CN202041119U - Counting detecting device for rocket emission - Google Patents
Counting detecting device for rocket emission Download PDFInfo
- Publication number
- CN202041119U CN202041119U CN2010206649501U CN201020664950U CN202041119U CN 202041119 U CN202041119 U CN 202041119U CN 2010206649501 U CN2010206649501 U CN 2010206649501U CN 201020664950 U CN201020664950 U CN 201020664950U CN 202041119 U CN202041119 U CN 202041119U
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- rocket
- detecting device
- emission
- sensor
- counting
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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.)
- Expired - Fee Related
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Abstract
The utility model provides a counting detecting device for rocket emission, mainly comprising an electric vortex type displacement sensor, a transmitter, a detecting mainboard of a CPU (Central Processing Unit provided with a display and a keyboard, and a power supply, when a rocket projectile is used to approach to the periphery of an electromagnetic field emitted by a sensor, the internal of the rocket body generates vortex to absorb energy of an oscillator, reducing oscillation capability of the sensor, and changing parameters of the internal circuit, non-contact detection of whether ammunition passes is completed according to change of attenuation amount, and whether a rocket ammunition emission is performed is identified via the transmitter's transmission to the CPU. The counting detecting device for rocket emission in the utility model is advantaged by simple structure, convenient and easy manufacture, and detection of emission process in the state of non-contact spacing, and the counting detecting device can be installed on a rocket emission cylinder, etc., providing simpleness and convenience.
Description
Technical field
The utility model is a kind of rocket launching counting and detecting device, count detection when can be used for space flight or military field rocket launching.
Background technology
At present, the transmitting tube of space flight or conventional weapon rocket all has the number of times in service life, and surpassing access times can influence fire accuracy and safe in utilization, causes casualty accident thereby explosion may take place in excessive use.And the record of legacy transmission rocket number of times mainly is the method by manual record, and advanced, poor in timeliness are unfavorable for the correct use and the scientific management of weaponry.In order to ensure the reliability and the security of rocket launching, make transmitting tube be in good tactics technology state, be necessary to invent a kind of counting and detecting device that is used for rocket launching.
Summary of the invention
The purpose of this utility model is mainly to be the deficiency that relies on the hand-kept method in order to overcome legacy transmission rocket quantity record, and a kind of fire a rocket counting and detecting device of number of times of automatic record that has is provided.The principle of the invention is by utilizing the electric vortex type displacement sensor, it belongs to the linear unit of metal induction, form by LC high-frequency generator and amplification treatment circuit, after connecting power supply, when utilizing body to be transmitted in around the electromagnetic field that proximity transducer sends, make that the metal body is inner to be produced eddy current automatically and drawn the energy of oscillator, make the decay of sensor oscillation ability, the internal circuit parameter changes, whether change according to attenuation and to finish contactless detection and have rocket to pass through, signal passes to central processing unit by transmitter and identifies and have or not rocket launching.
The technical scheme that the utility model adopted is: a kind of rocket launching counting and detecting device, mainly by sensor, transmitter, the central processing unit that has display and keyboard detects mainboard and power supply composition, it is characterized in that sensor adopts the electric vortex type displacement sensor, form by LC high-frequency generator and amplification treatment circuit, after connecting power supply, when utilizing around the electromagnetic field that the metal body sends at proximity transducer, shell is inner to be produced eddy current and has drawn the energy of oscillator, make the decay of sensor oscillation ability, the parameter of internal circuit changes, and whether finish contactless detection according to the variation of attenuation has rocket to pass through, and identifies thus to have or not rocket launching, signal is input to central processing unit by transmitter and reaches the counting purpose, shows by display.Central processing unit detects on the mainboard keyboard is installed, and real-time clock and storage chip can write down the time and the state of each rocket launching process, whether successful launch, the management of being convenient to equip.
The utility model beneficial effect is, but the security protection of this counting and detecting device is such as cannon, rocket-launching battery etc., simple and convenient to the transmitting tube outside of various firearms; Under the state of noncontact interval, use the emission process of electric vortex sensor measuring rocket, original equipment is not changed; Since induced field very a little less than, so to emission process without any influence.Realize the projectile amount of every transmitting tube of cumulative statistics accurately and reliably, guaranteed fire accuracy and safe in utilization; Adopt the electrostatic detection technology, rocket projectile is caused excite inadequately, guarantee the reliability and the security that detect owing to send the minute-pressure electric current.
Description of drawings
Fig. 1 is a structural representation of the present utility model
Among the figure: 1, electric vortex type displacement sensor 2, transmitter 3, power supply 4, have the detection mainboard of the central processing unit (CPU) of display and keyboard
The specific embodiment:
Be described in detail embodiment of the present utility model below in conjunction with accompanying drawing.
Fig. 1 is a kind of rocket launching counting and detecting device, mainly by electric vortex type displacement sensor 1, and transmitter 2, the central processing unit that has display and keyboard detects mainboard 4 and power supply 3 compositions, and power supply 3 is whole counting and detecting device power supply.
Claims (1)
1. rocket launching counting and detecting device, mainly by sensor, transmitter, the central processing unit that has display and a keyboard detects mainboard and power supply is formed, it is characterized in that sensor is the electric vortex type displacement sensor, is made up of LC high-frequency generator and amplification treatment circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206649501U CN202041119U (en) | 2010-12-17 | 2010-12-17 | Counting detecting device for rocket emission |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206649501U CN202041119U (en) | 2010-12-17 | 2010-12-17 | Counting detecting device for rocket emission |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202041119U true CN202041119U (en) | 2011-11-16 |
Family
ID=44968558
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010206649501U Expired - Fee Related CN202041119U (en) | 2010-12-17 | 2010-12-17 | Counting detecting device for rocket emission |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202041119U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020165606A1 (en) * | 2019-02-15 | 2020-08-20 | Mbda Uk Limited | Improvements in and relating to operating a munitions system |
| CN113654399A (en) * | 2021-08-18 | 2021-11-16 | 中国兵器装备集团自动化研究所有限公司 | Method and device for detecting gun firing times and gun body movement |
-
2010
- 2010-12-17 CN CN2010206649501U patent/CN202041119U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020165606A1 (en) * | 2019-02-15 | 2020-08-20 | Mbda Uk Limited | Improvements in and relating to operating a munitions system |
| GB2595823A (en) * | 2019-02-15 | 2021-12-08 | Mbda Uk Ltd | Improvements in and relating to operating a munitions system |
| GB2595823B (en) * | 2019-02-15 | 2023-10-18 | Mbda Uk Ltd | Improvements in and relating to operating a munitions system |
| US11958627B2 (en) | 2019-02-15 | 2024-04-16 | Mbda Uk Limited | Operating a munitions system |
| CN113654399A (en) * | 2021-08-18 | 2021-11-16 | 中国兵器装备集团自动化研究所有限公司 | Method and device for detecting gun firing times and gun body movement |
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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 |
Granted publication date: 20111116 Termination date: 20141217 |
|
| EXPY | Termination of patent right or utility model |