CN208269730U - Rocket gun control equipment detection maintenance training device - Google Patents
Rocket gun control equipment detection maintenance training device Download PDFInfo
- Publication number
- CN208269730U CN208269730U CN201820815926.XU CN201820815926U CN208269730U CN 208269730 U CN208269730 U CN 208269730U CN 201820815926 U CN201820815926 U CN 201820815926U CN 208269730 U CN208269730 U CN 208269730U
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- China
- Prior art keywords
- launching
- tube group
- launching tube
- flat pad
- support shaft
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- 238000001514 detection method Methods 0.000 title abstract description 10
- 238000012423 maintenance Methods 0.000 title abstract 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 17
- 238000007363 ring formation reaction Methods 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 6
- 230000008859 change Effects 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000004088 simulation Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000009955 peripheral mechanism Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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Abstract
The utility model discloses a rocket gun control equipment detection and maintenance training device, which comprises a base, wherein a launching platform is arranged above the base, and a plurality of supporting devices are directly arranged on the base and the launching platform; a launching cylinder group and a direction control device for controlling the launching cylinder group are arranged above the launching platform; the control device comprises a transmitting cylinder group supporting shaft; the launching cylinder group is connected with the upper end of the supporting shaft of the launching cylinder group; the lower end of the supporting shaft of the launching cylinder group is rotatably connected with the launching platform; the control device also comprises a motor, the motor is arranged on the launching platform, and an output shaft of the motor is in transmission connection with the launching cylinder group support shaft; the control device also comprises a rotary encoder, and a coded disc of the rotary encoder is in transmission connection with the transmitting cylinder group supporting shaft through a closed annular conveying belt. The utility model can connect the rotary encoder and each hydraulic cylinder through the controller; the launching direction of the launching platform on the horizontal plane and the launching angle of the launching platform on the vertical plane can be adjusted in the above mode.
Description
Technical field
The utility model relates to weaponry control technologies, in particular to a kind of training of rocket gun big gun control equipment Measuring error
Device.
Background technique
With the modernization construction process of army of China, the level of informatization of rocket gun is gradually increased, to the skill of fighter
Art requires very high.It operating by actual load merely, the relevant technologies could skillfully be grasped by generally requiring operation training 2 to three years, and
And careless slightly be easy to cause equips damage.In current rocket gun training, limiting vulnerable to space-time influences, and pole is lost in actual load
Greatly.Therefore urgently one kind can imitate the rocket gun attitude-control device of rocket gun operational scenarios.
Summary of the invention
Technical problem to be solved in the utility model be in view of the above shortcomings of the prior art, the utility model proposes
A kind of rocket gun big gun control equipment Measuring error training device.
The technical solution that the utility model solves above-mentioned technical problem is as follows:
A kind of rocket gun big gun control equipment Measuring error training device, including pedestal, it is flat that the pedestal top is provided with transmitting
Platform is provided with several support devices between the pedestal and the flat pad；
Launching tube group and the direction-control apparatus for controlling the launching tube group are provided with above the flat pad；
The control device includes launching tube group support shaft；
The launching tube group is connected with the launching tube group support shaft upper end；The launching tube group support shaft lower end and institute
State flat pad rotation connection；
The control device further includes motor, and the motor is arranged in the flat pad, the output shaft of the motor
It is sequentially connected with the launching tube group support shaft；
The control device further includes rotary encoder, the biography that the code-disc of the rotary encoder passes through closed annular
Band is sent to be sequentially connected with the launching tube group support shaft.
Further, the control device further includes tensioner；
The tensioner include tension roller, connecting rod, be fixedly connected on the flat pad upper surface U-shaped limit
Position slot and reset spring.
The tension roller and the conveyer belt, which roll, to be cooperated；One end of the connecting rod and the tension roller are rotatablely connected,
The other end is inserted into the interior of the limiting slot and connect with one end of the reset spring；The other end of the reset spring and institute
State the connection of limiting slot inner wall.
Further, the support device includes the upper hinged ear being fixedly connected with the flat pad lower end surface and institute
State the lower hinged ear and hydraulic cylinder that pedestal upper surface is fixedly connected；The hydraulic cylinder includes the liquid with the rotation connection of lower hinged ear
Cylinder pressure fixing end and the hydraulic cylinder movable end being rotatablely connected with the upper hinged ear.
The utility model proposes a kind of rocket gun big gun control equipment Measuring error training devices, are connected and are rotated by controller
Formula encoder and each hydraulic cylinder；Through the above way the direction of the launch on the horizontal level of adjustable flat pad with
And the launch angle on perpendicular, and recorded the current direction of the launch of flat pad by rotary encoder, it is
The operations such as analog transmissions, the training and examination of rocket launcher system fire provide physical platform.
Detailed description of the invention
Fig. 1 is the utility model overall structure diagram；
Fig. 2 is direction-control apparatus overlooking structure diagram in Fig. 1；
Fig. 3 is the enlarged diagram of the support device of Fig. 1；
Fig. 4 is the enlarged diagram of tensioner in Fig. 2；
Fig. 5 is the control logic schematic diagram of the utility model.
In figure: pedestal 1；Support device 2；Upper hinged ear 2.1；Lower hinged ear 2.2；Hydraulic cylinder fixing end 2.3；Hydraulic cylinder is living
Moved end 2.4；Flat pad 3；Launching tube group 4；Direction-control apparatus 5；Launching tube group support shaft 5.1；Rotary encoder 5.2；
Tensioner 5.3；Tension roller 5.31: connecting rod 5.32；Limiting slot 5.33；Reset spring 5.34；Conveyer belt 5.4.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figure 1, a kind of rocket gun big gun control equipment Measuring error training device, including pedestal 1, it is arranged above pedestal 1
There is flat pad 3, several support devices 2 are provided between pedestal 1 and flat pad 3；
Preferably, pedestal 1 and flat pad 3 are in the close cuboid of area shape, and 4 settings of support devices 2 exist
Launching tube group 4 and the direction-control apparatus 5 for controlling launching tube group 4 are provided with above flat pad 3；Control
Device 5 includes launching tube group support shaft 5.1；
As shown in Fig. 2, launching tube group 4 is connected with 5.1 upper end of launching tube group support shaft；Under launching tube group support shaft 5.1
End is rotatablely connected with flat pad 3；
Control device 5 further includes motor, and motor is inserted to be arranged in 3 upper surface of flat pad, the output shaft and hair of motor
Shooting cylinder group support shaft 5.1 is sequentially connected.
Preferably, the power output shaft of motor and launching tube group support shaft 5.1 are coaxially arranged.
Control device 5 further includes rotary encoder 5.2, the biography that the code-disc of rotary encoder 5.2 passes through closed annular
Band 5.4 and launching tube group support shaft 5.1 is sent to be sequentially connected.
Control device 5 further includes tensioner 5.3；
As shown in figure 4, tensioner 5.3 includes tension roller 5.31, connecting rod 5.32, is fixedly connected on flat pad 3
The limiting slot 5.33 and reset spring 5.34 of the U-shaped of end face；
Tension roller 5.31 and conveyer belt 5.4, which roll, to be cooperated；One end of connecting rod 5.32 and tension roller 5.31 are rotatablely connected, separately
One end is inserted into the interior of limiting slot 5.33 and connect with one end of reset spring 5.34；The other end of reset spring 5.34 and limit
The connection of 5.33 inner wall of slot.I.e. the other end of reset spring 5.34 is fixedly connected with 5.33 inner wall bottom of limiting slot.
In this way by tensioner 5.3, it ensure that conveyer belt 5.4 is able to maintain enough tension, so that rotary encoder
Device 5.2 can accurately record the case where launching tube group support shaft 5.1 rotates.
Preferably, the radius of launching tube group support shaft 5.1 is greater than 2 times of 5.2 code-disc of rotary encoder, in this way once sending out
Shooting cylinder group support shaft 5.1, which rotates a lesser angle, just can make rotary encoder 5.2 rotate biggish angle, convenient for rotation
Rotatable encoder 5.2 improves the accuracy of record.
It preferably, can be rapid after rotary encoder 5.2 makes whole device power-off restarting using absolute type encoder
Determine current launching tube group support shaft 5.1 towards angle rather than can only obtain launching tube group support shaft 5.1 this training/
Relative rotation angle during simulation/real training.
As shown in figure 3, support device 2 includes the upper hinged ear 2.1 being fixedly connected with 3 lower end surface of flat pad and pedestal 1
The lower hinged ear 2.2 and hydraulic cylinder that upper surface is fixedly connected；Hydraulic cylinder includes the hydraulic cylinder with the rotation connection of lower hinged ear 2.2
Fixing end 2.3 and the hydraulic cylinder movable end 2.4 being rotatablely connected with upper hinged ear 2.1.
Preferably, hydraulic cylinder as shown in Fig. 5 is the circuit control schematic diagram of the utility model.The utility model passes through place
Device control hydraulic cylinder and motor are managed, and is connected with encoder, is the power supply of each functional component by power supply.
(1) power module
Voltage needed for providing work needs straight including AC and DC voltage peace platform needed for driving peripheral execution unit
Galvanic electricity pressure.
(2) control cabinet workbench
The interface of control cabinet circuit unit is provided, while reserving fault setting interface, circuit shape can be changed by the module
State (mainly switching), simulated failure phenomenon, and reserve for detection mouth needed for the detection of external detection instrument.
(3) control platform is detected
Control cabinet Work Incentive signal and control signal are provided, the function presentation to control cabinet and fault detection are able to achieve,
And provide Function detection individual event selection and automatically two kinds of control modes of detection.
(4) Peripheral component interface platform
It is made of lighting demonstration platform, execution unit driving interface and fault setting interface three parts.Lighting demonstration platform
For showing the action state demonstration of the peripheral mechanism of line conduction state and part；Execution unit driving is mainly used for driving existing
Comprehensive simulation training aids；Fault setting interface connecting fault setup module, can be changed by the module circuit state (it is logical,
It is disconnected), simulated failure phenomenon.
(5) display platform
It is shown for test result, and query function is provided；Being capable of providing the demonstration of control cabinet working principle (follows detection to become
Change) and interface unit for electrical property parameters/state, and fault element and detection method are prompted according to testing result.
(6) fault setting module
By way of sealing in, the input of control control cabinet, the change of output parameter (state) change circuit state or periphery
The state of component, to realize the demonstration to phenomenon of the failure.
(7) peripheral components
Here mainly for the existing comprehensive simulation training aids in my room, the switching of mode of operation is set, controls corresponding mechanism
Movement and acquire feedback signal.
The above is only the preferred embodiments of the utility model, are not intended to limit the utility model, all in the utility model
Spirit and principle within, any modification, equivalent replacement, improvement and so on should be included in the protection model of the utility model
Within enclosing.
Claims (3)
1. a kind of rocket gun big gun control equipment Measuring error training device, it is characterised in that: including pedestal (1), on the pedestal (1)
Side is provided with flat pad (3), several support devices (2) are provided between the pedestal (1) and the flat pad (3)；
Launching tube group (4) and the direction controlling for controlling the launching tube group (4) are provided with above the flat pad (3)
Device (5)；The control device (5) includes launching tube group support shaft (5.1)；
The launching tube group (4) is connected with launching tube group support shaft (5.1) upper end；The launching tube group support shaft
(5.1) lower end and the flat pad (3) are rotatablely connected；
The control device (5) further includes motor, and the motor setting is in the flat pad (3), the output of the motor
Axis and the launching tube group support shaft (5.1) are sequentially connected；
The control device (5) further includes rotary encoder (5.2), and the code-disc of the rotary encoder (5.2) is by closing
The conveyer belt (5.4) of cyclization shape and the launching tube group support shaft (5.1) are sequentially connected.
2. rocket gun big gun control equipment Measuring error training device according to claim 1, it is characterised in that: the control dress
Setting (5) further includes tensioner (5.3)；
The tensioner (5.3) includes tension roller (5.31), connecting rod (5.32), is fixedly connected on the flat pad (3)
The limiting slot (5.33) and reset spring (5.34) of the U-shaped of upper surface；
The tension roller (5.31) and the conveyer belt (5.4), which roll, to be cooperated；One end of the connecting rod (5.32) with described
Power rod (5.31) rotation connection, the other end be inserted into the interior of the limiting slot (5.33) and with the reset spring (5.34) one
End connection；The other end of the reset spring (5.34) is connect with the limiting slot (5.33) inner wall.
3. according to claim 1 or 2 any rocket gun big gun control equipment Measuring error training devices, it is characterised in that: institute
Stating support device (2) includes the upper hinged ear (2.1) being fixedly connected with the flat pad (3) lower end surface and the pedestal (1)
The lower hinged ear (2.2) and hydraulic cylinder that upper surface is fixedly connected；The hydraulic cylinder includes being rotatablely connected with lower hinged ear (2.2)
Hydraulic cylinder fixing end (2.3) and hydraulic cylinder movable end (2.4) with upper hinged ear (2.1) rotation connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820815926.XU CN208269730U (en) | 2018-05-29 | 2018-05-29 | Rocket gun control equipment detection maintenance training device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820815926.XU CN208269730U (en) | 2018-05-29 | 2018-05-29 | Rocket gun control equipment detection maintenance training device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208269730U true CN208269730U (en) | 2018-12-21 |
Family
ID=64684805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820815926.XU Expired - Fee Related CN208269730U (en) | 2018-05-29 | 2018-05-29 | Rocket gun control equipment detection maintenance training device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208269730U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110444070A (en) * | 2019-08-05 | 2019-11-12 | 中国人民解放军陆军工程大学 | Simulated maintenance training device for antiaircraft gun equipment |
| CN112611258A (en) * | 2020-12-10 | 2021-04-06 | 武汉高德红外股份有限公司 | Integrated smoke screen shrapnel launching device |
| CN113883957A (en) * | 2020-07-03 | 2022-01-04 | 北京机械设备研究所 | Can dismantle operating floor in pit |
-
2018
- 2018-05-29 CN CN201820815926.XU patent/CN208269730U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110444070A (en) * | 2019-08-05 | 2019-11-12 | 中国人民解放军陆军工程大学 | Simulated maintenance training device for antiaircraft gun equipment |
| CN113883957A (en) * | 2020-07-03 | 2022-01-04 | 北京机械设备研究所 | Can dismantle operating floor in pit |
| CN113883957B (en) * | 2020-07-03 | 2023-05-23 | 北京机械设备研究所 | Detachable underground operation table |
| CN112611258A (en) * | 2020-12-10 | 2021-04-06 | 武汉高德红外股份有限公司 | Integrated smoke screen shrapnel launching device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20181221 Termination date: 20210529 |