CN206311009U - Guided missile centroid measurement system - Google Patents
Guided missile centroid measurement system Download PDFInfo
- Publication number
- CN206311009U CN206311009U CN201621308668.3U CN201621308668U CN206311009U CN 206311009 U CN206311009 U CN 206311009U CN 201621308668 U CN201621308668 U CN 201621308668U CN 206311009 U CN206311009 U CN 206311009U
- Authority
- CN
- China
- Prior art keywords
- guided missile
- type weighing
- supporting brackets
- bridge type
- measurement system
- Prior art date
- 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.)
- Active
Links
Landscapes
- Tests Of Electric Status Of Batteries (AREA)
Abstract
The utility model discloses a kind of guided missile centroid measurement system, it includes measuring instrument, two bridge type weighing sensors, two supporting brackets and connecting rods, it is connected by connecting rod between two supporting brackets, it is used to hold up guided missile, two bridge type weighing sensors are separately positioned on two supporting brackets, it is used to weigh guided missile, there is graduated scale in the connecting rod, two supporting brackets can be connected at different pitches, the measuring instrument connects two bridge type weighing sensors respectively, to acquisition process data, and show guided missile centroid position.This complete equipment facilitates the outfield target practice hanging point test job of guided missile, can quickly position hanging point position, high with integrated level, simple to operate, fully ensures reliability, the practicality of outfield application.
Description
Technical field
The utility model is related to a kind of guided missile centroid measurement system, it is adaptable to the outfield target practice hanging point test environment of guided missile.
Background technology
Guided missile as a kind of strategic materials, can be used for hit including tank, panzer, ground fortification etc. target, recently with
Developing rapidly for unmanned plane, air-to-ground guided missile is also more and more equipped on unmanned plane, for the strike of target, guided missile is hung
The treatment of point position plays an important role to the balance of unmanned plane and guided missile, and the optimal location of guided missile hanging point is exactly the matter of guided missile
Heart position.The centroid measurement method of existing certain type of missile uses what traditional lever principle was realized, this measurement side
Method needs repeatedly to adjust in realization can obtain the approximate location of guided missile barycenter, and ratio of precision is relatively low.
The content of the invention
The utility model provides a kind of guided missile centroid measurement system, this device achieves that to the intelligence of guided missile Mass Distribution
Collection, and the relative position of guided missile barycenter is included on intelligent display instrument, it is truly realized a key reality of guided missile centroid measurement
Existing integrated design.
Guided missile centroid measurement system of the present utility model includes measuring instrument, two bridge type weighing sensors, two supporting brackets
And connecting rod, it is connected by connecting rod between two supporting brackets, it is used to hold up guided missile, two bridge type weighing sensors
It is separately positioned on two supporting brackets, is used to weigh guided missile, there is graduated scale in the connecting rod, can be with different
Be connected for two supporting brackets by spacing, and the measuring instrument connects two bridge type weighing sensors respectively, to acquisition process number
According to, and show guided missile centroid position.
It is preferred that the tester includes Control card, smart display card, guidance panel, data-interface, charging inlet, master control
Unit, mV units, number electric unit, mould electric unit, the collection that bridge type weighing sensor data are used for by mV units are described
Main control unit is used to process gathered data, and guided missile barycenter station-keeping data is included on smart display card, institute
Guidance panel is stated to be gathered for realizing that a key of guided missile barycenter is started shooting.
It is preferred that several electric units are integrated with the intelligent display meter, for battery supply to be converted into needed for digit chip
Power supply；The mould electric unit, the power supply needed for for battery supply to be converted into bridge type weighing sensor.
It is preferred that described intelligent display meter possesses functions of the equipments configuration, display clearing, the low alarm of battery electric quantity, it is external to fill
Electrical equipment charges to device battery.
Intelligent acquisition instrument to the collection of guided missile Mass Distribution by the way of multi collect is averaged, and combined with hardware
Filtering improves precision, realizes centroid position precision ± 0.1mm.
Brief description of the drawings
Fig. 1 is the structural representation of the utility model system.
Fig. 2 is board structure figure.
Fig. 3 is the schematic diagram of support section.
Specific embodiment
The utility model is further described below in conjunction with accompanying drawing.
Guided missile centroid measurement system of the present utility model includes measuring instrument, two bridge type weighing sensors, 12, two supports
Support 13 and connecting rod 14, measuring instrument include top shrouding 1, instrument case 2, Control card 3, smart display card 4, guidance panel 5, number
According to interface 6, charging inlet 7, main control unit 8, mV units 9, number electric unit 10 and mould electric unit 11.
In Fig. 1, Control card 3 is stacked with smart display card 4 by contact pin socket, and is bolted on instrument
In watchcase 2, mechanical seal and electrical isolation are carried out by top shrouding 1, data-interface 6 realizes that gathered data is interacted, charging
Mouth 7 charges the battery.
In Fig. 2, the collection of weighing sensor data is carried out by mV units 9, main control unit 8 is processed gathered data
Afterwards, guided missile barycenter station-keeping data is included that on smart display card 4 key that guidance panel 5 realizes guided missile barycenter is opened
Machine is gathered.
In Fig. 2, the power supply needed for battery supply to be converted into electric unit 10 digit chip is counted, mould electric unit 11 is electric by battery
Source be converted into analog circuit needed for power supply.
In Fig. 3, bridge type weighing sensor 12 is integrated in guided missile supporting bracket 13, while protection sensor body, it is to avoid
Guided missile body is scratched by sharp objects, and connecting rod 14 reduces the complexity of centroid measurement.Connecting rod between two supporting brackets 13
14 are connected, and 1 bridge type weighing sensor 12 is integrated with each supporting bracket 13, have graduated scale in connecting rod 14, can
Be connected two supporting brackets 13 at different pitches.
When being weighed, the spacing as required of connecting rod 14 is connected two supporting brackets 13, bridge-type is weighed biography
Sensor 12 is connected with tester is weighed.And the spacing between two supporting brackets can be changed, the support to guided missile is converted
Point is repeatedly weighed, and calculating treatment is carried out by tester gathered data, to obtain the barycenter of guided missile.
The utility model advantage compared with prior art is as follows：
(1) intelligent display meter possesses functions of the equipments configuration, display clearing, the low alarm of battery electric quantity, and external charger is given
Device battery charges.
(2) intelligent acquisition instrument and is combined to the collection of guided missile Mass Distribution by the way of multi collect is averaged
Hardware filtering improves precision, realizes centroid position precision ± 0.1mm.
Claims (4)
1. a kind of guided missile centroid measurement system, it is characterised in that：Including measuring instrument, two bridge type weighing sensors, two supports
Support and connecting rod, are connected between two supporting brackets by connecting rod, are used to hold up guided missile, two bridge-type weighing and sensings
Device is separately positioned on two supporting brackets, is used to weigh guided missile, has graduated scale in the connecting rod, can be with difference
Spacing two supporting brackets are connected, the measuring instrument connects two bridge type weighing sensors respectively, to acquisition process
Data, and show guided missile centroid position.
2. guided missile centroid measurement system as claimed in claim 1, it is characterised in that：The measuring instrument includes Control card, intelligence
Card, guidance panel, data-interface, charging inlet, main control unit, mV units, number electric unit, mould electric unit can be shown, it is described logical
MV units are crossed for the collection of bridge type weighing sensor data, the main control unit is used to process gathered data, and will
Guided missile barycenter station-keeping data is displayed on smart display card, and the guidance panel is used to realize the key start of guided missile barycenter
Collection.
3. guided missile centroid measurement system as claimed in claim 2, it is characterised in that：Number electricity is integrated with the smart display card
Unit, the power supply needed for for battery supply to be converted into digit chip；The mould electric unit, for battery supply to be converted into
Power supply needed for bridge type weighing sensor.
4. guided missile centroid measurement system as claimed in claim 3, it is characterised in that：Described intelligent display meter possesses equipment
Functional configuration, display reset, the low alarm of battery electric quantity, and external charger charges to device battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621308668.3U CN206311009U (en) | 2016-11-30 | 2016-11-30 | Guided missile centroid measurement system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621308668.3U CN206311009U (en) | 2016-11-30 | 2016-11-30 | Guided missile centroid measurement system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206311009U true CN206311009U (en) | 2017-07-07 |
Family
ID=59250167
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621308668.3U Active CN206311009U (en) | 2016-11-30 | 2016-11-30 | Guided missile centroid measurement system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206311009U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108458772A (en) * | 2018-06-04 | 2018-08-28 | 彩虹无人机科技有限公司 | The measuring table and method of a kind of guided missile quality and axial barycenter |
-
2016
- 2016-11-30 CN CN201621308668.3U patent/CN206311009U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108458772A (en) * | 2018-06-04 | 2018-08-28 | 彩虹无人机科技有限公司 | The measuring table and method of a kind of guided missile quality and axial barycenter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203310494U (en) | Clock electronic scale | |
| CN105928600A (en) | Weight measurement method and device | |
| CN206311009U (en) | Guided missile centroid measurement system | |
| CN207337725U (en) | A kind of experimental provision of quick measure acceleration of gravity | |
| CN206575813U (en) | A kind of remote monitoring device for rice transplanter | |
| CN106403735A (en) | System for measuring center of mass of missile | |
| CN201852631U (en) | Quality measurement test device for simulating weightless environment | |
| CN202188993U (en) | Automatic measuring device for physical property indexes of soil mass | |
| CN107491004A (en) | Intelligent weighing tester and its application method | |
| CN103191483A (en) | Infusion bracket | |
| CN207007462U (en) | Fall-down test device | |
| CN103604487A (en) | Computer combination scale with function of automatic calibration and calibration method thereof | |
| CN206292252U (en) | A kind of quartz digital flexibility acceleration transducer | |
| CN203169718U (en) | Infusion support | |
| CN206892294U (en) | BMS measuring and analysing meters | |
| CN105737960A (en) | Joint weighing device of a plurality of weighing devices | |
| CN206745839U (en) | A kind of treadmill with function of weighing | |
| CN202757677U (en) | Inventory machine | |
| CN205228474U (en) | Rotation angle indicating device | |
| CN110208557A (en) | A kind of automatic control device for assisting detecting | |
| CN205898279U (en) | Electronic scale can open and shut | |
| CN201177870Y (en) | DC combination electric field and ion stream density measuring system | |
| CN203231807U (en) | Weighing machine with body balance measurement function | |
| CN107764467A (en) | A kind of Lever-type Standard Force Measuring Machine control system | |
| CN202757679U (en) | Inventory machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |