CN116030683A - Mechanical dismounting system and use method thereof - Google Patents
Mechanical dismounting system and use method thereof Download PDFInfo
- Publication number
- CN116030683A CN116030683A CN202310196074.6A CN202310196074A CN116030683A CN 116030683 A CN116030683 A CN 116030683A CN 202310196074 A CN202310196074 A CN 202310196074A CN 116030683 A CN116030683 A CN 116030683A
- Authority
- CN
- China
- Prior art keywords
- disassembly
- assembly
- module
- control module
- simulated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention discloses a mechanical dismounting system and a use method thereof, wherein the mechanical dismounting system comprises: the display module is used for displaying the simulated disassembly and assembly scene transmitted by the control module, collecting the interaction result of the crew and transmitting the interaction result to the control module, and displaying the conclusion given by the control module; the control module is used for generating and analyzing the simulated disassembly and assembly scene, transmitting the generated simulated disassembly and assembly scene to the display module, transmitting the analyzed simulated disassembly and assembly scene data to the simulation panel, comparing and analyzing the interaction result and the switch signal with a preset sequence according to the receiving sequence to obtain a conclusion, and transmitting the conclusion to the display module; the simulation panel is used for adjusting corresponding parameters on the simulation panel to be consistent with the simulated disassembly scene data, collecting switching signals of each loop on the simulation panel and transmitting the switching signals to the control module. The invention can solve the problems that the existing mechanical dismounting system has no universality and is inconvenient for the crew to comprehensively exercise.
Description
Technical Field
The invention belongs to the field of aviation engineering training, and particularly relates to a mechanical disassembly and assembly system and a use method thereof.
Background
There are generally two methods of training aircraft crews. For practical training, the crew needs to operate and practice on a real airplane, and for simulation training, simulation equipment is adopted to replace real airplane equipment, and the crew operates and practices on the simulation equipment.
Aircraft is a very accurate device and is expensive, and the price of a passenger aircraft can reach billions. During the assembly training, the service life of the aircraft is affected because the operation of the crew is not skilled or the crew is not familiar with the equipment and the aircraft is easily damaged. However, the new mobile phone staff has a process from strange to familiar in operation, so that the fault tolerance rate of the real training is low, and the training is inconvenient.
The inventor finds that in the practical use process, at least the following technical problems exist in the prior art:
different aircraft models have certain differences in specific operation panels or circuit structures, but existing simulation equipment only aims at a specific structure or subsystem, and if other structures or subsystems need to be exercised, related structures can be detached from the aircraft. However, the repeated operation process exists in practice, the related structure is disassembled and assembled from the airplane, the cost is high, and only one structure can be operated at a time, so that the comprehensive practice of the crew is inconvenient.
Disclosure of Invention
In order to overcome the defects, the inventor of the invention continuously reforms and innovates through long-term exploration attempts and multiple experiments and efforts, and provides a mechanical disassembly and assembly system and a use method thereof, which can solve the problems that the conventional mechanical disassembly and assembly system has no universality and is inconvenient for the crew to comprehensively exercise.
The technical scheme adopted by the invention for achieving the purpose is as follows: there is provided a mechanical disassembly and assembly system comprising: the display module is connected with the control module and is used for displaying the simulated disassembly and assembly scene transmitted by the control module, collecting the interaction result of the crew and transmitting the interaction result to the control module and displaying the conclusion given by the control module; the control module is used for generating and analyzing the simulated disassembly and assembly scene, transmitting the generated simulated disassembly and assembly scene to the display module, transmitting the analyzed simulated disassembly and assembly scene data to the simulation panel, comparing and analyzing the interaction result and the switch signal with a preset sequence according to the receiving sequence to obtain a conclusion, and transmitting the conclusion to the display module; the simulation panel is connected with the control module and used for adjusting corresponding parameters on the simulation panel to be consistent with the simulated disassembly scene data, collecting switching signals of each loop on the simulation panel and transmitting the switching signals to the control module.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the simulated disassembly scene simulates pipelines, circuits and circuits of the airborne electronic cabin and the electric connector, and the simulated disassembly scene data comprises the on-off of a loop, the state of an indicator lamp and the response of a button.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the analog panel includes: the system comprises a pipeline dismounting module, a cable dismounting module and an airborne equipment dismounting module, wherein a plurality of metal pipelines are arranged on the pipeline dismounting module, and the metal pipelines are connected with a control module to form a loop; the cable disassembly and assembly module is provided with a plurality of cables, and the cables are connected with the control module to form a loop; and the airborne equipment module is provided with airborne equipment, and the airborne equipment is connected with the control module to form a loop.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the on-off of each loop in the pipeline disassembly and assembly module, the on-off of each loop in the cable disassembly and assembly module and the on-off of each loop in the airborne equipment are consistent with the simulated disassembly and assembly scene data.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the system also comprises a storage module which is connected with the control module, wherein the control module calculates the score according to the obtained conclusion, and the storage module is used for storing the score calculated by the control module.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the simulation panel is a rectangular shell, and a mounting plate is horizontally arranged in the simulation panel to divide the simulation panel into a pipeline mounting area and an airborne equipment mounting area.
According to the mechanical disassembly and assembly system, a further preferable technical scheme is as follows: the display module is a touch screen.
A method of using a mechanical disassembly and assembly system, comprising the steps of: selecting a corresponding simulated disassembly scene on the display module; and operating the interactive interface and the simulation panel on the display module according to the corresponding sequence, so that the final conclusion is displayed on the display screen.
The application method of the mechanical disassembly and assembly system comprises the following steps of: the simulated disassembly and assembly scene comprises pipeline disassembly and assembly, cable disassembly and assembly and airborne equipment disassembly and assembly.
The application method of the mechanical disassembly and assembly system comprises the following steps of: if the selected simulated disassembly and assembly scene is pipeline disassembly and assembly, closing a valve on an interactive interface and disassembling and assembling corresponding pipelines according to an instruction of an operation manual displayed on a display module; if the selected simulated disassembly and assembly scene is cable disassembly and assembly, closing a control switch on the interactive interface and disassembling and assembling corresponding cables according to an instruction of an operation manual displayed on the display module; if the selected simulated dismounting scene is the dismounting of the airborne equipment, the jump switch on the interactive interface and the dismounting of the airborne equipment are closed according to the instruction of the operation manual displayed on the display module.
Compared with the prior art, the technical scheme of the invention has the following advantages/beneficial effects:
the invention is provided with the display module, the control module and the simulation panel, combines the actual maintenance condition, directly selects the simulation disassembly and assembly scene to be exercised on the display module by the crew member in a targeted way, can be disassembled and assembled on the simulation panel after the simulation scene is selected, compares and analyzes the operation sequence of the crew member with the preset sequence, and feeds back the conclusion of whether the operation sequence is correct or not to the crew member. The simulation panel provided by the invention can be used for practicing various disassembly and assembly, has certain universality, can be suitable for most disassembly and assembly structures on an airplane, and is convenient for crews to practice.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some embodiments of the present invention and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic illustration of the connection of a mechanical disassembly system of the present invention.
Fig. 2 is a schematic structural view of the analog panel of the present invention.
The marks in the figure are respectively: the device comprises a display module 1, a control module 2, a simulation panel 3 and a storage module 4; a 31 pipeline dismounting module, a 32 cable dismounting module, a 33 airborne equipment dismounting module and a 34 mounting plate; 311 metal pipeline, 312 pipeline interface, 322 cable connector, 331 on-board equipment, 332 locker.
Detailed Description
To make the objects, technical solutions and advantages of the present invention more apparent, the technical solutions in the embodiments of the present invention will be clearly and completely described below, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments. All other embodiments, based on the embodiments of the invention, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the invention. Accordingly, the detailed description of the embodiments of the invention provided below is not intended to limit the scope of the invention as claimed, but is merely representative of selected embodiments of the invention.
It should be noted that: like reference numerals and letters denote like items in the following figures, and thus, once an item is defined in one figure, it may not be further defined and explained in the following figures.
Examples:
as shown in fig. 1, a mechanical disassembly and assembly system includes: a display module 1, a storage module 4, a control module 2 and an analog panel 3. The display module 1, the storage module 4 and the analog panel 3 are all connected with the control module 2.
The display module 1 is a touch screen and is connected with the control module 2, and is used for displaying an interaction interface, recording interaction results of crews and transmitting the interaction results to the control module 2 in sequence. The simulation disassembly and assembly scene on the display module 1 generally aims at disassembly and assembly of pipelines, cables and disassembly and assembly of airborne equipment 331 on an airborne electronic cabin and an electric connector, and comprises a pipeline diagram, a circuit diagram, a cable diagram, an operation manual and the like. The crew operates the interactive interface according to the indication on the display module 1 to obtain the interactive result, the display module 1 transmits the interactive result to the control module 2, and then the conclusion fed back by the control module 2 is displayed.
After the crew selects the corresponding simulated disassembly and assembly scene, the simulation panel 3 is needed. The simulation panel 3 is connected with the control module 2, and is used for receiving the simulation disassembly and assembly scene data transmitted by the control module 2, correspondingly adjusting parameters on the simulation panel 3, and collecting switching signals of all channels on the simulation panel 3.
As shown in fig. 2, the analog panel 3 is provided with a pipeline dismounting module 31, a cable dismounting module 32 and an on-board equipment dismounting module 33. The simulation panel 3 is of a cuboid structure, and a mounting plate 34 is horizontally arranged in the simulation panel 3, so that the interior of the simulation panel 3 is divided into an upper pipeline mounting area and a lower airborne equipment mounting area. The upper end opening of the simulation panel 3 is communicated with the pipeline installation area and is provided with a detachable cover, and the pipeline dismounting module 31 is arranged in the pipeline installation area and is used for simulating a narrow space on an aircraft. The side wall of one end of the simulation panel 3 is open and is communicated with an airborne equipment installation area, and the airborne equipment 331 is installed in the airborne equipment installation area. The cable dismounting module 32 is mounted on the side wall of the analog panel 3.
The pipeline dismounting module 31 is provided with a plurality of metal pipelines 311 and a plurality of pipeline interfaces 312, when the metal pipelines 311 are connected to the pipeline interfaces 312, the metal pipelines are communicated with the control module 2 to form a loop, the metal pipelines 311 are used as a part of a passage, the passage is disconnected when the metal pipelines are removed, and the passage is connected when the metal pipelines are installed. The plurality of metal pipes 311 may form a plurality of loops, and by detecting switching signals of the respective loops, it is possible to determine which metal pipe 311 is attached or detached by a crew.
The cable assembly and disassembly module 32 is provided with a plurality of cables and cable connectors 322, and the cable assembly and disassembly module 32 is similar to the pipeline assembly and disassembly module 31. When the cable is connected to the cable connector 322, the circuit connected to the control module 2 is closed, and when the cable is not connected to the cable connector 322, the circuit connected to the control module 2 is opened. The plurality of cables can form a plurality of loops, and by detecting the switch signals of all loops, the operator can determine which cable is disassembled and assembled.
The airborne equipment 331 module comprises a thimble, airborne equipment 331 and a metal tag, and the thimble is connected with the control module 2. When the airborne equipment 331 is mounted on the simulation panel 3, the ejector pins shrink, the airborne equipment 331 is connected with the control module 2 through the ejector pins, and the loop of the airborne equipment 331 and the control module 2 is communicated; when the on-board device 331 is removed from the analog panel 3, the ejector pins are released, and the loop of the on-board device 331 and the control module 2 is disconnected, that is, by detecting the switch signals of the loop of the on-board device 331 and the control module 2, whether the on-board device 331 is removed or not can be determined.
The on-board device 331 is provided with a button, a knob and an indicator lamp, a plurality of lockers 332 are further arranged in front of the on-board device 331, and after the on-board device 331 is disassembled, a metal hanging tag is required to be hung on the lockers 332. The metal tag can be conductive, and is a part of a connected related loop, when the metal tag is hung on the locker 332, the related loop connected with the control module 2 is connected, and the control module 2 can receive a related switch signal of the loop, that is, can determine whether the crew has the metal tag hung or not, and at which position the crew hangs.
The storage module 4 is connected with the control module 2. The control module 2 compares and analyzes the interaction result and the switch signal according to the received operation sequence and a preset sequence to obtain a conclusion about whether the operation sequence is correct or not, the achievement of the computer staff can be calculated through the conclusion, and the storage module 4 is used for storing the achievement.
The display module 1, the storage module 4, the control module 2 and the like form a central control computer controlled by an embedded circuit board, the scene to be simulated is decomposed into embedded data through internal data analysis, and the embedded data is output to the simulation panel 3 through a wired circuit. The pipeline dismounting module 31, the cable dismounting module 32 and the airborne equipment dismounting module 33 on the simulation panel 3 are all connected with the embedded circuit board in a wired mode.
A method of using a mechanical disassembly and assembly system, comprising the steps of:
after the simulation disassembly and assembly scene is selected on the display module 1, the display module 1 displays a corresponding interactive interface and indicates a designated area on the simulation panel 3;
the crew operates the interactive interface and the simulation panel 3 according to a certain sequence, the operation sequence is obtained after the operation is completed, and the control module 2 compares the operation sequence with a preset sequence to obtain a conclusion of whether the operation sequence is correct or not;
and the crew selects the simulated disassembly and assembly scene, and repeats the process until the simulation is stopped, so as to obtain the final result.
Specifically, if the simulation disassembly and assembly scene selected by the crew is pipeline disassembly and assembly, a pipeline diagram and an operation manual capable of achieving man-machine interaction are displayed on the display module, and an operable area on the pipeline disassembly and assembly module 31 is specified to form a specified area.
The crew reads the operation manual, closes the valve on the pipeline diagram according to the instruction, and dismounts relevant pipeline in the appointed region to form the operation sequence, and the control module 2 records the operation sequence, compares the operation sequence with the preset sequence, and obtains the conclusion of whether the operation sequence is correct or not.
If the simulation disassembly and assembly scene selected by the crew is cable disassembly and assembly, displaying a cable diagram and an operation manual which can be subjected to man-machine interaction on the display module, and designating an operable area of the cable disassembly and assembly module to form a designated area.
The crew reads the operation manual, closes the empty switch on the cable map according to the instruction, and dismounts the relevant cable in the appointed area to form the operation sequence, the control module 2 records the operation sequence, compares the operation sequence with the preset sequence, and obtains the conclusion that whether the operation sequence is correct or not.
If the simulation disassembly scene selected by the crew is disassembly of the airborne equipment 331, a circuit diagram and an operation manual which can be interacted with each other are displayed on the display module, and an operable area of the airborne equipment 331 (which locker 332 the specified metal tag is hung on) is specified, so that a specified area is formed.
The crew reads the operation manual, closes the jump switch on the circuit diagram according to the instruction, hangs the metal hang-up card in the appointed area, forms the operation sequence, and control module 2 records the operation sequence, compares the operation sequence with the order of predetermineeing, obtains the conclusion that whether the operation sequence is correct.
It should be noted that the present invention can record the operation sequence, and the incomplete operation or the operation not in the sequence of the operation manual are regarded as the wrong sequence.
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the apparatus or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
The foregoing is merely a preferred embodiment of the present invention, and it should be noted that the above-mentioned preferred embodiment should not be construed as limiting the invention, and the scope of the invention should be defined by the appended claims. It will be apparent to those skilled in the art that various modifications and adaptations can be made without departing from the spirit and scope of the invention, and such modifications and adaptations are intended to be comprehended within the scope of the invention.
Claims (10)
1. A mechanical disassembly and assembly system, comprising:
the display module is connected with the control module and is used for displaying the simulated disassembly and assembly scene transmitted by the control module, collecting the interaction result of the crew and transmitting the interaction result to the control module and displaying the conclusion given by the control module;
the control module is used for generating and analyzing the simulated disassembly and assembly scene, transmitting the generated simulated disassembly and assembly scene to the display module, transmitting the analyzed simulated disassembly and assembly scene data to the simulation panel, comparing and analyzing the interaction result and the switch signal with a preset sequence according to the receiving sequence to obtain a conclusion, and transmitting the conclusion to the display module;
the simulation panel is connected with the control module and used for adjusting corresponding parameters on the simulation panel to be consistent with the simulated disassembly scene data, collecting switching signals of each loop on the simulation panel and transmitting the switching signals to the control module.
2. The mechanical disassembly and assembly system of claim 1, wherein the simulated disassembly and assembly scenario simulates the piping, wiring and circuitry of the on-board electronics compartment and electrical connector, and the simulated disassembly and assembly scenario data includes the on-off of the loop, status of the indicator lights and button reactions.
3. The mechanical disassembly and assembly system of claim 2, wherein the analog panel includes: the system comprises a pipeline dismounting module, a cable dismounting module and an airborne equipment dismounting module, wherein a plurality of metal pipelines are arranged on the pipeline dismounting module, and the metal pipelines are connected with a control module to form a loop; the cable disassembly and assembly module is provided with a plurality of cables, and the cables are connected with the control module to form a loop; and the airborne equipment module is provided with airborne equipment, and the airborne equipment is connected with the control module to form a loop.
4. A mechanical disassembly and assembly system according to claim 3 wherein the on-off of each circuit in the pipeline disassembly and assembly module, the on-off of each circuit in the cable disassembly and assembly module, and the on-off of each circuit in the on-board equipment are consistent with simulated disassembly and assembly scenario data.
5. The machine disassembly and assembly system of claim 4, further comprising a storage module coupled to the control module, the control module calculating the performance based on the reached conclusion, the storage module configured to store the performance calculated by the control module.
6. The mechanical dismounting system of claim 5 wherein the analog panel is a rectangular housing, and a mounting plate is horizontally disposed inside the analog panel to divide the analog panel into a pipeline mounting area and an on-board equipment mounting area.
7. The mechanical disassembly and assembly system of claim 6, wherein the display module is a touch screen.
8. A method of using a mechanical disassembly and assembly system, comprising the steps of:
s1: selecting a corresponding simulated disassembly scene on the display module;
s2: and operating the interactive interface and the simulation panel on the display module according to the corresponding sequence, so that the final conclusion is displayed on the display screen.
9. The method of claim 8, wherein the simulated assembly and disassembly scenarios include pipeline assembly and disassembly, cable assembly and on-board equipment assembly and disassembly.
10. The method of claim 9, wherein if the selected simulated disassembly scene is pipe disassembly, closing the valve on the interactive interface and disassembling the corresponding pipe according to an instruction of an operation manual displayed on the display module; if the selected simulated disassembly and assembly scene is cable disassembly and assembly, closing a control switch on the interactive interface and disassembling and assembling corresponding cables according to an instruction of an operation manual displayed on the display module; if the selected simulated dismounting scene is the dismounting of the airborne equipment, the jump switch on the interactive interface and the dismounting of the airborne equipment are closed according to the instruction of the operation manual displayed on the display module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310196074.6A CN116030683A (en) | 2023-03-03 | 2023-03-03 | Mechanical dismounting system and use method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310196074.6A CN116030683A (en) | 2023-03-03 | 2023-03-03 | Mechanical dismounting system and use method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116030683A true CN116030683A (en) | 2023-04-28 |
Family
ID=86079688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310196074.6A Pending CN116030683A (en) | 2023-03-03 | 2023-03-03 | Mechanical dismounting system and use method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116030683A (en) |
-
2023
- 2023-03-03 CN CN202310196074.6A patent/CN116030683A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2510556C (en) | Method and system for simulation-based troubleshooting and fault verification in operator-controlled complex systems | |
| KR101418484B1 (en) | Virtual training simulator and method of aircraft maintenance education using the same | |
| CN202632580U (en) | Integrated training simulator of flight and ejector of airplane | |
| CN111210696B (en) | Teaching control end simulator, student end simulator and radar equipment comprehensive training simulation system | |
| CN109697903A (en) | A kind of substation relay protection safety practical training method based on VR | |
| CN101620800A (en) | 500 KV substation analog simulation training system | |
| CN102881202A (en) | Virtual reality based on-load tap switch maintenance training method | |
| CN110189568A (en) | A kind of substation simulation system and method based on virtual reality technology | |
| CN109712461A (en) | A kind of aircraft maintenance virtual training system | |
| CN106251761A (en) | A kind of automobile electric appliance circuit Internet of Things controlled in wireless teaching system | |
| CN111145612A (en) | Aviation aircraft work simulation training device | |
| CN116030683A (en) | Mechanical dismounting system and use method thereof | |
| CN112071161A (en) | Aircraft fuel system simulation training teaching device | |
| CN106448320A (en) | Internet of Things wireless control teaching system of automotive electronic power steering | |
| US11417239B1 (en) | Electrical circuit training device and method | |
| JPH1039728A (en) | Plant simulator | |
| CN108873777A (en) | A kind of ground test launch control system monitor supervision platform and monitoring method | |
| CN113706967A (en) | Comprehensive simulation maintenance training system for engineering | |
| CN116071978A (en) | Electronic simulation cabin simulation training system and application method thereof | |
| CN201251859Y (en) | Instrument panel for airplane integrated-support simulated training system | |
| CN202306315U (en) | Comprehensive test platform of electronic control system of excavator | |
| CN108281060B (en) | A emulation cabin panel module for flight simulation | |
| CN105303951A (en) | Turbocharger engine practical training table | |
| CN219626167U (en) | Height measurement radar simulation training equipment | |
| CN111739378A (en) | System and process of cognitive power supply screen based on VR |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |