Aircraft maintenance simulation training device

Abstract

The utility model relates to the technical field of aircraft maintenance, and provides an aircraft maintenance simulation training device. Comprising a maintenance platform which is provided with a first display screen and a second display screen; a through hole is formed in the middle position of the table top of the maintenance table and is communicated with an inner cavity of the maintenance table; an arc-shaped vertical plate is arranged in the inner cavity, a plurality of transmission devices are in transmission connection with the arc-shaped vertical plate, and one of the component modules of the airplane is placed in the containing groove of each transmission device. The device has the beneficial effects that the cabin door module, the undercarriage module and the wing module in the airplane are taken as examples, the corresponding airplane composition modules are scaled down according to the proportion and placed in the accommodating grooves of the transmission devices, and when one of the cabin door module, the undercarriage module and the wing module needs to be trained and maintained, the corresponding button is pressed down; the corresponding transmission device transmits the module located in the containing groove out, the explosion view and the maintenance operation instruction of the module are displayed on the first display screen and the second display screen, operation is convenient, and the manufacturing cost is low.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft maintenance, in particular to an aircraft maintenance simulation training device. Background Art

[0002] An aircraft mainly includes structures such as a fuselage, wings, a power unit, and airborne equipment, and each structure is very complex. In the prior art, aircraft maintenance training is mainly carried out through VR simulation equipment, but the cost of such equipment is relatively high. In view of this, the present invention is proposed. Utility Model Content

[0003] The utility model aims to provide an aircraft maintenance simulation training device to solve the technical problems existing in the prior art.

[0004] To achieve the above-mentioned purpose, the technical solution adopted by the utility model is: an aircraft maintenance simulation training device, comprising: a maintenance platform, on which a first display screen and a second display screen are arranged, wherein the first display screen is used to display an exploded view of each component module of the aircraft, and the second display screen is used to display maintenance operation instructions of each component module of the aircraft;

[0005] A through hole is provided in the middle of the tabletop of the maintenance platform, and the through hole is communicated with the inner cavity of the maintenance platform; an arc-shaped vertical plate is provided in the inner cavity, and a plurality of transmission devices are transmission-connected on the arc-shaped vertical plate, and a receiving slot of each transmission device is used to place one of the aircraft's component modules; the receiving slot can extend out of the through hole.

[0006] In an optional embodiment, the plurality of transmission devices include a first transmission device, a second transmission device and a third transmission device, and the first transmission device, the second transmission device and the third transmission device have the same structure;

[0007] The receiving slot of the first transmission device is used for placing the door module, the receiving slot of the second transmission device is used for placing the landing gear module, and the receiving slot of the third transmission device is used for placing the wing module.

[0008] In an optional embodiment, the first transmission device, the second transmission device and the third transmission device all include telescopic rods, and the bottom of the telescopic rods is provided with arc-shaped grooves, and the arc-shaped grooves are in contact with the arc-shaped vertical plates.

[0009] In an optional embodiment, a motor is eccentrically arranged at the bottom of the telescopic rod, and the output shaft of the motor is connected to a rubber wheel, and the rubber wheel fits the arc surface of the arc vertical plate; the telescopic end of the telescopic rod is connected to the accommodating groove.

[0010] In an optional embodiment, a limiting protrusion is respectively provided at both ends of the arc-shaped vertical plate.

[0011] In an optional embodiment, a plurality of buttons and a plurality of prompt screens are provided between the first display screen and the second display screen, wherein the prompt screen is used to display the names of the aircraft component modules; and the number of the buttons is equal to the number of the prompt screens.

[0012] In an optional embodiment, the maintenance platform is provided with a first opening door and a second opening door; the maintenance platform is also provided with a curved panel.

[0013] In an optional embodiment, a tool box and a vertical plate are respectively provided on both sides of the table top of the maintenance table, and a plurality of parts boxes are provided on the vertical plate.

[0014] The beneficial effect of the utility model is that: taking the door module, landing gear module and wing module in the aircraft as an example, the corresponding aircraft component modules are scaled down in proportion and placed in the receiving slots of each transmission device. When training on the maintenance of one of the door module, landing gear module and wing module is required, the corresponding button is pressed, and the corresponding transmission device transmits the module in the receiving slot through the through hole. At this time, the exploded view of the module and the corresponding maintenance operation instructions are respectively displayed on the first display screen and the second display screen, which is convenient to operate, effective in maintenance training and low in production cost. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0016] Figure 1 The structure of the aircraft maintenance simulation training device provided in one embodiment of the utility model is schematically shown. Figure 1 .

[0017] Figure 2 The structure of the aircraft maintenance simulation training device provided in one embodiment of the utility model is schematically shown. Figure 2 .

[0018] Figure 3 It is a top view of an aircraft maintenance simulation training device provided in one embodiment of the utility model.

[0019] Figure 4 for Figure 3 AA section view.

[0020] Figure 5 for Figure 3 Middle BB section view.

[0021] Figure 6The present invention is a schematic diagram of the structure of a transmission device in an aircraft maintenance simulation training device provided in one embodiment of the present invention.

[0022] Among them, the figure markings are: 1-maintenance table, 11-first display screen, 12-second display screen, 13-button, 14-prompt screen, 15-table top, 16-tool box, 17-vertical board, 18-parts box, 19-first opening door, 110-second opening door, 111-through hole, 112-arc panel; 2-inner cavity, 21-arc vertical board, 22-first transmission device, 23-second transmission device, 24-third transmission device, 221-telescopic rod, 222-accommodating groove, 223-rubber wheel, 224-arc groove, 225-motor. DETAILED DESCRIPTION

[0023] In order to make the technical problems, technical solutions and beneficial effects to be solved by the present invention more clearly understood, the present invention is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not used to limit the present invention.

[0024] It should be noted that when a component is referred to as being "fixed on" or "disposed on" another component, it may be directly or indirectly located on the other component. When a component is referred to as being "connected to" another component, it may be directly or indirectly connected to the other component. The directions or positions indicated by the terms "upper", "lower", "left", "right", "front", "back", "vertical", "horizontal", "top", "bottom", "inside", "outside", etc. are based on the directions or positions shown in the accompanying drawings and are only for the convenience of description and cannot be understood as limitations on the present technical solution. The terms "first" and "second" are only used for the convenience of description and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features. "Multiple" means two or more, unless otherwise clearly and specifically defined.

[0025] Please see attached Figure 1-6 The purpose of this embodiment is to provide an aircraft maintenance simulation training device, including: a maintenance platform 1, on which a first display screen 11 and a second display screen 12 are arranged, wherein the first display screen 11 is used to display an exploded view of each component module of the aircraft, and the second display screen 12 is used to display the maintenance operation instructions of each component module of the aircraft; a through hole 111 is arranged in the middle position of the table top 15 of the maintenance platform 1, and the through hole 111 is connected to the inner cavity 2 of the maintenance platform 1; an arc-shaped vertical plate 21 is arranged in the inner cavity 2, and a plurality of transmission devices are transmission-connected to the arc-shaped vertical plate 21, and a component module of each component module of the aircraft is placed in the receiving groove 222 of each transmission device; the receiving groove 222 can extend out of the through hole 111.

[0026] Specifically, the plurality of transmission devices include a first transmission device 22, a second transmission device 23 and a third transmission device 24, and the first transmission device 22, the second transmission device 23 and the third transmission device 24 have the same structure; the receiving groove 222 of the first transmission device 22 is used to place the door module, the receiving groove 222 of the second transmission device 23 is used to place the landing gear module, and the receiving groove 222 of the third transmission device 24 is used to place the wing module. The first transmission device 22, the second transmission device 23 and the third transmission device 24 all include a telescopic rod 221, and the bottom of the telescopic rod 221 is provided with an arc groove 224, and the arc groove 224 is in contact with the arc-shaped vertical plate 21. The bottom of the telescopic rod 221 is also eccentrically provided with a motor 225, and the output shaft of the motor 225 is connected to a rubber wheel 223, and the rubber wheel 223 is in contact with the arc surface of the arc-shaped vertical plate 21; the telescopic end of the telescopic rod 221 is connected to the receiving groove 222. A limiting protrusion is respectively provided at both ends of the arc-shaped vertical plate 21. When the corresponding module needs to be called, the motor 225 rotates to drive the rubber wheel 223 to rotate, and the transmission device moves along the curved vertical plate 21 by relying on the friction between the rubber wheel 223 and the curved surface of the curved vertical plate 21. When the accommodating groove 222 moves to the position of the through hole 111, the telescopic rod 221 is extended and retracted, and the corresponding aircraft component module is presented on the table 15.

[0027] In addition, a plurality of buttons 13 and a plurality of prompt screens 14 are arranged between the first display screen 11 and the second display screen 12. The prompt screen 14 is used to display the name of the aircraft component module; the number of buttons 13 is equal to the number of prompt screens 14. The maintenance platform 1 is provided with a first opening door 19 and a second opening door 110. After the doors are opened, the aircraft component module can be placed in or taken out of the receiving groove 222; the maintenance platform 1 is also provided with a curved panel 112 for the operator to stand. Tool boxes 16 and vertical boards 17 are respectively arranged on both sides of the table 15 of the maintenance platform 1. The vertical boards 17 are provided with a plurality of parts boxes 18 to provide tools and parts for maintenance trainers.

[0028] During use, taking the door module, landing gear module and wing module in the aircraft as an example, the corresponding aircraft component modules are scaled down in proportion and placed in the receiving slots 222 of each transmission device. The door module can be placed in the first transmission device 22, the landing gear module can be placed in the second transmission device 23, and the wing module can be placed in the third transmission device 24. When it is necessary to train and repair one of the door module, landing gear module and wing module, taking the repair of the door module as an example, press the button 13 corresponding to the prompt screen 14 (displaying the door module), and the first transmission device 22 will transmit the door module in the receiving slot 222 through the through hole 111. At this time, the explosion diagram of the door module and the corresponding maintenance operation instructions are respectively displayed on the first display screen 11 and the second display screen 12, which is convenient to operate, effective in maintenance training and low in production cost.

[0029] Any modifications, equivalent substitutions and improvements made within the spirit and principles of this utility model should be included in the protection scope of this utility model.

Claims

1. An aircraft maintenance simulation training device, comprising: A maintenance platform (1), wherein the maintenance platform (1) is provided with a first display screen (11) and a second display screen (12), wherein the first display screen (11) is used to display an exploded view of each component module of the aircraft, and the second display screen (12) is used to display maintenance operation instructions for each component module of the aircraft; The invention is characterized in that a through hole (111) is provided in the middle of the tabletop (15) of the maintenance platform (1), and the through hole (111) is communicated with the inner cavity (2) of the maintenance platform (1); an arc-shaped vertical plate (21) is provided in the inner cavity (2), and a plurality of transmission devices are connected to the arc-shaped vertical plate (21) in a transmission manner, and a receiving groove (222) of each of the transmission devices is used to place one of the aircraft's component modules; the receiving groove (222) can extend out of the through hole (111).

2. The aircraft maintenance simulation training device according to claim 1, characterized in that: The plurality of transmission devices include a first transmission device (22), a second transmission device (23) and a third transmission device (24), and the first transmission device (22), the second transmission device (23) and the third transmission device (24) have the same structure; The receiving slot (222) of the first transmission device (22) is used to place a door module, the receiving slot (222) of the second transmission device (23) is used to place a landing gear module, and the receiving slot (222) of the third transmission device (24) is used to place a wing module.

3. The aircraft maintenance simulation training device according to claim 2, characterized in that: The first transmission device (22), the second transmission device (23) and the third transmission device (24) all comprise a telescopic rod (221), the bottom of the telescopic rod (221) is provided with an arc-shaped groove (224), and the arc-shaped groove (224) is in contact with the arc-shaped vertical plate (21).

4. The aircraft maintenance simulation training device according to claim 3, characterized in that: A motor (225) is also eccentrically arranged at the bottom of the telescopic rod (221); the output shaft of the motor (225) is connected to a rubber wheel (223); the rubber wheel (223) fits the arc surface of the arc-shaped vertical plate (21); and the telescopic end of the telescopic rod (221) is connected to the accommodating groove (222).

5. The aircraft maintenance simulation training device according to claim 1, characterized in that: A limiting protrusion is respectively provided at both ends of the arc-shaped vertical plate (21).

6. The aircraft maintenance simulation training device according to claim 1, characterized in that: A plurality of buttons (13) and a plurality of prompt screens (14) are arranged between the first display screen (11) and the second display screen (12); the prompt screens (14) are used to display the names of the aircraft component modules; and the number of the buttons (13) is equal to the number of the prompt screens (14).

7. The aircraft maintenance simulation training device according to claim 1, characterized in that: The maintenance platform (1) is provided with a first opening door (19) and a second opening door (110); the maintenance platform (1) is also provided with a curved panel (112).

8. The aircraft maintenance simulation training device according to claim 1, characterized in that: A tool box (16) and a vertical plate (17) are respectively arranged on both sides of a table top (15) of the maintenance table (1), and a plurality of parts boxes (18) are arranged on the vertical plate (17).

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