CN212347727U - Model rocket igniter based on super capacitor - Google Patents

Model rocket igniter based on super capacitor Download PDF

Info

Publication number
CN212347727U
CN212347727U CN202020228110.4U CN202020228110U CN212347727U CN 212347727 U CN212347727 U CN 212347727U CN 202020228110 U CN202020228110 U CN 202020228110U CN 212347727 U CN212347727 U CN 212347727U
Authority
CN
China
Prior art keywords
shell
knob switch
super capacitor
lithium ion
gear
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
Application number
CN202020228110.4U
Other languages
Chinese (zh)
Inventor
李易
王文豪
杨德敏
崔佳豪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Priority to CN202020228110.4U priority Critical patent/CN212347727U/en
Application granted granted Critical
Publication of CN212347727U publication Critical patent/CN212347727U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention provides a model rocket igniter based on a super capacitor, belonging to the field of model rockets; the LED ignition device comprises a knob switch, an emission button, an LED indicator lamp, an ignition head interface, a shell and a control circuit; the shell is of a detachable split box body structure, the knob switch, the emission button and the LED indicator lamp are all arranged on one side wall surface of the shell, the ignition head interface is arranged on the other side wall surface of the shell, and the control circuit is arranged in the shell; the knob switch comprises a knob switch 1 gear and a knob switch 2 gear, and the LED indicator lamp is a light emitting diode; the control circuit comprises a lithium ion battery, a protection resistor R and a super capacitor C; the ignition head is more reliably ignited by adopting the charging and discharging of the rechargeable lithium battery and the super capacitor, and the LED lamp is adopted to indicate the emission state, so that the emission is safer.

Description

Model rocket igniter based on super capacitor
Technical Field
The invention belongs to the field of model rockets, and particularly relates to a model rocket igniter based on a super capacitor.
Background
With the gradual development of aerospace science popularization culture, the launching of small rockets such as small solid rocket performance, scientific research rocket model competition and the like is more common to enter the life of ordinary people, so that a safe and reliable ignition device needs to be provided.
The existing similar device is mainly a small handheld igniter designed and produced by a medium rocket company (four Kai model), as shown in figures 1 and 2, the picture sources are as follows: igniter instructions sold by Zhongtian rocket corporation (four Keys model). The device mainly comprises a power supply, a safety pin, an indicator light, a transmitting button, a plastic shell, a lead, a crocodile clip and the like. When the alligator clip switches on the igniter and simultaneously inserts the safety pin, the internal circuit is switched on and the indicator light lights up. When the firing button is pressed, the metal sheet short-circuits the internal resistor and the light-emitting diode, the circuit current is increased, and the ignition head is ignited. Problems with this igniter:
a. the plastic shell has insufficient sealing performance and has great danger when being emitted in severe environments such as rain and snow;
b. the internal power supply is provided by a dry battery, the battery has small capacity and low voltage, and cannot be charged, so that the environmental pollution is easily caused;
c. the instantaneous discharge current is small, and the large-resistance ignition head cannot be ignited;
d. the firing button is susceptible to shock causing misfires.
Disclosure of Invention
The technical problem to be solved is as follows:
in order to avoid the defects of the prior art, the invention provides a model rocket igniter based on a super capacitor, which enhances the shell sealing property to adapt to launching tasks in different launching scenes (particularly in severe environment); a novel power supply is adopted, so that larger battery capacity and power supply voltage are provided, and the rechargeable battery is chargeable; by adopting a novel circuit structure, large current is generated, and the ignition head is ensured to be successfully ignited; and a more reliable launching button is adopted, so that the launching safety is improved.
The technical scheme of the invention is as follows: a model rocket igniter based on super capacitor is characterized in that: the LED ignition device comprises a knob switch, an emission button, an LED indicator lamp, an ignition head interface, a shell and a control circuit; the shell is of a detachable split box body structure, the knob switch, the emission button and the LED indicator lamp are all arranged on one side wall surface of the shell, the ignition head interface is arranged on the other side wall surface of the shell, and the control circuit is arranged in the shell; the knob switch comprises a knob switch 1 gear and a knob switch 2 gear, and the LED indicator lamp is a light emitting diode;
the control circuit comprises a lithium ion battery, a protection resistor R and a super capacitor C; the lithium ion battery is used as a direct current power supply U, the anode of the lithium ion battery is sequentially connected with a knob switch 1 gear S1, a light emitting diode and an ignition head interface OUT1 in series, and the cathode of the lithium ion battery is connected with the ignition head interface OUT 2; the knob switch 2 gear S2 is connected in series with a protection resistor R and then connected in parallel with the direct current power supply U and the knob switch 1 gear S1, and is connected in parallel with the super capacitor C, and the emission button is used as a normally open switch S3 and connected in parallel with the light emitting diode; all the components are connected through wires.
The further technical scheme of the invention is as follows: the shell is made of metal aluminum and comprises a main shell, a metal rear cover and a battery cover plate; the main shell is of a box body structure with an opening at one side, and the metal rear cover is embedded into the opening of the main shell and is fixed along the circumferential direction through four countersunk head screws; the battery cover plate is embedded in a battery mounting hole formed in the metal rear cover and is fixed by a countersunk head screw.
The further technical scheme of the invention is as follows: the joint of the shell is sealed by sealant.
The further technical scheme of the invention is as follows: the lithium ion battery is a 9V rechargeable lithium ion battery.
Advantageous effects
The invention has the beneficial effects that:
1. the invention adopts the embedded assembly of the metal shell, so that the shell has stronger sealing property and shock resistance, and meets the use requirement under worse conditions;
2. the service life of the igniter can be greatly prolonged by adopting the rechargeable lithium ion battery with high energy density; higher voltage and capacitance ensure more reliable ignition;
3. the parallel super capacitor C is charged and discharged for ignition, S3 is closed, the super capacitor C is directly connected into a circuit, and instantaneous large current is released to ensure the ignition reliability;
4. by adopting the structure that the protective resistor R and the knob switch are connected with the super capacitor C in parallel, the residual electric quantity after ignition is finished can be released, the capacitor can be protected, and the service life is prolonged.
5. And the light emitting diode is adopted to indicate the emitting state, so that the circuit state is better judged, and the emitting is safer and more reliable.
Drawings
FIG. 1 is a schematic representation of the use of a prior art igniter;
FIG. 2 is a general block diagram of a prior art igniter;
FIG. 3 is an external view of the igniter of the invention;
FIG. 4 is a rear elevational view of an igniter of the invention;
fig. 5 is a control circuit diagram of the igniter of the invention.
Description of reference numerals: 1. knob switch, 2 emission buttons, 3 LED indicator lamps, 4 ignition head interfaces, 5 main shell, 6 metal rear cover, 7 battery cover plate.
Detailed Description
The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
Referring to fig. 3 and 4, the model rocket igniter based on the super capacitor comprises a knob switch 1, a launching button 2, an LED indicator lamp 3, an ignition head interface 4, a shell and a control circuit; the shell is of a detachable split box structure and made of metal aluminum, and comprises a main shell 5, a metal rear cover 6 and a battery cover plate 7; the main shell 1 is a box structure with an opening at one side, and the metal rear cover 6 is embedded into the opening of the main shell 5 and is fixed along the circumferential direction through four countersunk head screws; the battery cover plate 7 is embedded in a battery mounting hole formed in the metal rear cover 6 and is fixed by a countersunk head screw. The joint of the shell is sealed by sealant.
The knob switch 1, the emission button 2 and the LED indicator lamp 3 are all arranged on one side wall surface of the shell, the ignition head interface 4 is arranged on the other side wall surface of the shell, and the control circuit is arranged in the shell; the knob switch 1 comprises a knob switch 1 gear and a knob switch 2 gear, and the LED indicator lamp 3 is a light emitting diode; the lithium ion battery is a 9V rechargeable lithium ion battery, has higher voltage, larger battery capacity and energy density, and can be charged, and the service life of the igniter is prolonged.
Referring to fig. 5, the control circuit includes a lithium ion battery, a protection resistor R, and a super capacitor C; the lithium ion battery is used as a direct current power supply U, the anode of the lithium ion battery is sequentially connected with a knob switch 1 gear S1, a light emitting diode and an ignition head interface OUT1 in series, and the cathode of the lithium ion battery is connected with the ignition head interface OUT 2; the knob switch 2 gear S2 is connected in series with a protection resistor R and then connected in parallel with the direct current power supply U and the knob switch 1 gear S1, and is connected in parallel with the super capacitor C, and the emission button is used as a normally open switch S3 and connected in parallel with the light emitting diode; all the components are connected through wires.
The ignition head interface 4 is connected in series with an ignition head which needs to be ignited from the outside, the knob switch 1 controls charging and discharging of the internal super capacitor C, and the emission button 2 controls ignition of the ignition head.
And (4) safety state: when the knob switch 1 is in the 1-position, i.e., S1 is open, S2 is closed, and S3 is open, the whole circuit is in a safety state, and no current flows in the circuit.
And (3) detecting the state: when the knob switch 1 is in the 2-position, i.e., S1 is closed, S2 is opened, and S3 is opened, the super capacitor C is charged by the direct-current power supply. At this time, if the ignition head is connected to the ignition head interface 4, the ignition head is equivalent to a resistor which is connected in series to enter the circuit, the loop is conducted, the LED indicating lamp 3 is turned on, and the brightness is increased along with the rise of the voltage at the two ends of the super capacitor C. Further, the state of the LED indicator light 3 can indicate the emission state, when the light is not on, the circuit is broken, and the circuit needs to be checked again after the power supply is cut off; when the LED indicator lamp 3 gradually becomes bright, the circuit is normal, and emission can be carried out.
And (3) a transmitting state: when the brightness of the LED indicator lamp 3 reaches the specified brightness, namely the voltage across the super capacitor C reaches the specified voltage, the emission button 2 is pressed, namely S3 is closed. At the moment, the LED indicating lamp 3 is broken, the current in the loop is increased instantly, and the ignition head is ignited to finish the transmitting task.
And (4) ending the emission: when the emission is finished, a certain amount of charges may still exist in the super capacitor C, at this time, the knob switch is pulled back to the 1-position of the knob switch, i.e., S1 is turned off, S2 is turned on, and S3 is turned off, and the protection resistor R and the capacitor form a discharge loop to completely release the residual charges.
The ignition head is more reliably ignited by adopting the charging and discharging of the rechargeable lithium battery and the super capacitor, and the LED lamp is adopted to indicate the emission state, so that the emission is safer.
Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and that variations, modifications, substitutions and alterations can be made in the above embodiments by those of ordinary skill in the art without departing from the principle and spirit of the present invention.

Claims (4)

1. A model rocket igniter based on super capacitor is characterized in that: the LED ignition device comprises a knob switch, an emission button, an LED indicator lamp, an ignition head interface, a shell and a control circuit; the shell is of a detachable split box body structure, the knob switch, the emission button and the LED indicator lamp are all arranged on one side wall surface of the shell, the ignition head interface is arranged on the other side wall surface of the shell, and the control circuit is arranged in the shell; the knob switch comprises a knob switch 1 gear and a knob switch 2 gear, and the LED indicator lamp is a light emitting diode;
the control circuit comprises a lithium ion battery, a protection resistor R and a super capacitor C; the lithium ion battery is used as a direct current power supply U, the anode of the lithium ion battery is sequentially connected with a knob switch 1 gear S1, a light emitting diode and an ignition head interface OUT1 in series, and the cathode of the lithium ion battery is connected with the ignition head interface OUT 2; the knob switch 2 gear S2 is connected in series with a protection resistor R and then connected in parallel with the direct current power supply U and the knob switch 1 gear S1, and is connected in parallel with the super capacitor C, and the emission button is used as a normally open switch S3 and connected in parallel with the light emitting diode; all the components are connected through wires.
2. The supercapacitor-based model rocket igniter of claim 1, wherein: the shell is made of metal aluminum and comprises a main shell, a metal rear cover and a battery cover plate; the main shell is of a box body structure with an opening at one side, and the metal rear cover is embedded into the opening of the main shell and is fixed along the circumferential direction through four countersunk head screws; the battery cover plate is embedded in a battery mounting hole formed in the metal rear cover and is fixed by a countersunk head screw.
3. The supercapacitor-based model rocket igniter of claim 1, wherein: the joint of the shell is sealed by sealant.
4. The supercapacitor-based model rocket igniter of claim 1, wherein: the lithium ion battery is a 9V rechargeable lithium ion battery.
CN202020228110.4U 2020-02-28 2020-02-28 Model rocket igniter based on super capacitor Active CN212347727U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020228110.4U CN212347727U (en) 2020-02-28 2020-02-28 Model rocket igniter based on super capacitor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020228110.4U CN212347727U (en) 2020-02-28 2020-02-28 Model rocket igniter based on super capacitor

Publications (1)

Publication Number Publication Date
CN212347727U true CN212347727U (en) 2021-01-15

Family

ID=74144670

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020228110.4U Active CN212347727U (en) 2020-02-28 2020-02-28 Model rocket igniter based on super capacitor

Country Status (1)

Country Link
CN (1) CN212347727U (en)

Similar Documents

Publication Publication Date Title
RU57423U1 (en) INDIVIDUAL ACCUMULATOR LAMP
CN201190905Y (en) Electric torch with gang control
CN212347727U (en) Model rocket igniter based on super capacitor
CN101604839B (en) Over-discharge protection circuit for rechargeable battery
CN206977141U (en) A kind of Multi-function super electric capacity car emergency startup power supply
CN101706079A (en) Emergency LED fluorescent lamp
CN107221977A (en) A kind of application process of iron lithium phosphate battery and its protection circuit plate
CN203534355U (en) Detonation box with detonation detection function
CN2859987Y (en) Luminous diode wall lamp
KR101021623B1 (en) Led illumination device for emergency
CN113856092A (en) Fire extinguishing bomb data collection launching control device
CN109185921B (en) High-integration electronic cigarette lighter chip
CN201636555U (en) Miniature mine lamp with auxiliary light source
CN215001697U (en) Super capacitor multi-channel timing igniter based on embedded circuit board
CN2883897Y (en) Multifunction emergency bulbs
CN2733162Y (en) LED miner's lamp
CN2869584Y (en) Mine-use safety helmet light
CN202252908U (en) Methane alarming mining lamp
CN202074252U (en) Multi-way rechargeable light-emitting diode (LED) flashlight
CN212617715U (en) Rechargeable flashlight
CN209562880U (en) A kind of airport navigation lighting fault equipment based on LORA technology
CN201925729U (en) Multi-functional movable illuminating lamp
CN201246655Y (en) Emergent lamp capable of performing timing discharging for battery
CN201866682U (en) Solar lamp with function of charger
CN220363278U (en) Roof lamp control circuit of carriage for goods and goods van

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant