are arranged in the guide blocks. The left spring is close to the left control lever, and the right spring is close to the right control lever. The left spring and the left control lever are connected by a left connecting rod, and the right spring and the right control lever are connected by a right connecting rod.

[0011] Preferably, the foot pedal linkage assembly includes a support shaft, a left linkage shaft and a right linkage shaft. The support shaft is arranged on the cabin base, and the left linkage shaft and the right linkage shaft are used to connect the left foot pedal and the right foot pedal, and the axes of the left linkage shaft and the right linkage shaft are both parallel to the axis of the support shaft.

[0012] Preferably, the left foot rudder includes a first left pedal and a first right pedal. The first left pedal is connected to the support shaft through a first left rotating plate, and the first right pedal is connected to the support shaft through a first right rotating plate. Both the first left rotating plate and the first right rotating plate are arranged in an L shape, and the arrangement directions of the L shapes of the first left rotating plate and the first right rotating plate are opposite. The right foot rudder includes a second left pedal and a second right pedal. The second left pedal is connected to the support shaft through a second left rotating plate, and the second right pedal is connected to the support shaft through a second right rotating plate. The second left pedal is identical in shape and size to the first left pedal, and the second right pedal is identical in shape and size to the first right pedal. One end of the first left rotating plate away from the first left pedal and one end of the second left rotating plate away from the second left pedal are respectively arranged at both ends of the left linkage shaft, and one end of the first right rotating plate away from the first right pedal and one end of the second right rotating plate away from the second right pedal are respectively arranged at both ends of the right linkage shaft.

[0013] Preferably, a first left linkage plate and a second left linkage plate are respectively arranged at both ends of the left linkage shaft, and a first right linkage plate and a second right linkage plate are respectively arranged at both ends of the right linkage shaft. The foot rudder linkage assembly further includes a first left support rod, a second left support rod, a first right support rod, and a second right support rod. Both ends of the first left support rod are respectively connected to the first left pedal and the first left linkage plate, both ends of the second left support rod are respectively connected to the second left pedal and the second left linkage plate, both ends of the first right support rod are respectively connected to the first right pedal and the first right linkage plate, and both ends of the second right support rod are respectively connected to the second right pedal and the second right linkage plate.

[0014] Preferably, it further includes a transmission assembly, including a left bevel gear and a right bevel gear. The left bevel gear is arranged on the first left rotating plate or the second left rotating plate, and the right bevel gear is arranged on the first right rotating plate or the second right rotating plate. Both the left bevel gear and the right bevel gear are arranged coaxially with the support shaft, the tips of the teeth of the left bevel gear and the right bevel gear face each other, and the left bevel gear and the right bevel gear are meshed and connected through a middle bevel gear, and the middle bevel gear is arranged on the engine room base.

[0015] Preferably, a left seat and a right seat are arranged on the engine room base, and the left seat and the right seat are respectively located behind the left rocker and the right rocker.

[0016] Preferably, it further includes a control system, including a detection component and a control component. The detection component includes an angle sensor and a distance sensor, which are arranged on the rocker unit and the foot rudder unit for detecting the angle change amount and the distance change amount. The control component is connected to the avionics system, the operation buttons, the visual display system, and the detection component for controlling the overall normal operation of the device.

[0017] The effects provided in the utility model content are only the effects of the embodiments, rather than all the effects of the utility model. The above technical solutions have the following advantages:

[0018] 1. The utility model adopts a linkage operation with two operation positions, enabling the trainee to be at one operation position and the instructor to be at the other operation position. This facilitates the instructor to understand the trainee's simulated flight state in real time and correct any possible operation errors of the trainee in a timely manner, thus improving the quality and efficiency of training.

[0019] 2. The utility model is provided with a rocker unit, and the rocker unit includes a left rocker and a right rocker connected by a rocker linkage component. The movement of the left rocker or the right rocker can drive the simultaneous movement of the other right rocker or left rocker, realizing the synchronization of hand movements during dual-person simulation training and improving the accuracy and efficiency of training.

[0020] 3. The utility model is provided with a rudder pedal unit, including a left rudder pedal and a right rudder pedal connected by a rudder pedal linkage component. The movement of the left rudder pedal or the right rudder pedal can drive the movement of the other right rudder pedal or left rudder pedal, realizing the synchronization of foot movements during dual-person simulation training, reducing the possibility of errors during training, and improving the accuracy of training.

[0021] 4. The utility model is provided with a centering unit, which can automatically return the left rocker and the right rocker to their initial positions after moving and rotating, avoiding the trainee forgetting to return to the neutral position and reducing the operation steps, alleviating the learning intensity of simulation training, and improving safety and learning efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] The drawings are used to provide a further understanding of the utility model and form a part of the specification. They are used together with the embodiments of the utility model to explain the utility model and do not constitute a limitation to the utility model.

[0023] Figure 1 It is a schematic structural diagram of the embodiment of the utility model removing the visual display system;

[0024] Figure 2 It is a schematic overall structural diagram of the embodiment of the utility model;

[0025] Figure 3 It is a schematic position diagram of the rocker unit of the embodiment of the utility model;

[0026] Figure 4 It is a schematic structural diagram of the rocker unit of the embodiment of the utility model;

[0027] Figure 5 It is a schematic front view partially sectional structural diagram of the rocker unit of the embodiment of the utility model;

[0028] Figure 6 It is a schematic structural diagram of the rudder pedal unit of the embodiment of the utility model Figure 1 ;

[0029] Figure 7 is Figure 6Enlarged view of part A

[0030] Figure 8 Structural schematic of the foot rudder unit according to an embodiment of the present utility model Figure 2 。

[0031] In the figure, 1, simulated cabin; 2, cabin base; 3, front panel; 4, left rocker; 5, right rocker; 6, rocker linkage assembly; 7, left foot rudder; 8, right foot rudder; 9, foot rudder linkage assembly; 10, avionics system; 11, operation button; 12, visual display system; 13, transmission assembly; 14, left seat; 15, right seat; 101, fixing plate; 401, left handle; 402, left control rod; 501, right handle; 502, right control rod; 601, slide rail; 602, slider; 603, translation plate; 604, left gear disk; 605, right gear disk; 606, chain; 607, front spring; 608, rear spring; 609, middle position plate; 610, guide block; 611, left spring; 612, right spring; 613, left connecting rod; 614, right connecting rod; 701, left pedal 1; 702, right pedal 1; 703, left rotating plate 1; 704, right rotating plate 1; 801, left pedal 2; 802, right pedal 2; 803, left rotating plate 2; 804, right rotating plate 2; 901, support shaft; 902, left linkage shaft; 903, right linkage shaft; 904, left support rod 1; 905, left support rod 2; 906, right support rod 1; 907, right support rod 2; 9021, left linkage plate 1; 9022, left linkage plate 2; 9031, right linkage plate 1; 9032, right linkage plate 2; 1301, left bevel gear; 1302, right bevel gear; 1303, middle bevel gear. Detailed implementation manners

[0032] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described 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 of the embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0033] As Figures 1-8 shown, the present utility model provides a technical solution:

[0034] A two-person aviation simulation training device, comprising: a simulation cabin 1, arranged on a cabin base 2, including a front panel 3 and a fixing plate 101. A rocker unit is arranged between the front panel 3 and the fixing plate 101, and a foot rudder unit is arranged on the cabin base 2 below the rocker unit. The rocker unit and the foot rudder unit are used for simulating the control of hands and feet during training; the rocker unit includes a left rocker 4 and a right rocker 5, and the left rocker 4 and the right rocker 5 are connected by a rocker linkage component 6 for the simultaneous rotation or forward and backward movement of the left rocker 4 and the right rocker 5; the foot rudder unit includes a left foot rudder 7 and a right foot rudder 8, and the left foot rudder 7 and the right foot rudder 8 are connected by a foot rudder linkage component 9 for the synchronous movement of the left foot rudder 7 and the right foot rudder 8; an avionics system 10, arranged on the front panel 3, for displaying real-time data of the simulated flight; manipulation buttons 11, arranged on the front panel 3, for assisting in controlling the state of the simulated flight; a visual display system 12, for displaying the surrounding environment of the simulated flight.

[0035] In this embodiment, the left rocker 4 includes a left handle 401 and a left control rod 402. The left handle 401 is arranged at one end of the left control rod 402, and the other end of the left control rod 402 penetrates through the front panel 3 and is arranged inside the simulation cabin 1 to connect the rocker linkage component 6; the right rocker 5 includes a right handle 501 and a right control rod 502. The right handle 501 is arranged at one end of the right control rod 502, and the other end of the right control rod 502 penetrates through the front panel 3 and is arranged inside the simulation cabin 1 to connect the rocker linkage component 6. Moreover, both the left handle 401 and the right handle 501 are located outside the front panel 3 of the simulation cabin 1, and the axes of the left control rod 402 and the right control rod 502 are parallel to each other, so that the left rocker 4 and the right rocker 5 can move synchronously through the rocker linkage component 6, improving the practicability of the device.

[0036] In this embodiment, the rocker linkage assembly 6 includes a translation mechanism and a rotation mechanism. The translation mechanism includes a slide rail 601, preferably includes at least two slide rails 601, the two slide rails 601 are arranged in parallel with each other in the simulation cabin 1, and the length direction of the slide rail 601 is parallel to the axis of the left control rod 402, a slider 602 is slidably arranged on the slide rail 601, and a translation plate 603 is arranged on the slider 602. The left control rod 402 and the right control rod 502 are both rotatably arranged on the translation plate 603, and the left control rod 402 and the right control rod 502 are both used to drive the translation plate 603 to move along the length direction of the slide rail 601. The left control rod 402 and the right control rod 502 are driven by the translation mechanism to move the translation plate 603 along the length direction of the slide rail 601. The rocker 4 or the right rocker 5 can drive the other rocker to translate along the length direction of the slide rail 601; the rotating mechanism includes a left sprocket 604 and a right sprocket 605, the left sprocket 604 is coaxially arranged at the end of the left control rod 402 away from the left handle 401, and the right sprocket 605 is coaxially arranged at the end of the right control rod 502 away from the right handle 501, and the left sprocket 604 and the right sprocket 605 are both located on the side of the fixed plate 101 away from the translation plate 603, the left sprocket 604 and the right sprocket 605 are connected by a chain 606 for synchronous and unidirectional rotation of the left control rod 402 and the right control rod 502, thereby improving the accuracy and stability of the linkage.

[0037] In this embodiment, it further includes a centering unit, which includes a left - right centering component and a front - rear centering component. The front - rear centering component includes a front spring 607 and a rear spring 608, both of which are sleeved on the left control rod 402 and the right control rod 502. The two ends of the front spring 607 are respectively connected to the inner wall of the front panel 3 and one side of the translation plate 603. The two ends of the rear spring 608 are respectively connected to the wall of the fixed plate 101 in the simulation cabin 1 and the side of the translation plate 603 away from the front spring 607. The front spring 607 and the rear spring 608 are located on both sides of the translation plate 603, so as to compress the front spring 607 or the rear spring 608 during the movement of the translation plate 603. The left - right centering component includes a middle - position plate 609, which is arranged in the middle of the translation plate 603. Guide blocks 610 are arranged on both sides of the middle - position plate 609. Guide grooves are opened on the guide blocks 610. A left spring 611 and a right spring 612 are arranged in the guide grooves. The left spring 611 is located on the side of the middle - position plate 609 close to the left control rod 402, and the right spring 612 is located on the side of the middle - position plate 609 close to the right control rod 502. And a left connecting rod 613 is connected between the left spring 611 and the left control rod 402, and a right connecting rod 614 is connected between the right spring 612 and the right control rod 502. A left support rod is arranged on the left control rod 402, which can rotate around the axis of the left control rod 402 as the left control rod 402 rotates. One end of the left support rod away from the left control rod 402 is rotatably connected to the left connecting rod 613. A right support rod is arranged on the right control rod 502, which can rotate around the axis of the right control rod 502 as the right control rod 502 rotates. One end of the right support rod away from the right control rod 502 is rotatably connected to the right connecting rod 614, which facilitates the compression of the left spring 611 and the right spring 612 and improves the practicability.

[0038] In another embodiment, the opening diameter of the guide groove is larger than the diameters of the left connecting rod 613 and the right connecting rod 614, so that the left connecting rod 613 and the right connecting rod 614 can move slightly up and down relative to the opening of the guide groove, so as to avoid interfering with the actions of the left control rod 402 and the right control rod 502 when the left control rod 402 and the right control rod 502 rotate to drive the left connecting rod 613 and the right connecting rod 614 to have a small - amplitude up - down displacement, which improves the practicability of the device. And a blocking plate is arranged at the opening of the guide groove to prevent the left connecting rod 613 and the right connecting rod 614 from slipping out of the guide groove, which improves the safety of the device.

[0039] In this embodiment, the foot - rudder linkage component 9 includes a support shaft 901, a left linkage shaft 902 and a right linkage shaft 903. The support shaft 901 is arranged on the cabin base 2. The left linkage shaft 902 and the right linkage shaft 903 are used to connect the left foot - rudder 7 and the right foot - rudder 8 to transmit the actions of the left foot - rudder 7 and the right foot - rudder 8, and the axes of the left linkage shaft 902 and the right linkage shaft 903 are both parallel to the axis of the support shaft 901.

[0040] In this embodiment, the left foot rudder 7 includes a left pedal one 701 and a right pedal one 702. The left pedal one 701 is rotatably connected to the support shaft 901 through a left rotating plate one 703, and the middle of the left pedal one 701 is rotatably connected to one end of the left rotating plate one 703. The right pedal one 702 is rotatably connected to the support shaft 901 through a right rotating plate one 704, and the middle of the right pedal one 702 is rotatably connected to one end of the right rotating plate one 704. Both the left rotating plate one 703 and the right rotating plate one 704 are L-shaped, and the laying directions of the L-shapes of the left rotating plate one 703 and the right rotating plate one 704 are opposite. The right foot rudder 8 includes a left pedal two 801 and a right pedal two 802. The left pedal two 801 is rotatably connected to the support shaft 901 through a left rotating plate two 803, and the middle of the left pedal two 801 is rotatably connected to one end of the left rotating plate two 803. The right pedal two 802 is rotatably connected to the support shaft 901 through a right rotating plate two 804, and the middle of the right pedal two 802 is rotatably connected to one end of the right rotating plate two 804. The left pedal two 801 is set to have the same shape and size as the left pedal one 701, and the right pedal two 802 is set to have the same shape and size as the right pedal one 702. One end of the left rotating plate one 703 away from the left pedal one 701 and one end of the left rotating plate two 803 away from the left pedal two 801 are respectively rotatably arranged at both ends of the left linkage shaft 902, and one end of the right rotating plate one 704 away from the right pedal one 702 and one end of the right rotating plate two 804 away from the right pedal two 802 are respectively rotatably arranged at both ends of the right linkage shaft 903, so as to connect the left pedal one 701 and the left pedal two 801 through the left linkage shaft 902 and connect the right pedal one 702 and the right pedal two 802 through the right linkage shaft 903, improving the practicability.

[0041] In this embodiment, a left linkage plate one 9021 and a left linkage plate two 9022 are respectively arranged at both ends of the left linkage shaft 902, and a right linkage plate one 9031 and a right linkage plate two 9032 are respectively arranged at both ends of the right linkage shaft 903. The foot rudder linkage assembly 9 further includes a left support rod one 904, a left support rod two 905, a right support rod one 906 and a right support rod two 907. Both ends of the left support rod one 904 are respectively rotatably connected to the bottom of the left pedal one 701 and one end of the left linkage plate one 9021 away from the left linkage shaft 902. Both ends of the left support rod two 905 are respectively rotatably connected to the bottom end of the left pedal two 801 and one end of the left linkage plate two 9022 away from the left linkage shaft 902. Both ends of the right support rod one 906 are respectively rotatably connected to the bottom end of the right pedal one 702 and one end of the right linkage plate one 9031 away from the right linkage shaft 903. Both ends of the right support rod two 907 are respectively rotatably connected to the bottom end of the right pedal two 802 and one end of the right linkage plate two 9032 away from the right linkage shaft 903. The left support rod one 904 and the left support rod two 905 are of the same length and parallel to each other, and the right support rod one 906 and the right support rod two 907 are of the same length and parallel to each other, so as to transmit the force of the foot on the pedal to the linkage shaft to drive another pedal connected to the linkage shaft to perform synchronous actions.

[0042] In this embodiment, it further includes a transmission assembly 13, which includes a left bevel gear 1301 and a right bevel gear 1302. The left bevel gear 1301 is arranged on the first left rotating plate 703 or the second left rotating plate 803, and the right bevel gear 1302 is arranged on the first right rotating plate 704 or the second right rotating plate 804. Both the left bevel gear 1301 and the right bevel gear 1302 are coaxially arranged with the support shaft 901 but not connected to the support shaft 901. The support shaft 901 does not affect the rotation of the left bevel gear 1301 and the right bevel gear 1302. The tips of the teeth of the left bevel gear 1301 and the right bevel gear 1302 face each other, and the left bevel gear 1301 and the right bevel gear 1302 are meshed and connected through a middle bevel gear 1303 to transmit kinetic energy. The middle bevel gear 1303 is rotatably arranged on the engine nacelle base 2, improving stability.

[0043] In this embodiment, a left seat 14 and a right seat 15 are arranged on the engine nacelle base 2. The left seat 14 and the right seat 15 are respectively located behind the left rocker 4 and the right rocker 5 for use by trainees or instructors. The left seat 14 and the right seat 15 can adopt conventional seats on the market and can be adjusted in the front-back, up-down, and backrest angle directions, improving the comfort of training.

[0044] In another embodiment, the avionics system 10 and the control buttons 11 can select systems of the same type as those of single-person aviation simulation training equipment, and only two sets need to be set on this device, which is more economical.

[0045] In this embodiment, the visual display system 12 adopts a triple display screen and is placed in front of the trainee during training, facilitating the trainee to observe and improving the training effect; in another embodiment, other devices with visual display, such as VR devices, can also be used, providing a better experience and improving the practicality of the device.

[0046] In this embodiment, it further includes a control system, which includes a detection component and a control component. The detection component includes an angle sensor and a distance sensor, which are arranged on the rocker unit and the foot rudder unit and are used to detect the angle change amount and the distance change amount. Specifically, the angle sensor is arranged on the left control lever 402, the right control lever 502, the left linkage shaft 902, and the right linkage shaft 903, and the distance sensor is arranged on the translation plate 603. The data measured by the angle sensor and the distance sensor can both be displayed on the display screen of the avionics system 10, enabling the trainee to timely and accurately understand the current state of the simulated flight, facilitating control and correction; the control component can be controlled by a control chip such as a single-chip microcomputer. The control component is connected to the avionics system 10, the control buttons 11, the visual display system 12, and the detection component, and is used to control the overall normal operation of the device.

[0047] Working principle: First, the device is powered on and each power-consuming system of the device is started. The trainee sits on one of the seats, and the other seat can be idle or used by the instructor for operation. Then, the trainee conducts simulated training and controls the flight state through the joystick unit and foot rudder unit on one side. At this time, the joystick unit and foot rudder unit on the other side will synchronously present the same actions. When there is an instructor on that side, the instructor can timely control and correct possible operation mistakes of the trainee or synchronously teach the trainee control actions, which is convenient for the trainee to quickly learn and improves the quality of simulated training and the efficiency of teaching.

[0048] The details not described in this utility model are all conventional technical means well known to those skilled in the art.

[0049] In the description of this utility model, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc. is based on the orientation or positional relationship shown in the drawings. It is only for the convenience of describing this utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to this utility model.

[0050] In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include one or more of such features. In the description of this utility model, the meaning of "a plurality" is two or more, unless otherwise specifically defined.

[0051] Although the embodiments of this utility model have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of this utility model. The scope of this utility model is defined by the appended claims and their equivalents.

[0052] Finally, it should be noted that the above are only the preferred embodiments of this utility model and are not used to limit this utility model. Although this utility model has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments or perform equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of this utility model shall be included within the protection scope of this utility model.

Claims

1. A two-person aviation simulation training device, comprising a simulated cabin (1) arranged on a cabin base (2), a front panel (3) arranged on one side of the simulated cabin (1), and further comprising: An avionics system (10), arranged on the front panel (3), for displaying real-time data of simulated flight; The operating button (11) is arranged on the front panel (3) and is used for assisting in controlling the simulated flight state; the visual display system (12) is used for displaying the surrounding environment of the simulated flight, and is characterized in that: A rocker unit is arranged on the front panel (3), and a rudder foot unit is arranged on the cabin base (2) below the rocker unit. The rocker unit and the rudder foot unit are used for simulated training control. The rocker unit comprises a left rocker (4) and a right rocker (5), wherein the left rocker (4) and the right rocker (5) are connected via a rocker linkage assembly (6) for synchronous movement of the left rocker (4) and the right rocker (5); The rudder foot unit comprises a left rudder foot (7) and a right rudder foot (8), and the left rudder foot (7) and the right rudder foot (8) are connected via a rudder foot linkage assembly (9) for synchronous action of the left rudder foot (7) and the right rudder foot (8).

2. A two-person aviation simulation training device according to claim 1, characterized in that: The left rocker (4) comprises a left handle (401) and a left control rod (402), wherein the left handle (401) is arranged at one end of the left control rod (402), and the other end of the left control rod (402) passes through the front panel (3) and is arranged in the simulated cabin (1) to connect to the rocker linkage assembly (6); The right rocker (5) comprises a right handle (501) and a right control rod (502), wherein the right handle (501) is arranged at one end of the right control rod (502), and the other end of the right control rod (502) passes through the front panel (3) and is arranged in the simulated cabin (1) to connect with the rocker linkage assembly (6); The left handle (401) and the right handle (501) are both located outside the simulated cabin (1), and the axes of the left control rod (402) and the right control rod (502) are parallel to each other.

3. A two-person aviation simulation training device according to claim 2, characterized in that: The rocker linkage assembly (6) comprises a translation mechanism and a rotation mechanism, the translation mechanism comprises a slide rail (601), the slide rail (601) is arranged in the simulated cabin (1), and the length direction of the slide rail (601) is parallel to the axis of the left control rod (402), a slider (602) is slidably arranged on the slide rail (601), a translation plate (603) is arranged on the slider (602), the left control rod (402) and the right control rod (502) are both rotatably arranged on the translation plate (603), and the left control rod (402) and the right control rod (502) are both used to drive the translation plate (603) to move along the length direction of the slide rail (601); The rotating mechanism comprises a left toothed disc (604) and a right toothed disc (605). The left toothed disc (604) is coaxially arranged at one end of the left control rod (402) away from the left handle (401), and the right toothed disc (605) is coaxially arranged at one end of the right control rod (502) away from the right handle (501). The left toothed disc (604) and the right toothed disc (605) are connected by a chain (606) for synchronous and unidirectional rotation of the left control rod (402) and the right control rod (502).

4. A two-person aviation simulation training device according to claim 3, characterized in that: It also includes a centering unit, including left and right centering components and front and rear centering components. The front and rear centering components include a front spring (607) and a rear spring (608), which are sleeved on the left control rod (402) and the right control rod (502). The two ends of the front spring (607) are respectively connected to the inner wall of the front panel (3) and the translation plate (603). The two ends of the rear spring (608) are respectively connected to the plate wall of the fixed plate (101) in the simulated cabin (1) and the translation plate (603). The front spring (607) and the rear spring (608) are located on both sides of the translation plate (603). The left and right return components include a middle plate (609) which is arranged on the translation plate (603). Guide blocks (610) are arranged on both sides of the middle plate (609). A left spring (611) and a right spring (612) are arranged in the guide blocks (610). The left spring (611) is located on a side of the middle plate (609) close to the left control rod (402). The right spring (612) is located on a side of the middle plate (609) close to the right control rod (502). The left spring (611) and the left control rod (402) are connected via a left connecting rod (613). The right spring (612) and the right control rod (502) are connected via a right connecting rod (614).

5. A two-person aviation simulation training device according to claim 4, characterized in that: The rudder foot linkage assembly (9) comprises a support shaft (901), a left linkage shaft (902) and a right linkage shaft (903); the support shaft (901) is arranged on a cabin base (2); the left linkage shaft (902) and the right linkage shaft (903) are used to connect a left rudder foot (7) and a right rudder foot (8); and the axes of the left linkage shaft (902) and the right linkage shaft (903) are parallel to the axis of the support shaft (901).

6. A two-person aviation simulation training device according to claim 5, characterized in that: The left foot rudder (7) comprises a left pedal (701) and a right pedal (702), the left pedal (701) is connected to the support shaft (901) via a left rotating plate (703), and the right pedal (702) is connected to the support shaft (901) via a right rotating plate (704), the left rotating plate (703) and the right rotating plate (704) are both arranged in an L shape, and the L-shapes of the left rotating plate (703) and the right rotating plate (704) are arranged in opposite directions; The right foot rudder (8) comprises a left pedal 2 (801) and a right pedal 2 (802), wherein the left pedal 2 (801) is connected to the support shaft (901) via a left rotating plate 2 (803), and the right pedal 2 (802) is connected to the support shaft (901) via a right rotating plate 2 (804), and the left pedal 2 (801) is consistent in shape and size with the left pedal 1 (701), and the right pedal 2 (802) is consistent in shape and size with the right pedal 1 (702); One end of the left rotating plate 1 (703) away from the left pedal 1 (701) and one end of the left rotating plate 2 (803) away from the left pedal 2 (801) are respectively arranged at two ends of the left linkage shaft (902), and one end of the right rotating plate 1 (704) away from the right pedal 1 (702) and one end of the right rotating plate 2 (804) away from the right pedal 2 (802) are respectively arranged at two ends of the right linkage shaft (903).

7. A two-person aviation simulation training device according to claim 6, characterized in that: The two ends of the left linkage shaft (902) are respectively provided with a left linkage plate 1 (9021) and a left linkage plate 2 (9022), and the two ends of the right linkage shaft (903) are respectively provided with a right linkage plate 1 (9031) and a right linkage plate 2 (9032); The rudder foot linkage assembly (9) also includes a left support rod 1 (904), a left support rod 2 (905), a right support rod 1 (906) and a right support rod 2 (907). The two ends of the left support rod 1 (904) are respectively connected to the left pedal 1 (701) and the left linkage plate 1 (9021). The two ends of the left support rod 2 (905) are respectively connected to the left pedal 2 (801) and the left linkage plate 2 (9022). The two ends of the right support rod 1 (906) are respectively connected to the right pedal 1 (702) and the right linkage plate 1 (9031). The two ends of the right support rod 2 (907) are respectively connected to the right pedal 2 (802) and the right linkage plate 2 (9032).

8. A two-person aviation simulation training device according to claim 7, characterized in that: The invention also comprises a transmission assembly (13), comprising a left bevel gear (1301) and a right bevel gear (1302), wherein the left bevel gear (1301) is arranged on the left rotating plate 1 (703) or the left rotating plate 2 (803), and the right bevel gear (1302) is arranged on the right rotating plate 1 (704) or the right rotating plate 2 (804), and the left bevel gear (1301) and the right bevel gear (1302) are both arranged coaxially with the support shaft (901), and the tooth tips of the left bevel gear (1301) and the right bevel gear (1302) are opposite to each other, and the left bevel gear (1301) and the right bevel gear (1302) are meshedly connected via a middle bevel gear (1303), and the middle bevel gear (1303) is arranged on the cabin base (2).

9. A two-person aviation simulation training device according to claim 8, characterized in that: A left seat (14) and a right seat (15) are arranged on the cabin base (2), and the left seat (14) and the right seat (15) are respectively located behind the left rocker (4) and the right rocker (5).

10. A two-person aviation simulation training device according to claim 9, characterized in that: It also includes a control system, including a detection component and a control component, wherein the detection component includes an angle sensor and a distance sensor, which are arranged on the rocker unit and the foot rudder unit and are used to detect the angle change and the distance change; The control component is connected to the avionics system (10), the operating buttons (11), the visual display system (12) and the detection component, and is used to control the normal operation of the entire device.

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