CN113570926A - Aircraft accessory dismouting simulation trainer - Google Patents
Aircraft accessory dismouting simulation trainer Download PDFInfo
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- CN113570926A CN113570926A CN202110820933.5A CN202110820933A CN113570926A CN 113570926 A CN113570926 A CN 113570926A CN 202110820933 A CN202110820933 A CN 202110820933A CN 113570926 A CN113570926 A CN 113570926A
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- 238000004088 simulation Methods 0.000 title claims abstract description 64
- 238000012549 training Methods 0.000 claims abstract description 59
- 238000009434 installation Methods 0.000 claims abstract description 21
- 238000012544 monitoring process Methods 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 description 9
- 230000002265 prevention Effects 0.000 description 5
- 230000008569 process Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000011179 visual inspection Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000013480 data collection Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000007726 management method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000013024 troubleshooting Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000012459 cleaning agent Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
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- Electrically Operated Instructional Devices (AREA)
Abstract
The invention discloses a simulated training device for dismounting aircraft accessories, which comprises: the intelligent torque sensing module and the double-wrench dismounting intelligent simulation box; the intelligent torque sensing module comprises a cover plate simulation training object with a plurality of screws, wherein pull pressure sensors are respectively connected below the screws, the pull pressure sensors are connected with a computer, and the computer is used for monitoring the states of the pull pressure sensors; the double-wrench disassembly and assembly intelligent simulation box comprises an installation module, wherein a torque force sensor is installed at the bottom of the installation module, and the torque force sensor is connected with a computer. According to the invention, the movement and strength of the student can be imaged through the upper computer, and the student can visually see the original fuzzy concept, so that the movement of the student can be improved, and the working principle can be understood; if errors occur, the simulator can prompt and record, and later-period improved learning is facilitated.
Description
Technical Field
The invention relates to the technical field of aviation devices, in particular to a simulation training device for dismounting and mounting aircraft accessories.
Background
In the utility model patent application with application number CN200820126819.2, an instrument panel for an airplane integrated safety and training simulation system is proposed, among which mention: the training work of the aircraft comprehensive guarantee professional technical personnel can be carried out in two forms: loading training and simulation training. The actual-mounting training refers to the fact that a trained technician uses a completely real airplane to conduct comprehensive support skill training, and the simulation training refers to the fact that the trained technician uses a simulation training system designed according to airplane actual mounting to conduct comprehensive support skill training. Because the airplane is expensive and the high and new technologies are more applied, the comprehensive guarantee technology training work is carried out on the actual airplane, so that the limited service life of actual airplane equipment is consumed, and various unsafe factors are easily generated.
Taking an active main war plane as an example, the cost is low, the cost is nearly ten million yuan RMB, the cost is more, the service life is about 1000 hours, and once the service life is reached, the airplane is scrapped and can not be used any more; the service life of the airplane is inevitably consumed in the mounting training, and meanwhile, as the service life of the airplane is prolonged, the airplane can have a plurality of unexpected hidden dangers and can hurt trained personnel, so that the mounting training is not economical and safe.
Compared with the actual installation training, the simulation training can not only achieve the purpose of not losing the service life of actual installation airplane equipment, but also achieve the purpose of simulation training of airplane fault states which are difficult to carry out on the actual installation airplane, and greatly improve the quality and benefit of airplane comprehensive guarantee technology training work while saving training cost.
At present, all the control devices of the simulation training system for the comprehensive airplane guarantee almost adopt actual or simulated instruments and equipment, and have the advantages that the training device is close to a real airplane device, but the following inevitable defects exist: 1. the price is high, because the real instrument equipment is the instrument equipment used on the airplane and installed on the simulation training device, and the real instrument equipment for the airplane is very expensive, even if the instrument equipment is simulated, the price is very high, so the manufacturing cost of the whole simulation training device is very high, generally, about 100 ten thousand yuan of renowned folk coins are few, and about ten million yuan of renowned folk coins are many; 2. the simulation training device has a single function, and only can train the installed instrument after the installation of the actual instrument on the simulation training device is completed, and can not perform simulation training of working processes in various fault states, simulation training of operation of detection equipment, debugging method and part accessory disassembly and assembly training, field inquiry of maintenance data, multimedia software demonstration and the like, so that training courses are few, and training content is single; 3. the failure rate is high, maintainability is poor, the failure rate of dress instrument equipment is very high, and the personnel that is responsible for troubleshooting often do not obtain due training, and the personnel that are responsible for troubleshooting spend a large amount of time to the simulation training system carry out the maintenance of relevant instrument equipment.
Disclosure of Invention
The invention mainly aims to provide a simulated training device for dismounting an aircraft accessory, and aims to solve the technical problem that in the prior art, the force is not easy to control when a worker directly demounts the accessory.
In order to achieve the above object, the present invention provides a simulated training device for aircraft accessory disassembly, comprising: the intelligent torque sensing module and the double-wrench dismounting intelligent simulation box;
the intelligent torque sensing module comprises a cover plate simulation training object with a plurality of screws, wherein pull pressure sensors are respectively connected below the screws, the pull pressure sensors are connected with a computer, and the computer is used for monitoring the states of the pull pressure sensors;
the double-wrench disassembly and assembly intelligent simulation box comprises an installation module, wherein a torque force sensor is installed at the bottom of the installation module, and the torque force sensor is connected with a computer.
Preferably, the installation module is an installation module with three gas circuit pipe joints.
Preferably, the pull pressure sensor is connected with a first data acquisition box, and the first data acquisition box converts data uploaded by the pull pressure sensor into an RS485 signal and uploads the RS485 signal to a computer.
Preferably, the torque force sensor is connected with a second data acquisition box, and the second data acquisition box converts data uploaded by the torque force sensor into an RS485 signal and uploads the RS485 signal to a computer.
Preferably, the cover plate simulation training object is a cover plate training object with six fastening screws.
Preferably, a pre-tightening torque value is set on the aircraft accessory disassembly and assembly simulation training device, and when the actual torque value is larger than the pre-tightening torque value, an error is displayed.
In the invention, the action and the strength of the student can be imaged by the upper computer, and the student can visually see the original fuzzy concept, thus being beneficial to improving the action and understanding the working principle; if errors occur, the simulator can prompt and record, and later-period improved learning is facilitated.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
FIG. 1 is a work card diagram of the present invention;
the implementation, functional features and advantages of the objects of the present invention will be further explained with reference to the accompanying drawings.
Detailed Description
It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1, in the present embodiment, a simulated training device for aircraft accessory disassembly and assembly is provided, which includes: the intelligent torque sensing module and the double-wrench dismounting intelligent simulation box;
in this embodiment, the intelligent torque sensing module includes a cover plate simulation training object with a plurality of screws, the lower parts of the plurality of screws are respectively connected with a pull pressure sensor, the pull pressure sensors are connected with a computer, and the computer is used for monitoring the state of each pull pressure sensor;
in this embodiment, two spanner dismouting intelligence simulation box includes the installing module, torque force sensor is installed to the bottom of installing module, torque force sensor connects the computer.
In this embodiment, the installation module is an installation module with three gas circuit pipe joints.
In this embodiment, the pull pressure sensor is connected to a first data acquisition box, and the first data acquisition box converts data uploaded by the pull pressure sensor into RS485 signals and uploads the RS485 signals to a computer.
In this embodiment, the torque force sensor is connected to a second data acquisition box, and the second data acquisition box converts data uploaded by the torque force sensor into an RS485 signal and uploads the RS485 signal to a computer.
In this embodiment, the deck simulation training object is a deck training object with six fastening screws.
In this embodiment, a pre-tightening torque value is set on the aircraft accessory disassembly and assembly simulation training device, and when the actual torque value is larger than the pre-tightening torque value, an error is displayed.
Specifically, the working principle of the cover plate torque force testing module is as follows:
1. a training subject was simulated using a cover plate with 6 screws.
2. An independent tension and pressure sensor is arranged below each cover plate screw, and when the screws are tightened, the sensors can sense the tightening force of the screws, so that the students can know how much tightening force is applied to which screw.
3. The data of each sensor is collected through a data collection box and converted into RS485 signals to be uploaded to a computer, and the computer can monitor the state of each sensor in real time.
4. By monitoring the states of the sensors, the student can know whether the operation is performed sequentially according to the specified 'diagonal tightening' principle or not in the sequence of tightening the screws, and can know whether the student performs the 'diagonal pre-tightening before step-by-step force application tightening' mode or not by monitoring the tension of each sensor.
5. The movement and the strength of the student can be imaged through the upper computer, the student can visually see the original fuzzy concept, the movement of the student can be improved, and the working principle can be understood.
6. If errors occur, the simulator can prompt and record, and later-period improved learning is facilitated.
The torque force module of the double-spanner has the following functions:
1. an installation module with three gas circuit pipe joints is used as a simulated training object.
2. An independent torque force sensor is installed at the bottom of the installation module, the air channel pipe joint on the module is disassembled when a single wrench or a double wrench is used in an irregular mode, and the force generated when the pipe joint is twisted by the wrench can be transmitted to the torque force sensor at the bottom of the installation module, so that the operation of a student is not standardized.
3. When the double wrench is used correctly to disassemble the pipe joint, because the double wrenches are mutually opposite acting forces, the operating torque of the wrenches is hardly transmitted to the torque sensor at the bottom, and the trainee is indicated to be operating correctly.
4. Data of the torque sensor are collected through the data collection box and converted into RS485 signals to be uploaded to the computer, and the computer can monitor the state of the torque sensor in real time.
5. The movement and the strength of the student can be imaged through the upper computer, the student can visually see the original fuzzy concept, the movement of the student can be improved, and the working principle can be understood.
6. If errors occur, the simulator can prompt and record, and later-period improved learning is facilitated.
Specifically, the aircraft accessory disassembly and assembly simulation training further comprises the following preparation work:
(1) preparing and counting required tools;
(2) knowing the attention in construction and providing necessary labor protection tools;
(3) and preparing and arranging workplaces.
Disassembling the accessory, disassembling and assembling the simulation box cover plate:
specifically, the step of disassembling the accessory disassembly and assembly simulation box cover plate comprises the following steps:
(1) checking whether the number of the screws of the accessory dismounting simulation box is complete and clean;
(2) marking the mounting position and direction of the accessory dismounting simulation box cover plate;
(3) removing a fuse on a fixing screw of the accessory dismounting simulation box cover plate;
(4) loosening 6 fixing screws on the cover plate according to the diagonal principle;
(5) and after the fixing screw is unscrewed, the cover plate is taken down and placed in the tray.
Specifically, dismantle annex dismouting simulation box apron still includes following risk prevention and control point:
(1) placing the screws in special storage positions, and counting the number of the screws;
(2) prevent that annex dismouting simulation box apron from falling to ground.
Specifically, dismantle annex dismouting simulation box apron still including visual inspection and cleanness:
(1) visually checking whether threads at the fixed connection positions of the screws and the accessory simulation disassembly and assembly boxes are damaged or not;
(2) visual inspection of the cover plate was performed without damage and was cleaned.
Installing an accessory dismounting simulation box:
specifically, the mounting and dismounting simulation box for the accessories comprises the following steps:
(1) selecting an accessory dismounting simulation box display page in a training management system, and setting a tightening torque value and a difference value;
(2) pre-installing the accessory dismounting simulation box cover plate according to the marked position and direction;
(3) according to the diagonal assembly sequence, 6 fastening screws are pre-installed by hands and are tightened to a state with tightness, the corresponding pre-tightening torque value of the display page of the accessory simulation box is checked to be not larger than a set value, and if the fastening screws are assembled in the non-diagonal mode or the pre-tightening torque value is larger than the set value, an error prompt is given to the display page of the accessory disassembly and assembly simulation box;
(4) according to the diagonal assembly sequence, a wrench is used for tightening screws, the display page of the accessory simulation box is checked, and if the off-diagonal assembly of the tightening screws or the pre-tightening torque value is larger than a set value, the display page of the accessory disassembly and assembly simulation box presents an error prompt;
(5) and marking the mark line on the screw after the accessory simulation unpacking box is installed.
Specifically, the installation accessory dismouting simulation box still includes following risk prevention and control point:
(1) the torque wrench should avoid slipping in the using process;
(2) the torque wrench should avoid colliding with other parts during use.
Furthermore, the method also comprises the following steps of checking and cleaning the work site after completion:
(1) rechecking whether the conditions of neglected installation and neglected tightness exist;
(2) arranging workplaces and counting tools;
(3) and returning the tool.
Operational safety precautions:
(1) when the accessory assembling and disassembling simulation box is trained, the accessory assembling and disassembling simulation box is strictly assembled and disassembled according to the requirements of a work card, and the simulation box is supported by hands when the accessory assembling and disassembling simulation box is finally taken down, so that the accessory assembling and disassembling simulation box is prevented from falling down and smashing training personnel;
(2) when the safety is exercised, the nipper pliers are strictly forbidden to use to violently pull the fuse to the direction of the nipper pliers and other people, otherwise, the nipper pliers have the risk of hurting people.
Further, the fixed moment exercise includes the following preparatory tasks:
(1) preparing and counting required tools;
(2) knowing the attention in construction and providing necessary labor protection tools;
(3) and preparing and arranging workplaces.
Further, the fixed moment exercise comprises the steps of:
(1) setting a torque value of a torque wrench according to the requirement of a teacher;
(2) selecting a moment feeling page in a training management system to set a target value and a difference value;
(3) slowly screwing the torque sensing module at a constant speed by using a torque wrench;
(4) stopping screwing after the torque wrench is screwed to give out a first sound prompt sound, and performing screwing operation again until the torque wrench gives out the prompt sound;
(5) and (3) taking down the torque wrench, and checking whether the three intelligent judgment points of the torque sensing page meet the requirements (green meets the requirements, and red does not meet the requirements).
Further, the fixed moment exercise includes the following risk prevention and control points:
(1) the torque wrench should avoid slipping in the using process;
(2) the torque wrench should avoid colliding with other parts during use.
Furthermore, the method also comprises the following steps of disassembling the flaring tee pipe joint:
specifically, the disassembly of the flared tee fitting comprises the following preparatory operations:
(1) preparing and counting required tools;
(2) knowing the attention in construction and providing necessary labor protection tools;
(3) and preparing and arranging workplaces.
Specifically, the method for disassembling the flared tee pipe joint comprises the following steps:
(1) inspecting the appearance of the flared pipe joint, and having no damage, deformation and the like;
(2) cutting off the fuse by using diagonal pliers, and removing the fuse on the pipe joint by using sharp-nose pliers;
(3) sequentially loosening the pipe nuts of the pipe joint by using double wrenches;
(4) the pipe nut is unscrewed by hand, and the pipeline is disconnected;
(5) immediately plugging the pipeline port and the pipe joint by using a special plug or a sealing bag;
(6) and marking the disassembled three-way pipe joint and placing the three-way pipe joint at a specified position.
Specifically, the disassembly of the flared tee fitting comprises the following risk prevention and control points:
(1) the pipe nut and the pipe joint are prevented from being disassembled and assembled by single wrench operation;
(2) preventing unprotected direct placement of the catheter;
(3) in the process of removing the fuse, the fuse hole is prevented from being damaged, the fuse needs to be loosened firstly, and the fuse is cut off by using diagonal pliers and then removed.
Specifically, disassembling the flared tee fitting further comprises visual inspection:
(1) checking whether the pipe nut and the pipe joint have the phenomena of no damage, thread sliding and the like;
(2) and a magnifying glass is used for checking whether the bell mouth and the pipe joint are damaged or scratched.
Furthermore, the method also comprises the following steps of:
specifically, the installation of the flaring tee pipe joint comprises the following steps:
(1) taking down the plugging objects of the catheter port and the pipe joint;
(2) cleaning threads on the pipe nut and the pipe joint;
(3) connecting the conduit to the fitting: firstly, aligning and placing pipelines at two ends of a pipe joint into the bottom of the pipe joint and tightly attaching the pipelines, and then easily and smoothly screwing three pipe nuts onto the pipe joint by hands until the three pipe nuts cannot be screwed by hands;
(4) screwing the pipe joint pipe nut by using a double wrench;
(5) the tube nut is secured.
Specifically, the installation flaring tee bend coupling includes following risk prevention and control point:
(1) cleaning agents and the like are prevented from entering the inner cavity of the catheter;
(2) preventing the pipe joint from being forcibly aligned by tightening the pipe nut.
The foregoing is illustrative of the preferred embodiments of this invention, and it is to be understood that the invention is not limited to the precise form disclosed herein and that various other combinations, modifications, and environments may be resorted to, falling within the scope of the concept as disclosed herein, either as described above or as apparent to those skilled in the relevant art. And that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (6)
1. An aircraft accessory dismouting simulation trainer, its characterized in that includes: the intelligent torque sensing module and the double-wrench dismounting intelligent simulation box;
the intelligent torque sensing module comprises a cover plate simulation training object with a plurality of screws, wherein pull pressure sensors are respectively connected below the screws, the pull pressure sensors are connected with a computing device, and the computing device is used for monitoring the states of the pull pressure sensors;
the double-wrench disassembly and assembly intelligent simulation box comprises an installation module, wherein a torque force sensor is installed at the bottom of the installation module, and the torque force sensor is connected with a computing device.
2. The simulated training device for aircraft accessory disassembly as claimed in claim 1, wherein said mounting module is a mounting module with three gas circuit tube connectors.
3. The simulated training device for aircraft accessory disassembly and assembly as claimed in claim 1, further comprising a first data acquisition box, wherein the pull pressure sensor is connected with the first data acquisition box, and the first data acquisition box converts data uploaded by the pull pressure sensor into an RS485 signal and uploads the RS485 signal to the computing device.
4. The aircraft accessory disassembly and assembly simulation training device as claimed in claim 1, further comprising a second data acquisition box, wherein the torque sensor is connected with the second data acquisition box, and the second data acquisition box converts data uploaded by the torque sensor into an RS485 signal and uploads the RS485 signal to the computing device.
5. The aircraft accessory disassembly and assembly simulation training device of claim 1, wherein the cover plate simulation training object is a cover plate training object with six fastening screws.
6. The aircraft accessory disassembly and assembly simulation training device of claim 1, wherein a pretension torque value is set on the aircraft accessory disassembly and assembly simulation training device, and when the actual torque value is larger than the pretension torque value, an error is displayed.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202110820933.5A CN113570926A (en) | 2021-07-20 | 2021-07-20 | Aircraft accessory dismouting simulation trainer |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202110820933.5A CN113570926A (en) | 2021-07-20 | 2021-07-20 | Aircraft accessory dismouting simulation trainer |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9230446B1 (en) * | 2009-12-01 | 2016-01-05 | The Boeing Company | Integrated live and simulation environment system for an aircraft |
| CN105825752A (en) * | 2016-04-22 | 2016-08-03 | 吉林大学 | Force feedback device-based virtual corneal surgery training system |
| CN205881286U (en) * | 2016-03-25 | 2017-01-11 | 中山大学孙逸仙纪念医院 | Cardiopulmonary resuscitation simulates training system |
| CN108267969A (en) * | 2017-12-14 | 2018-07-10 | 广州民航职业技术学院 | A kind of aircraft composition system maintenance real training monitoring system and its implementation |
| CN209357268U (en) * | 2018-06-20 | 2019-09-06 | 长春汽车工业高等专科学校 | Torque test stand and torsional moment test system |
| CN209417958U (en) * | 2017-11-17 | 2019-09-20 | 国家电网公司 | A skill training device based on augmented reality technology |
| CN110349469A (en) * | 2019-07-21 | 2019-10-18 | 李力 | A kind of boss bolt pretightning force controlled training system of HWIL simulation |
| CN211087584U (en) * | 2019-12-09 | 2020-07-24 | 中国民航大学 | An intelligent teaching and training device for basic navigation skills |
-
2021
- 2021-07-20 CN CN202110820933.5A patent/CN113570926A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9230446B1 (en) * | 2009-12-01 | 2016-01-05 | The Boeing Company | Integrated live and simulation environment system for an aircraft |
| CN205881286U (en) * | 2016-03-25 | 2017-01-11 | 中山大学孙逸仙纪念医院 | Cardiopulmonary resuscitation simulates training system |
| CN105825752A (en) * | 2016-04-22 | 2016-08-03 | 吉林大学 | Force feedback device-based virtual corneal surgery training system |
| CN209417958U (en) * | 2017-11-17 | 2019-09-20 | 国家电网公司 | A skill training device based on augmented reality technology |
| CN108267969A (en) * | 2017-12-14 | 2018-07-10 | 广州民航职业技术学院 | A kind of aircraft composition system maintenance real training monitoring system and its implementation |
| CN209357268U (en) * | 2018-06-20 | 2019-09-06 | 长春汽车工业高等专科学校 | Torque test stand and torsional moment test system |
| CN110349469A (en) * | 2019-07-21 | 2019-10-18 | 李力 | A kind of boss bolt pretightning force controlled training system of HWIL simulation |
| CN211087584U (en) * | 2019-12-09 | 2020-07-24 | 中国民航大学 | An intelligent teaching and training device for basic navigation skills |
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