CN108168384A - A kind of full bullet of guided missile tilts swing testing system - Google Patents
A kind of full bullet of guided missile tilts swing testing system Download PDFInfo
- Publication number
- CN108168384A CN108168384A CN201711164073.4A CN201711164073A CN108168384A CN 108168384 A CN108168384 A CN 108168384A CN 201711164073 A CN201711164073 A CN 201711164073A CN 108168384 A CN108168384 A CN 108168384A
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- China
- Prior art keywords
- guided missile
- control
- monitoring
- cable
- testing
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- 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A kind of full bullet of guided missile tilts swing testing system, the system is made of inclination Swaying Test Platform, mounting and clamping system, control system, measuring system, monitoring system, the full bullet of guided missile tilts swing testing system and solves the problems such as clamping when guided missile snaps into line tilt rolling test entirely, explosion-proof, remote control, measurement are with monitoring, the pilot system is full-featured, security consideration is thoughtful, the test capability that ship-based missile carries out environmental suitability examination is improved, is had a good application prospect.
Description
Technical field
The present invention relates to technical field of mechanical environmental test, and in particular to the inclination rolling test with the full bullet of priming system guided missile
System.
Background technology
Tilt and wave inclination and wave environmental activity that environmental suitability refers to that Ship Equipment encounters in its lifetime
Lower to realize its all predetermined function characteristic and not destroyed ability, it is one of important quality characteristic of Ship Equipment.Incline
Oblique rolling test carries out on Swaying Test Platform is tilted.Guided missile snaps into line tilt rolling test with larger technical difficulty entirely.
The storage configuration of simulated missile is answered in the connection of guided missile and testing stand, and with connection reliability, it is ensured that wide-angle is waved under environment
It will not loosen.
Guided missile of participating in the experiment carries priming system, aviation kerosine and gas cylinder, and there are priming system explosion, aviation coals during experiment
The security risks such as oil leakage burning, gas cylinder explosion, need fully to ensure test products and people in the design of pilot system
The safety of member.It is reliably connected and security implementation to ensure that full bullet tilts the product of rolling test, devises full bullet inclination and wave
Pilot system.The system includes tilting Swaying Test Platform, mounting and clamping system, control system, measuring system, monitoring system etc..It solves
Full bullet tilts the problems such as clamping of rolling test, explosion-proof, remote control, measurement are with monitoring, realizes the full bullet inclination of guided missile and shakes
Pendulum experiment.
Invention content
When guided missile snaps into line tilt rolling test entirely, the storage configuration of simulated missile is answered in the connection of guided missile and testing stand, and
With higher connection reliability.Guided missile of participating in the experiment carries priming system, aviation kerosine and gas cylinder, there is safety during experiment
Risk needs fully to ensure test products and the safety of personnel in the design of pilot system.
The present invention devises the full bullet of guided missile and tilts swing testing system, ensure that product is reliable for experimental technique difficult point
Connection and experiment safety realize the full bullet of guided missile and tilt rolling test.
For overcome the deficiencies in the prior art, the present invention provides a kind of full bullet of guided missile and tilts swing testing system, the system
Used technical solution is：A kind of full bullet of guided missile tilts swing testing system, and the system is by inclination Swaying Test Platform, clamping system
System, control system, measuring system, monitoring system composition, guided missile are connected by mounting and clamping system with experiment table top, and control system is to inclining
Oblique Swaying Test Platform is controlled, and is controlled and is used network remote control mode, during measuring system can test body
Acceleration carries out monitored over time and acquisition, and the parameter of electric machine in testing stand operational process is monitored in real time, measuring system
Network remote control mode is taken, monitoring system includes high-definition camera, and complete monitoring and video recording, monitoring are carried out to experiment process
System uses the mode of remote network control.
It is 3DOF testing stand to tilt Swaying Test Platform, can be carried out at the same time rolling, pitching, the inclination in yawing direction are shaken
Put environmental simulation.
Mounting and clamping system uses the form of clip, and clip is made of upper and lower two parts, is bolted between two parts,
Lower catch hoop is connect by screw with experiment table top, and there are gaps between upper and lower clip, apply pressing force for clip and provide space,
Pressing force between clip is provided by the pretightning force of connection bolt, and clip inner ring bonding felt protects body outer surface,
The connection of tooling and testing stand table top also carries out insulation processing, ensures the insulation of guided missile and table top.
The control system carries out motion control to tilting Swaying Test Platform, using remote controlled manner, SERVO CONTROL cabinet
Testing ground is positioned over, control computer is located in the control room outside scene, and SERVO CONTROL cabinet passes through cable with control computer
Connection, by router to signal enhancing among cable, meanwhile, by tilt Swaying Test Platform power switch and emergency stop switch from
It draws, is positioned in control room in SERVO CONTROL cabinet.
The measuring system includes data collecting instrument, and data collecting instrument is located at testing ground, including body response data, shakes
Data including the motor temperature data of pendulum testing stand access data collecting instrument by cable, and metering computer is located at outside 200 meters
Control room in, data collecting instrument is connect with metering computer by cable, by router to signal enhancing among cable.
The monitoring system includes 2 high-definition cameras, and carrying out complete monitoring and video recording, monitoring system to experiment process makes
With the mode of remote network control, high-definition camera is located at testing ground, and test products are carried out from 2 orthogonal directions respectively
Monitoring, monitoring computer bit is in the control room outside 200 meters, and high-definition camera is connect with monitoring calculation machine by cable, in cable
Between by router carry out 2 tunnel monitoring signals signal distribution and signal enhancing.
The full bullet of guided missile tilt swing testing system solve clamping when guided missile snaps into line tilt rolling test entirely, it is explosion-proof,
Remote control, measurement with monitoring the problems such as, the pilot system is full-featured, and security consideration is thoughtful, improve ship-based missile into
The test capability of row environmental suitability examination, has a good application prospect.
Description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, to embodiment or will show below
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention, for those of ordinary skill in the art, without creative efforts, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is that the full bullet of guided missile tilts swing testing system examination composition figure.
Fig. 2 is that the full bullet of guided missile tilts swing testing system yoke configurations figure.
Fig. 3 is that the full bullet of guided missile tilts swing testing system table top seal figure.
Specific embodiment
The present invention is further described with reference to embodiment.
Embodiment 1
As shown in Figs. 1-3, the full bullet of guided missile tilts swing testing system by inclination Swaying Test Platform, mounting and clamping system, control system
The compositions such as system, measuring system, monitoring system.
It is 3DOF testing stand to tilt Swaying Test Platform, can be carried out at the same time rolling, pitching, the inclination in yawing direction are shaken
Put environmental simulation.
The storage configuration of mounting and clamping system simulated missile has connection reliability, it is ensured that wide-angle is waved will not pine under environment
It is de-.The full bullet 1 of guided missile is connected by clip 5 with tilter table top 6.Connecting tooling use clip form, clip by front band 7,
8 two parts of lower catch hoop form, and are connected between two parts by clamp connection bolt 9.Lower catch hoop 8 passes through bolt and tilter table top
6 connections.There are 6mm gaps between front band 7, lower catch hoop 8, apply pressing force for clip and provide space, front band 7, lower catch hoop 8
Between pressing force by clamp connection bolt 9 pretightning force provide.Clip inner ring be bonded 5mm thickness felt layers 10, to body outside
It is protected on surface.
To realize the insulation between the full bullet 1 of guided missile and rolling test table top 6, ensure the safety of guided missile, it is exhausted to devise table top
Edge device.Seal includes insulation board 2, insulation sleeve 12 and insulation plain cushion 15, and material is the nylon of thickness 2mm.Lower catch hoop 8 with
Insulation board 2 is encased inside between tilter table top 6, insulating cylinder 12, nut are inserted into lower catch hoop 8 and the connection through-hole of tilter table top 6
Insulation spacer 15 is encased inside between 13 and tilter table top 6.Table top seal is ensureing to lead between tilter table top 6 and clip 5
While crossing bolt 11 and be fastenedly connected, the insulation between tilter table top 6 and clip 5 is realized, and then realize the full bullet 1 of guided missile
With the insulation between rolling test table top 6.
Control system carries out motion control to tilting Swaying Test Platform, using remote controlled manner.SERVO CONTROL cabinet is placed
In testing ground, control computer is located in the control room outside 200 meters.SERVO CONTROL cabinet is connected with control computer by cable
It connects, by router to signal enhancing among cable.Meanwhile by the power switch for tilting Swaying Test Platform and emergency stop switch from watching
It takes in switch board and draws, be positioned in control room.
Acceleration during measuring system can test body carries out monitored over time and acquisition, and testing stand is run
The parameters such as motor temperature in the process are monitored in real time, and measuring system takes network remote control mode.Data collecting instrument position
In testing ground, body response data, motor temperature data of Swaying Test Platform etc. access data collecting instrument by cable.It measures
Computer bit is in the control room outside 200 meters.Data collecting instrument is connect with metering computer by cable, passes through road among cable
By device to signal enhancing.
Monitoring system includes 2 high-definition cameras, carries out complete monitoring and video recording to experiment process, monitoring system uses remote
The mode of journey network control.High-definition camera is located at testing ground, and test products are supervised from 2 orthogonal directions respectively
Control.Computer bit is monitored in the control room outside 200 meters.High-definition camera is connect with monitoring calculation machine by cable, among cable
Signal distribution and the signal enhancing of 2 tunnel monitoring signals are carried out by router.
Claims (6)
1. a kind of full bullet of guided missile tilts swing testing system, the system by inclination Swaying Test Platform, mounting and clamping system, control system,
Measuring system, monitoring system composition, which is characterized in that guided missile is connected by mounting and clamping system with experiment table top, and control system is to inclining
Oblique Swaying Test Platform is controlled, and is controlled and is used network remote control mode, during measuring system can test body
Acceleration carries out monitored over time and acquisition, and the parameter of electric machine in testing stand operational process is monitored in real time, measuring system
Network remote control mode is taken, monitoring system includes high-definition camera, and complete monitoring and video recording, monitoring are carried out to experiment process
System uses the mode of remote network control.
2. the full bullet of guided missile according to claim 1 tilts swing testing system, which is characterized in that tilting Swaying Test Platform is
3DOF testing stand can be carried out at the same time rolling, environmental simulation is waved in pitching, the inclination in yawing direction.
3. the full bullet of guided missile according to claim 1 tilts swing testing system, which is characterized in that mounting and clamping system uses clip
Form, clip is made of upper and lower two parts, is bolted between two parts, and lower catch hoop passes through screw and experiment table top
Connection there are gap between upper and lower clip, provides space, the pressing force between clip is by connection spiral shell for clip application pressing force
The pretightning force of bolt provides, and clip inner ring bonding felt is protected body outer surface, tooling and the connection of testing stand table top
Insulation processing is carried out, ensures the insulation of guided missile and table top.
4. the full bullet of guided missile according to claim 1 tilts swing testing system, which is characterized in that the control system is to inclining
Oblique Swaying Test Platform carries out motion control, and using remote controlled manner, SERVO CONTROL cabinet is positioned over testing ground, control computer
In the control room outside scene, SERVO CONTROL cabinet is connect with control computer by cable, passes through router pair among cable
Signal enhancing, meanwhile, the power switch for tilting Swaying Test Platform and emergency stop switch out of SERVO CONTROL cabinet are drawn, are positioned over control
In system.
5. the full bullet of guided missile according to claim 1 tilts swing testing system, which is characterized in that the measuring system includes
Data collecting instrument, data collecting instrument are located at testing ground, exist including body response data, the motor temperature data of Swaying Test Platform
Interior data access data collecting instrument by cable, and metering computer is located in the control room outside 200 meters, and data collecting instrument is with surveying
Amount computer is connected by cable, by router to signal enhancing among cable.
6. the full bullet of guided missile according to claim 1 tilts swing testing system, which is characterized in that the monitoring system includes
2 high-definition cameras carry out experiment process complete monitoring and video recording, and monitoring system uses the mode of remote network control, high
Clear camera is located at testing ground, and test products are monitored from 2 orthogonal directions respectively, and monitoring computer bit is in 200
In control room outside rice, high-definition camera is connect with monitoring calculation machine by cable, and 2 tunnel monitoring are carried out by router among cable
The signal distribution of signal and signal enhancing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711164073.4A CN108168384B (en) | 2017-11-21 | 2017-11-21 | A kind of full bullet inclination swing testing system of guided missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711164073.4A CN108168384B (en) | 2017-11-21 | 2017-11-21 | A kind of full bullet inclination swing testing system of guided missile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108168384A true CN108168384A (en) | 2018-06-15 |
| CN108168384B CN108168384B (en) | 2019-11-12 |
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ID=62527139
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711164073.4A Active CN108168384B (en) | 2017-11-21 | 2017-11-21 | A kind of full bullet inclination swing testing system of guided missile |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112595656A (en) * | 2020-12-09 | 2021-04-02 | 中国兵器工业第五九研究所 | Testing device and evaluation method for adaptability of explosive device long-storage environment for bomb |
| RU220742U1 (en) * | 2023-02-17 | 2023-10-02 | Федеральное Государственное Казенное Военное Образовательное Учреждение Высшего Образования "Тихоокеанское Высшее Военно-Морское Училище Имени С.О. Макарова" Министерства Обороны Российской Федерации (Г. Владивосток) | DYNAMIC TEST BENCH FOR CHECKING THE SYSTEM FOR FIXING A QUADROCOPTER ON THE LANDING SITE |
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| CN102269540A (en) * | 2011-06-15 | 2011-12-07 | 北京机械设备研究所 | Measurement device for unbalanced impulse |
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| CN205158781U (en) * | 2015-11-25 | 2016-04-13 | 上海新跃仪表厂 | Modular fixture with insulating function |
| CN105676885A (en) * | 2016-04-20 | 2016-06-15 | 中国工程物理研究院总体工程研究所 | Dual-driving servo control device of large-torque serial swing table, and control methods |
| CN106425567A (en) * | 2016-10-20 | 2017-02-22 | 成都久欣时代科技有限公司 | Seat type fixture for missile noses |
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2017
- 2017-11-21 CN CN201711164073.4A patent/CN108168384B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102269540A (en) * | 2011-06-15 | 2011-12-07 | 北京机械设备研究所 | Measurement device for unbalanced impulse |
| CN203479545U (en) * | 2012-12-20 | 2014-03-12 | 苏州电器科学研究院股份有限公司 | Multidimensional incline swing combination device |
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| CN205158781U (en) * | 2015-11-25 | 2016-04-13 | 上海新跃仪表厂 | Modular fixture with insulating function |
| CN105676885A (en) * | 2016-04-20 | 2016-06-15 | 中国工程物理研究院总体工程研究所 | Dual-driving servo control device of large-torque serial swing table, and control methods |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112595656A (en) * | 2020-12-09 | 2021-04-02 | 中国兵器工业第五九研究所 | Testing device and evaluation method for adaptability of explosive device long-storage environment for bomb |
| RU220742U1 (en) * | 2023-02-17 | 2023-10-02 | Федеральное Государственное Казенное Военное Образовательное Учреждение Высшего Образования "Тихоокеанское Высшее Военно-Морское Училище Имени С.О. Макарова" Министерства Обороны Российской Федерации (Г. Владивосток) | DYNAMIC TEST BENCH FOR CHECKING THE SYSTEM FOR FIXING A QUADROCOPTER ON THE LANDING SITE |
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| Publication number | Publication date |
|---|---|
| CN108168384B (en) | 2019-11-12 |
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