CN203489793U - Rocket bomb for artificial influence weather operating system - Google Patents
Rocket bomb for artificial influence weather operating system Download PDFInfo
- Publication number
- CN203489793U CN203489793U CN201320543271.2U CN201320543271U CN203489793U CN 203489793 U CN203489793 U CN 203489793U CN 201320543271 U CN201320543271 U CN 201320543271U CN 203489793 U CN203489793 U CN 203489793U
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- rocket projectile
- module
- rocket bomb
- processor
- positioning device
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Abstract
The utility model discloses a rocket bomb for an artificial influence weather operating system. The rocket bomb comprises a rocket bomb body and a positioning device box, wherein the positioning device box is fixedly arranged in an air cap of the rocket bomb body; the positioning device box is internally provided with a processor, a GPRS (General Packet Radio Service) module, a GPS (Global Positioning System) module, a built-in antenna which is arranged on the GPRS module and batteries for supplying power to each part of the positioning device box; the GPRS module is in communication connection with the processor; a position data output port of the GPS module is electrically connected with a position data input port of the processor. According to the rocket bomb for the artificial influence weather operating system disclosed by the utility model, the positioning device box is arranged, so that a field control system and/or a remote command control system can be enabled to track the flight track of the rocket bomb.
Description
Technical field
The utility model relates to a kind of Weather modification operation system, relates in particular to and has the location tracking structure of rocket projectile for the Weather modification operation system of positioning function.
Background technology
The effect that weather modification rocket is sowed operating system is when possessing Weather modification operation condition, transmitting by ground rocket projectile is transported to catalyst in cloud layer, subcooled water in cloud layer is carried out to catalysis, catalyst can reduce the temperature of cloud layer and increase artificial-ice nucleus, facilitates precipitation or increases more precipitation.
Existing do not possess positioning function for Weather modification operation rocket projectile, field control system and remote command control system cannot position and record the flight path of rocket projectile, can not meet the accuracy that increases rain hail mitigation operation, also greatly restrict the practical and intelligent of weather modification equipment operation.
Because Weather modification operation rocket projectile applied environment is very severe, add the impact of high rotation, vibrations and overload, make existing locating and tracking system be difficult to directly apply on Weather modification operation rocket projectile.
Utility model content
The purpose of this utility model is to be used to provide a kind of rocket projectile with positioning function.
The technical solution adopted in the utility model is: a kind of Weather modification operation system rocket projectile, comprise rocket projectile body, described Weather modification operation system also comprises the positioner box in the blast cap that is fixedly installed in rocket projectile body with rocket projectile, in described positioner box, be provided with processor, GPRS module, GPS module, be installed on built-in aerial in GPRS module and be the battery of the each several part power supply of positioner box, described GPRS module is connected with processor communication, the position data output of described GPS module is electrically connected to preferably with the position data input port of processor, described positioner box is installed in blast cap and the Cang Linjieweizhichu that sows rocket projectile body.
Preferably, at least a portion of the outer surface of described positioner box and the inner surface of blast cap fit.
Preferably, on described positioner box, damping device is installed.
The beneficial effects of the utility model are: Weather modification operation system of the present utility model by positioner box is set, just can make field control system and/or remote command control system can track the flight path of rocket projectile with rocket projectile.
Accompanying drawing explanation
Fig. 1 is the partial schematic sectional view with rocket projectile according to Weather modification operation system described in the utility model;
Fig. 2 is the frame principle figure of the internal structure of positioner box in Fig. 1.
The specific embodiment
As illustrated in fig. 1 and 2, Weather modification operation system of the present utility model comprises rocket projectile body with rocket projectile, for example to be installed on the positioner box 2 in the blast cap 1 of rocket projectile body by trip bolt 4, in this positioner box 2, be provided with processor 21, GPRS module 22, GPS module 23, be installed on built-in aerial in GPRS module 23 and be the battery 24 of the each several part power supply of positioner box, GPRS module 22 and processor 21 communication connections, with the position data that GPS module 23 is collected, by communication network, be sent to field control system and/or remote command control system, the position data output of GPS module 23 is electrically connected to the position data input port of processor 1.This positioner box 2 can be installed in blast cap 1 with rocket projectile body sow 3 adjoining position places, storehouse.
At least a portion of the outer surface of this positioner box 2 can fit with the inner surface of blast cap, further to guarantee not rocket projectile body motion relatively of positioner box 2.
The utility model utilize GPRS packet-switch technology have at a high speed, in real time, the wide feature of network coverage, with GPS location in real time and fast with the GIS advantage to geographical data tracking demonstration intuitively, realized real-time location, tracking to moving target.Positioner box is arranged in rocket projectile, and while starting working, the flight path by GPS chip positioning rocket projectile is also recorded, by GPRS mode, be transferred to remote command center, when GPRS link is obstructed, data first preserve, and while waiting until link-recovery, then send.
Rocket projectile of the present utility model can possess following characteristics after mounting and positioning device box:
1, by GPS module collecting device positional information;
2, by GPRS module wireless transmission, return positional information;
3, can and send interval to acquisition interval arranges;
4, system low-power consumption operation, recyclable reusing;
5, command centre's integrating third-party map carries out real-time locating and displaying;
6, module is small and light, and built-in aerial is easy to install and replace.
The foregoing is only preferably embodiment of the utility model, be not used for limiting practical range of the present utility model, the equivalence of in every case doing in protection domain of the present utility model changes and modifies, and all should think and fall in protection domain of the present utility model.
Claims (4)
1. a Weather modification operation system rocket projectile, comprise rocket projectile body, it is characterized in that: described Weather modification operation system also comprises the positioner box in the blast cap that is fixedly installed in rocket projectile body with rocket projectile, in described positioner box, be provided with processor, GPRS module, GPS module, be installed on built-in aerial in GPRS module and be the battery of the each several part power supply of positioner box, described GPRS module is connected with processor communication, and the position data output of described GPS module is electrically connected to the position data input port of processor.
2. Weather modification operation system rocket projectile according to claim 1, is characterized in that: described positioner box is installed in blast cap and the Cang Linjieweizhichu that sows rocket projectile body.
3. Weather modification operation system rocket projectile according to claim 1 and 2, is characterized in that: at least a portion of the outer surface of described positioner box and the inner surface of blast cap fit.
4. Weather modification operation system rocket projectile according to claim 1 and 2, is characterized in that: on described positioner box, damping device is installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320543271.2U CN203489793U (en) | 2013-09-03 | 2013-09-03 | Rocket bomb for artificial influence weather operating system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320543271.2U CN203489793U (en) | 2013-09-03 | 2013-09-03 | Rocket bomb for artificial influence weather operating system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203489793U true CN203489793U (en) | 2014-03-19 |
Family
ID=50260616
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320543271.2U Expired - Fee Related CN203489793U (en) | 2013-09-03 | 2013-09-03 | Rocket bomb for artificial influence weather operating system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203489793U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
-
2013
- 2013-09-03 CN CN201320543271.2U patent/CN203489793U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104266555A (en) * | 2014-09-30 | 2015-01-07 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
| CN104266555B (en) * | 2014-09-30 | 2017-02-15 | 程鹏 | Artificial precipitation hail prevention rocket positioning system |
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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 |
Granted publication date: 20140319 Termination date: 20160903 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |