CN204535576U - A kind of civil rocket bullet blast cap with GPS following function - Google Patents
A kind of civil rocket bullet blast cap with GPS following function Download PDFInfo
- Publication number
- CN204535576U CN204535576U CN201420766327.5U CN201420766327U CN204535576U CN 204535576 U CN204535576 U CN 204535576U CN 201420766327 U CN201420766327 U CN 201420766327U CN 204535576 U CN204535576 U CN 204535576U
- Authority
- CN
- China
- Prior art keywords
- gps
- blast cap
- tracker
- gps tracker
- following function
- 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.)
- Expired - Fee Related
Links
Landscapes
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model relates to a kind of civil rocket bullet blast cap with GPS following function, belongs to civil rocket bullet field.Civil rocket bullet blast cap of the present utility model, comprises blast cap, GPS tracker, padded coaming, sealing heat-barrier material; Rocket projectile blast cap of the present utility model by setting up protective housing outside GPS tracker, and by padded coaming and the encapsulation of sealing heat-barrier material outside GPS tracker, greatly improves GPS tracker anti-overload ability; Gps antenna simultaneously after encapsulation and the axis being parallel of radio antenna and blast cap, ensure that the functional reliability of GPS tracker.
Description
Technical field
The utility model relates to a kind of civil rocket bullet blast cap with GPS following function, belongs to civil rocket bullet field.
Background technology
Existing civil rocket bullet is as hail-proof rain-increasing rocket etc., be uncontrolled missile, rocket is after completing hail-proof rain-increasing operation, by high-altitude parachute-opening freely falling body to ground, because high-altitude wind speed is comparatively large, in descent, the decrease speed of the body that releases a parachute and the impact of descent direction wind-engaging larger, cause body actual falling point and theoretical offset landings comparatively large, parametric controller needs to collect rocket trajectories track by GPS tracker.
The installation requirement of tradition GPS tracker is not high, the high overload requirement of rocket projectile can not be met, be arranged on after on rocket projectile by GPS tracker by the installation method of traditional GPS tracker, in rocket projectile flight course, GPS tracker is cisco unity malfunction by overload effect.
Utility model content
The purpose of this utility model is poor in order to solve GPS tracker anti-overload ability on traditional civil rocket bullet, cisco unity malfunction shortcoming, and provides a kind of civil rocket bullet blast cap with GPS following function.
The purpose of this utility model is achieved through the following technical solutions:
A kind of civil rocket bullet blast cap with GPS positioning function of the present utility model, comprises blast cap, GPS tracker, padded coaming, sealing heat-barrier material;
GPS tracker comprises GPS housing, GPS circuit board, gps antenna, radio antenna;
GPS housing is back-end closure cylinder cylindrical shell, the front end face of this cylinder cylindrical shell connects two front ends by two passing hole and closes and the small cylinder cylindrical shell be parallel to each other, and the gps antenna be connected with GPS circuit board and radio antenna insert in two small cylinder cylindrical shells of GPS housing forward end respectively;
Padded coaming adopts polyurethane foam glue;
Sealing heat-barrier material adopts epoxy resin solid seal glue;
GPS tracker is arranged in blast cap, and padded coaming is filled in the front end of GPS tracker, and the rear end of GPS tracker is encapsulated by sealing heat-barrier material, and makes two small cylinder cylindrical shells of GPS tracker front end and the axis being parallel of blast cap.
Beneficial effect
Rocket projectile blast cap of the present utility model by setting up protective housing outside GPS tracker, and by padded coaming and the encapsulation of sealing heat-barrier material outside GPS tracker, greatly improves GPS tracker anti-overload ability; Gps antenna simultaneously after encapsulation and the axis being parallel of radio antenna and blast cap, ensure that the functional reliability of GPS tracker.
Accompanying drawing explanation
Fig. 1 is the civil rocket bullet blast cap sectional view that the utility model has GPS following function;
Wherein: 1-blast cap; 2-polyurethane foam glue; 3-GPS antenna; 4-radio antenna; 5-GPS tracker; 6-epoxy resin solid seal glue;
Detailed description of the invention
Below in conjunction with drawings and Examples, content of the present utility model is described further:
Embodiment
A kind of civil rocket bullet blast cap with GPS positioning function of the present utility model, as shown in Figure 1, comprises blast cap 1, GPS tracker 5, padded coaming, sealing heat-barrier material;
GPS tracker 5 comprises GPS housing, GPS circuit board, gps antenna 3, radio antenna 4;
GPS housing is back-end closure cylinder cylindrical shell, the front end face of this cylinder cylindrical shell connects two front ends by two passing hole and closes and the small cylinder cylindrical shell be parallel to each other, and the gps antenna be connected with GPS circuit board and radio antenna insert in two small cylinder cylindrical shells of GPS housing forward end respectively;
Padded coaming adopts polyurethane foam glue 2;
Sealing heat-barrier material adopts epoxy resin solid seal glue 6;
GPS tracker 5 is arranged in blast cap 1, and the rear end of front end filled polyurethane foamed glue 2, the GPS tracker 5 of GPS tracker 5 is encapsulated by epoxy resin solid seal glue 6, and makes two small cylinder cylindrical shells of GPS tracker 5 front end and the axis being parallel of blast cap 1.
During installation, first polyurethane foam glue 2 is poured into blast cap 1, then load GPS tracker 5, make two small cylinder cylindrical shells of GPS tracker 5 front end and the axis being parallel of blast cap 1, after polyurethane foam adhesive curing, then epoxy resin solid seal glue 6 is poured into the rear end of GPS tracker 5, until solidified forming.
Claims (3)
1. there is a civil rocket bullet blast cap for GPS following function, it is characterized in that: comprise blast cap, GPS tracker, padded coaming, sealing heat-barrier material;
GPS tracker comprises GPS housing, GPS circuit board, gps antenna, radio antenna;
GPS housing is back-end closure cylinder cylindrical shell, the front end face of this cylinder cylindrical shell connects two front ends by two passing hole and closes and the small cylinder cylindrical shell be parallel to each other, and the gps antenna be connected with GPS circuit board and radio antenna insert in two small cylinder cylindrical shells of GPS housing forward end respectively;
GPS tracker is arranged in blast cap, and padded coaming is filled in the front end of GPS tracker, and the rear end of GPS tracker is encapsulated by sealing heat-barrier material, and makes two small cylinder cylindrical shells of GPS tracker front end and the axis being parallel of blast cap.
2. a kind of civil rocket bullet blast cap with GPS following function as claimed in claim 1, is characterized in that: padded coaming adopts polyurethane foam glue.
3. a kind of civil rocket bullet blast cap with GPS following function as claimed in claim 1, is characterized in that: sealing heat-barrier material adopts epoxy resin solid seal glue.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420766327.5U CN204535576U (en) | 2014-12-09 | 2014-12-09 | A kind of civil rocket bullet blast cap with GPS following function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420766327.5U CN204535576U (en) | 2014-12-09 | 2014-12-09 | A kind of civil rocket bullet blast cap with GPS following function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204535576U true CN204535576U (en) | 2015-08-05 |
Family
ID=53749567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420766327.5U Expired - Fee Related CN204535576U (en) | 2014-12-09 | 2014-12-09 | A kind of civil rocket bullet blast cap with GPS following function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204535576U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110006296A (en) * | 2019-03-29 | 2019-07-12 | 河北省人工影响天气办公室 | Hail-suppression rocket bullet of increasing rain artificially sows job trace monitoring and trajectory deviation-rectifying system |
-
2014
- 2014-12-09 CN CN201420766327.5U patent/CN204535576U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110006296A (en) * | 2019-03-29 | 2019-07-12 | 河北省人工影响天气办公室 | Hail-suppression rocket bullet of increasing rain artificially sows job trace monitoring and trajectory deviation-rectifying system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2012037533A3 (en) | Pyrophoric projectile | |
| CN202609086U (en) | Downwards-throwing popup type parachute opening device of unmanned plane | |
| WO2016105638A3 (en) | Aircraft battery containment pods | |
| CN203666965U (en) | Thermal protection mechanism of hypersonic aircraft | |
| IN2015DN02281A (en) | ||
| CN203323620U (en) | Rain-increasing hail-suppressing rocket projectile recycling device | |
| CN107972872A (en) | A kind of unmanned plane deceleration delivery device | |
| CN207580177U (en) | A kind of unmanned plane with buffer gear | |
| CN204535576U (en) | A kind of civil rocket bullet blast cap with GPS following function | |
| CN201842261U (en) | Pneumatic executive device used for separating two objects | |
| CN202557800U (en) | Pneumatic artificial muscle contraction device for soft landing of airborne landing equipment | |
| CN103387054A (en) | Altitude landing device | |
| CN202890102U (en) | Civil hail preventing rain increasing rocket catalyst diffusing device | |
| CN203190896U (en) | Civil rocket projectile with locating function | |
| CN204078072U (en) | A kind of agricultural spray remotely-piloted vehicle | |
| CN205027218U (en) | Earth's surface passes safty shield who explodes detonator | |
| CN203996907U (en) | A kind of landing auxiliary device of cyclogyro | |
| CN203489792U (en) | Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running | |
| CN206826934U (en) | A kind of concertina type protection device of unmanned plane screw wing | |
| CN109911405A (en) | Goods packing device, packing method for low latitude air-drop | |
| CN205079680U (en) | Explosive post suitable for moisture presplit blasting | |
| CN203975223U (en) | Miniature quadrotor wireless data transmitter | |
| CN204767410U (en) | Anti - umbrella formula model rocket recoverable capsule separating mechanism | |
| CN103419931A (en) | Autonomous lift-off aircraft | |
| CN203347941U (en) | Anti-electromagnetic interference engine ignition tool |
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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150805 Termination date: 20191209 |