CN205451567U - A control box is used to lead in emulation for aircraft maintenance training simulator - Google Patents
A control box is used to lead in emulation for aircraft maintenance training simulator Download PDFInfo
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- CN205451567U CN205451567U CN201521134793.2U CN201521134793U CN205451567U CN 205451567 U CN205451567 U CN 205451567U CN 201521134793 U CN201521134793 U CN 201521134793U CN 205451567 U CN205451567 U CN 205451567U
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- emulation
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- inertial navigation
- aircraft maintenance
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Abstract
The utility model discloses a control box is used to lead in emulation for aircraft maintenance training simulator, include through the back lid, the airtight cavity that box body and control panel constituteed, control panel is last to be provided with a plurality of trisome mistake proofing band switch, two lamps reset key switch and signal lamp, be provided with data acquisition board in the airtight cavity, all trisome mistake proofing band switch, two lamps reset key switch and signal lamp and all are connected with data acquisition board, data acquisition board connects the digital control board, power supply converter board is connected to the digital control board, after cover and be provided with total wire terminal of CAN and power connection, the communication end and the total wire terminal of CAN of data acquisition board and digital control board are met, power supply converter board's input and power connection meet. Utilizing bus technique and data collection and control technique and method, forming and be used to lead the outside shape of control box, control function, operation, the identical emulation of instruction function with the aircraft and be used to lead the control box, technological practical application provides effective support for the analog simulation training.
Description
[technical field]
This utility model belongs to imitation technology field, is specifically related to a kind of emulation inertial navigation for aircraft maintenance training simulator and controls box.
[background technology]
The skills training work of airplane synthetic guarantee professional and technical personnel can be carried out with point two kinds of forms: actual load training and analog simulation are trained.Actual load training refers to allow the technical staff trained use the most real aircraft to carry out comprehensive coverage skill training, and analog simulation training refers to that allowing the technical staff trained use carries out comprehensive coverage skill training according to the analog simulation training system that actual load airplane design is good.Actual load aircraft carries out comprehensive coverage technical training work, not only need to consume fuel, also can consume the finite lifetime of actual load airplane equipment, and easily produce various unsafe factor, likely damaging trainee, therefore actual load training is the most uneconomical but also dangerous.Compared with actual load training, analog simulation training not only can solve problem above, and can be implemented in the analog simulation training of the airplane fault state being difficult on actual load aircraft to carry out, while saving training cost, substantially increase the quality and benefits of airplane synthetic guarantee technical training work.Therefore, aircraft maintenance analog simulation training system is utilized to carry out airplane synthetic guarantee technical training, it has also become the Main Means of aeronautical maintenance flight crew training and effective ways.
At present, the emulation passenger cabin of all aircraft maintenance analog simulation training systems nearly all have employed actual load or imitated inertial navigation controls box, its advantage is that real cockpit pressed close to by emulation passenger cabin, but there is also following inevitably shortcoming: the most expensive, requirement due to aviation safety, the reliability requirement that actual load inertial navigation controls box is the highest, necessarily makes manufacturing cost higher, even Counterfeit Item is the most expensive；2. function singleness, actual load inertial navigation controls box can not carry out the analog simulation training of malfunction work process, and therefore training content is single；3. maintainability is poor, and it is complicated that actual load inertial navigation controls this body structure of box, and connection is numerous and diverse, once breaks down, and necessarily causes inconvenient maintenance.Therefore, using actual load or imitated inertial navigation to control box and necessarily make simulated training system price increase, training function is not complete, inconvenient maintenance, is unfavorable for the universal of this advanced training means of analog simulation training and promotes.
[utility model content]
The purpose of this utility model is to provide a kind of low price, dependable performance and actual load inertial navigation to control box external shape, operating function, the on all four emulation inertial navigation control box for aircraft maintenance training simulator of mark mark.
In order to achieve the above object, this utility model includes passing through bonnet, the closed cavity that box body and control panel are formed, some three body mistake proofing band switches it are provided with on control panel, double lamp reset button switchs and signal lights, data acquisition board it is provided with in closed cavity, all three body mistake proofing band switches, double lamp reset button switchs and signal lights are all connected with data acquisition board, data acquisition board connects digital control plate, digital control plate connects power conversion board, CAN joint and power connection it is provided with on bonnet, the communication terminal of data acquisition board and numeral panel connects with CAN joint, the input of power conversion board connects with power connection.
Described bonnet is connected by some long posts that are connected with between control panel.
The described long post that connects is four, is separately fixed on four angles of bonnet, and long one end connecting post is external screw thread, and the other end is internal thread hole.
Being connected post connection on some between described data acquisition board with digital control plate, digital control plate being connected post connection with between power conversion board under some, connecting if being connected post by dry course between power conversion board with bonnet.
Described bottom connects post, lower connection post and upper connection post and is four, and it is external screw thread that bottom connects one end of post, and the other end is internal thread hole, connects post all identical with the structure that bottom connects post with upper connection post.
Described signal lights and all three body mistake proofing band switches and double lamp reset button switch are laid on control panel outer surface by four row three column matrix modes, signal lights is laid in the first row secondary series, three three mistake proofing band switches are laid in the third line respectively and respectively arrange, and six double lamp reset button switchs are laid in the second row respectively and respectively arrange and respectively arrange with fourth line.
Described CAN joint is four core quick-release couplings, and power connection is seven core quick-release couplings.
The model of described three mistake proofing band switches is 5W2D, and the model of double lamp reset button switchs is LAS3-AF-11 (X), and two warning lights are respectively white and amber, and signal lights is rectangle, amber.
The model of described collection plate is KJ-DPIN-T2V4, and the model of digital control plate is KJ-DPOUT-T2V4, and the model of power conversion board is KJ-POWER-T2V4.
The closed cavity that described bonnet, box body and control panel are constituted is cuboid.
Compared with prior art, this utility model newly utilizes bussing technique and data acquisition and control technology and method, formed and control box external shape with aircraft inertial navigation, control function, mode of operation, instruction function identical emulation inertial navigation control box, actual application for analog simulation training technique provides effectively support, has the advantages that
1, functional simulation is complete；Can all control function and instruction function by analog simulation aircraft inertial navigation control box, and mode of operation is identical with actual load；
2, training function programme-control；Control program by training software and can carry out the analog simulation training of aircraft inertial navigation system control course of normal operation and failture evacuation；
3, simple in construction, dependable performance；Use mechanics principle to design effective frame for movement, while cost not being significantly increased, it is ensured that parts connect reliable, durable, be suitable under various adverse circumstances using.
Further, this utility model used CAN joint is four core quick-release couplings, additionally it is possible to being applied to the analog simulation equipment of the weaponry training such as helicopter, naval vessel, tank, application prospect is extensive.
[accompanying drawing explanation]
Fig. 1 is parts assembling figure of the present utility model；
Fig. 2 is structural representation of the present utility model.
[detailed description of the invention]
This utility model is described further by lower combination accompanying drawing.
nullSee Fig. 1 and Fig. 2，This utility model includes by bonnet 11、The closed cavity that box body 12 and control panel 1 are formed，Some three body mistake proofing band switches 13 it are provided with on control panel 1、Double lamp reset button switchs 14 and signal lights 15，Data acquisition board 3 it is provided with in closed cavity，All three body mistake proofing band switches 13、Double lamp reset button switchs 14 and signal lights 15 are all connected with data acquisition board 3，Data acquisition board 3 connects digital control plate 5，Digital control plate 5 connects power conversion board 7，CAN joint 9 and power connection 10 it is provided with on bonnet 11，The communication terminal of data acquisition board 3 and numeral panel 5 connects with CAN joint 9，The input of power conversion board 7 connects with power connection 10，CAN joint 9 is four core quick-release couplings，Power connection 10 is seven core quick-release couplings.
It is connected post 2 by some length between bonnet 11 with control panel 1 to connect, pass through to be connected post 4 on some between data acquisition board 3 with digital control plate 5 to connect, digital control plate 5 connects by being connected post 6 under some with between power conversion board 7, connects if being connected post 8 by dry course between power conversion board 7 with bonnet 11.
Signal lights 15 and all three body mistake proofing band switches 13 and double lamp reset button switch 14 are laid on control panel outer surface by four row three column matrix modes, signal lights 15 is laid in the first row secondary series, three three mistake proofing band switches 13 are laid in the third line respectively and respectively arrange, and six double lamp reset button switchs 14 are laid in the second row respectively and respectively arrange and respectively arrange with fourth line.
Preferably, the long post 2 that connects is four, it is separately fixed on four angles of bonnet 11, long one end connecting post 2 is external screw thread, and the other end is internal thread hole, and bottom connects post 8, lower connection post 6 and upper connection post 4 and is four, it is external screw thread that bottom connects one end of post 8, the other end is internal thread hole, connects post 6 all identical with the structure that bottom connects post 8 with upper connection post 4, and external screw thread and female thread are M3.
Preferably, the model of three mistake proofing band switches 13 is 5W2D, the model of double lamp reset button switchs 14 is LAS3-AF-11 (X), two warning lights are respectively white and amber, signal lights 15 is rectangle, amber, and the model of collection plate 3 is KJ-DPIN-T2V4, the model of digital control plate 5 is KJ-DPOUT-T2V4, and the model of power conversion board 7 is KJ-POWER-T2V4.
Preferably, the closed cavity that bonnet 11, box body 12 and control panel 1 are constituted is cuboid.
During use, CAN joint 9 and power connection 10 are inserted in equipment needed thereby, three body mistake proofing band switches 13, double lamp reset button switch 14 all send data to CAN joint 9 by data acquisition board 3 and data panel 5, data acquisition board 3 and data panel 5, according to the switch data collected, control all three body mistake proofing band switches 13, double lamp reset button switch 14 and the switch of signal lights 15.
Claims (10)
- null1. the emulation inertial navigation for aircraft maintenance training simulator controls box，It is characterized in that: include by bonnet (11)、The closed cavity that box body (12) and control panel (1) are formed，Some three bodies mistake proofing band switch (13) it are provided with on control panel (1)、Double lamp reset button switchs (14) and signal lights (15)，Data acquisition board (3) it is provided with in closed cavity，All three bodies mistake proofing band switch (13)、Double lamp reset button switchs (14) and signal lights (15) are all connected with data acquisition board (3)，Data acquisition board (3) connects digital control plate (5)，Digital control plate (5) connects power conversion board (7)，CAN joint (9) and power connection (10) it is provided with on bonnet (11)，The communication terminal of data acquisition board (3) and numeral panel (5) connects with CAN joint (9)，The input of power conversion board (7) connects with power connection (10).
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterised in that: connected by some long posts (2) that are connected between described bonnet (11) with control panel (1).
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 2 controls box, it is characterized in that: the described long post (2) that connects is four, it is separately fixed on four angles of bonnet (11), long one end connecting post (2) is external screw thread, and the other end is internal thread hole.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterized in that: between described data acquisition board (3) with digital control plate (5), on some, be connected post (4) connection, connect by being connected post (6) under some between digital control plate (5) with power conversion board (7), power conversion board (7) with bonnet (11) if between be connected post (8) connection by dry course.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 4 controls box, it is characterized in that: described bottom connects post (8), lower connection post (6) and upper connection post (4) and is four, it is external screw thread that bottom connects one end of post (8), the other end is internal thread hole, connects post (6) all identical with the structure that bottom connects post (8) with upper connection post (4).
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterized in that: described signal lights (15) and all three bodies mistake proofing band switch (13) and double lamp reset button switch (14) are laid on control panel outer surface by four row three column matrix modes, signal lights (15) is laid in the first row secondary series, three three mistake proofing band switches (13) are laid in the third line respectively and respectively arrange, and six double lamp reset button switchs (14) are laid in the second row respectively and respectively arrange and respectively arrange with fourth line.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterised in that: described CAN joint (9) is four core quick-release couplings, and power connection (10) is seven core quick-release couplings.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 6 controls box, it is characterized in that: the model of described three mistake proofing band switches (13) is 5W2D, the model of double lamp reset button switchs (14) is LAS3-AF-11 (X), two warning lights are respectively white and amber, signal lights (15) is rectangle, amber.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterized in that: the model of described collection plate (3) is KJ-DPIN-T2V4, the model of digital control plate (5) is KJ-DPOUT-T2V4, and the model of power conversion board (7) is KJ-POWER-T2V4.
- A kind of emulation inertial navigation for aircraft maintenance training simulator the most according to claim 1 controls box, it is characterised in that: the closed cavity that described bonnet (11), box body (12) and control panel (1) are constituted is cuboid.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521134793.2U CN205451567U (en) | 2015-12-30 | 2015-12-30 | A control box is used to lead in emulation for aircraft maintenance training simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521134793.2U CN205451567U (en) | 2015-12-30 | 2015-12-30 | A control box is used to lead in emulation for aircraft maintenance training simulator |
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| Publication Number | Publication Date |
|---|---|
| CN205451567U true CN205451567U (en) | 2016-08-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521134793.2U Expired - Fee Related CN205451567U (en) | 2015-12-30 | 2015-12-30 | A control box is used to lead in emulation for aircraft maintenance training simulator |
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| CN (1) | CN205451567U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109903635A (en) * | 2017-12-11 | 2019-06-18 | 青岛飞鹰仿真科技有限公司 | A kind of modular simulation device cockpit |
-
2015
- 2015-12-30 CN CN201521134793.2U patent/CN205451567U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109903635A (en) * | 2017-12-11 | 2019-06-18 | 青岛飞鹰仿真科技有限公司 | A kind of modular simulation device cockpit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160810 Termination date: 20181230 |