CN201378018Y - Electronic igniter of one-key multiple repeating model rockets - Google Patents
Electronic igniter of one-key multiple repeating model rockets Download PDFInfo
- Publication number
- CN201378018Y CN201378018Y CN200920011920U CN200920011920U CN201378018Y CN 201378018 Y CN201378018 Y CN 201378018Y CN 200920011920 U CN200920011920 U CN 200920011920U CN 200920011920 U CN200920011920 U CN 200920011920U CN 201378018 Y CN201378018 Y CN 201378018Y
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- switch
- model
- signal source
- rockets
- electric pulse
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Abstract
The utility model relates to an electronic igniter of one-key multiple repeating model rockets, which comprises an electric pulse generation device and an ignition device. The electric pulse generation device includes a battery, a J806H signal source, a main power switch K1, a protection switch K2, a launching switch K3 and an 8550 triode. The ignition device includes a DS2Y-S-DC 5V relay, light emitting diodes, a resistor and a flame arrestor. A slide rheostat R1 is connected with the J806H signal source. When in use, the main power switch K1 is opened, the light emitting diodes (LED) are lighted, the flame arrestor is prepared for working, and the circuit connection is normal. The protection switch K2 is turned on, and the launching switch K3 is closed to start the ignition device. The frame arrestor instantly generates high heat to ignite the model rockets sequentially. The launching speed can be adjusted through the slide rheostat R1. The utility model has the advantages of reasonable structure, wide application, high efficiency and safety, convenient operation and the like.
Description
Technical field
The utility model relates to a kind of igniter, many pieces of running fire model rockets of especially a kind of key ignition.
Background technology
In electronic equipment, igniter is the igniter that people use always, but people utilize the various combustible materials of ignition remote control, and can protect inherently safe.But in present rocket model ignition process, people but can only be to the emission of lighting a fire separately one by one of a plurality of rockets, very trouble and inconvenience.For this reason, we provide many pieces of running fire model rockets of a kind of key ignition very necessary.
Summary of the invention
The purpose of this utility model provides many pieces of running fire model rockets of a kind of key ignition, is used to solve the problem that common rocket model igniter can't be launched many pieces of rockets one by one fast.
For achieving the above object, many pieces of running fire model rockets of the utility model one key ignition, comprise electric pulse generator and igniter, electric pulse generator is made up of battery, J806H signal source, total power switch K1, protection switch K2, emission switch K3 and 8550 triodes; Igniter is formed one group by DS2Y-S-DC5V relay, light emitting diode, resistance and showing tremendous enthusiasm resistance head; On J806H signal source slice, thin piece, connect slide rheostat R1.
After adopting said structure, during use, open total power switch K1, a plurality of LEDs all ignite, a showing tremendous enthusiasm resistance this moment preparation, and circuit connects normal.Start protection switch K2, closed again emission switch K3 makes igniter start working, and a showing tremendous enthusiasm resistance moment generation high heat is lighted rocket model, and lights one by one.Emission rate can be mediated from slide rheostat R1.
Compared with the prior art, the beneficial effects of the utility model are: rational in infrastructure, be widely used, highly effective and safe, easy and simple to handle, can disposablely light many pieces of rocket models, sparking mode fast and safely is provided.
Description of drawings
Fig. 1 is the circuit diagram of many pieces of running fire model rockets of the utility model one key ignition.
The specific embodiment
As shown in Figure 1, many pieces of running fire model rockets of the utility model one key ignition, comprise electric pulse generator and igniter, electric pulse generator is made up of battery, J806H signal source, total power switch K1, protection switch K2, emission switch K3 and 8550 triodes; Igniter is formed one group by DS2Y-S-DC5V relay, light emitting diode, resistance and showing tremendous enthusiasm resistance head; On J806H signal source slice, thin piece, connect slide rheostat R1.
Claims (1)
1, many pieces of running fire model rockets of a kind of key ignition, comprise electric pulse generator and igniter, it is characterized in that: electric pulse generator is made up of battery, J806H signal source, total power switch K1, protection switch K2, emission switch K3 and 8550 triodes; Igniter is formed one group by DS2Y-S-DC5V relay, light emitting diode, resistance and showing tremendous enthusiasm resistance head; On J806H signal source slice, thin piece, connect slide rheostat R1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920011920U CN201378018Y (en) | 2009-03-16 | 2009-03-16 | Electronic igniter of one-key multiple repeating model rockets |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920011920U CN201378018Y (en) | 2009-03-16 | 2009-03-16 | Electronic igniter of one-key multiple repeating model rockets |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201378018Y true CN201378018Y (en) | 2010-01-06 |
Family
ID=41518134
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200920011920U Expired - Fee Related CN201378018Y (en) | 2009-03-16 | 2009-03-16 | Electronic igniter of one-key multiple repeating model rockets |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201378018Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075914A (en) * | 2012-12-26 | 2013-05-01 | 北京电子工程总体研究所 | Detonation simulator |
| CN104049555A (en) * | 2013-10-22 | 2014-09-17 | 北京理工大学 | Intelligent control device for model rockets |
| CN104457420A (en) * | 2013-09-24 | 2015-03-25 | 上海机电工程研究所 | Launching method of guided missile safe launching system |
-
2009
- 2009-03-16 CN CN200920011920U patent/CN201378018Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103075914A (en) * | 2012-12-26 | 2013-05-01 | 北京电子工程总体研究所 | Detonation simulator |
| CN103075914B (en) * | 2012-12-26 | 2015-01-21 | 北京电子工程总体研究所 | Detonation simulator |
| CN104457420A (en) * | 2013-09-24 | 2015-03-25 | 上海机电工程研究所 | Launching method of guided missile safe launching system |
| CN104457420B (en) * | 2013-09-24 | 2016-08-17 | 上海机电工程研究所 | The launching technique of guided missile safety emission system |
| CN104049555A (en) * | 2013-10-22 | 2014-09-17 | 北京理工大学 | Intelligent control device for model rockets |
| CN104049555B (en) * | 2013-10-22 | 2016-06-08 | 北京理工大学 | The intelligent controlling device of a kind of model rocket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100106 Termination date: 20110316 |