CN205998144U - The igniter working under high rotational speeds - Google Patents

The igniter working under high rotational speeds Download PDF

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Publication number
CN205998144U
CN205998144U CN201620984351.5U CN201620984351U CN205998144U CN 205998144 U CN205998144 U CN 205998144U CN 201620984351 U CN201620984351 U CN 201620984351U CN 205998144 U CN205998144 U CN 205998144U
Authority
CN
China
Prior art keywords
module
microprocessor
relay
under high
rotational speeds
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
Application number
CN201620984351.5U
Other languages
Chinese (zh)
Inventor
贾琳琳
万天军
庞桂林
艾文涛
徐志修
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.)
AVIC Aerospace Life Support Industries Ltd
Original Assignee
AVIC Aerospace Life Support Industries Ltd
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 AVIC Aerospace Life Support Industries Ltd filed Critical AVIC Aerospace Life Support Industries Ltd
Priority to CN201620984351.5U priority Critical patent/CN205998144U/en
Application granted granted Critical
Publication of CN205998144U publication Critical patent/CN205998144U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of igniter working under high rotational speeds is it is characterised in that include power module, wireless data transmission module, microprocessor, relay and ignition module;Wherein this power module is connected with wireless data transmission module, microprocessor;This wireless data transmission module receives the telecommand of ground remote control device by antenna and is sent to microprocessor;Microprocessor is connected with drive module, and relay is connected with drive module, and ignition module is connected with relay module.

Description

The igniter working under high rotational speeds
Technical field
This utility model is related to igniter, more particularly, to a kind of igniter working under high rotational speeds.
Background technology
Bullet is high-speed rotation after launching, and under these conditions, will be slowed down using parachute it is necessary that controlling The igniter that parachute is opened reliably working under high-speed rotation.Igniter is exported from charged pool, igniting by cable, During high-speed rotation, battery power cable and igniting cable plate may be got rid of in interrupting and splitting it is also possible to cause battery moment to power Break it is also possible to cause ignition signal to interrupt.Have no product and the introduction that can be suitable for igniter under high rotational speeds at present.
Utility model content
The purpose that this utility model is wanted is to provide a kind of igniter that can work under high rotational speeds.
This utility model be employed technical scheme comprise that by reaching above-mentioned purpose:
Provide a kind of igniter working under high rotational speeds it is characterised in that including power module, wireless Digital transmission module, microprocessor, relay and ignition module;Wherein this power module is connected with wireless data transmission module, microprocessor; This wireless data transmission module receives the telecommand of ground remote control device by antenna and is sent to microprocessor;Microprocessor and driving Module connects, and relay is connected with drive module, and ignition module is connected with relay module.
In the igniter working under high rotational speeds described in the utility model, this power module includes being connected Battery and power-switching circuit.
In the igniter working under high rotational speeds described in the utility model, relay includes electromagnetic induction line Circle, one diode of this electromagnetic induction coil reversal connection.
This utility model produce beneficial effect be:This utility model structure is simple, small volume, lightweight it is easy to install And dismounting, it is applicable to high-speed rotation, strong vibration, the IGNITION CONTROL under the conditions of impact, integral waterproofing, in high humidity, underwater environment Can also work.
Brief description
Below in conjunction with drawings and Examples, the utility model is described in further detail, in accompanying drawing:
Fig. 1 is the structured flowchart of the igniter that this utility model embodiment works under high rotational speeds;
Fig. 2 is the circuit diagram of the igniter that this utility model embodiment works under high rotational speeds.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and enforcement Example, is further elaborated to this utility model.It should be appreciated that specific embodiment described herein is only in order to explain this Utility model, is not used to limit this utility model.
The igniter that this utility model embodiment works under high rotational speeds, can be referred to remote control outside wireless receiving Order, output current, excite priming system to complete parachute-opening.Igniter carries wireless data transmission module to complete wirelessly using microcontroller The transmitting-receiving of signal.
As shown in figure 1, the igniter that this utility model embodiment works under high rotational speeds include power module, Wireless data transmission module, microprocessor, relay and ignition module;Wherein this power module and wireless data transmission module, microprocessor Connect;This wireless data transmission module receives the telecommand of ground remote control device by antenna and is sent to microprocessor;Microprocessor It is connected with drive module, relay is connected with drive module, ignition module is connected with relay module.
In igniter, microcontroller adopts the pattern of inquire-receive, compares with firing command after receiving serial data, if It is that the switching tube that high level opens drive module is exported by control port, thus driving relay make contact, igniting dress Battery in putting discharges through priming system (i.e. ignition module), excites priming system to work, jettisoning umbrella hatchcover, parachute-opening.Selection of Battery Rechargeable battery, moment (in the 50ms) discharge current of battery is not less than 2A.Microcontroller adopts surface mount packages, wireless data sending mould Block adopts no package module to reduce volume.Select the relay having compared with high-reliability, tolerance acceleration is not less than 49g, tolerance Vibration be not less than 20g (10~3000Hz), resistance to be hit not less than 73g, contact specified carrying current capacity is not less than 1A.Igniting In device, battery and circuit should be isolated layering and be placed, and quality should be uniformly distributed centered on machine shaft as far as possible.The rotation of motor It is mainly used in the bullet after analog transmissions.
Igniter should have a metal shell, and battery and circuit board are all well fixed in housing, and carries out Fill glue to fix.Shell and umbrella cabin accomplish to be fitted close as far as possible, shell also will centered on machine shaft symmetrical configuration, uniform quality Distribution.The antenna of wireless data transmission module should be placed on shell, to ensure the reception of signal.
As shown in Fig. 2 igniter of the present utility model specifically includes following part:
1) power module
Power module is made up of with power-switching circuit two parts battery.Battery provides 11.1V power supply, supplies to relay Electricity, simultaneously as the importation of power-switching circuit.11.1V Power convert is 5V power supply by power-switching circuit part, uses In to wireless data transmission module and microprocessor power supply.
2) wireless data transmission module
Wireless data transmission module receives the telecommand of ground remote control device by antenna, passes to microprocessor by serial port.
3) microprocessor
Microcontroller adopts the pattern of inquire-receive, compares with firing command after receiving serial data, if then passing through control Port P1.0 processed exports high level.The data receiving is inputted by STC12C5201AD serial port, and serial port works in mode 1.String The baud rate of row mouth is set as 1200 according to the transfer rate of wireless data transmission module.Time constant TH1=thus can be calculated TL1=0xe8.
4) drive module
This drive module connection adopts low side to drive.Microprocessor control port P1.0 exports high level, IRLR3410's DS end turns on, and A point is connected with battery cathode.Microprocessor control port P1.0 exports low level, and the DS end of IRLR3410 is ended, A point output voltage reaches stable high level.
5) relay
Relay includes electromagnetic induction coil, one diode of this electromagnetic induction coil reversal connection.A point is connected with battery cathode Afterwards, relay coil end will pass through certain electric current, thus producing galvanomagnetic-effect, will turn on 1,2 ends of relay contact.Continue One diode of electric apparatus coil end reversal connection, shields to circuit, protects audion not reverse by relay coil two ends Electromotive force burns.
6) ignition module
Ignition module is priming system, and excitation current is sent out for 2A/.After relay contact 1,2 termination is logical, battery is through priming system Electric discharge, excites priming system to work.
As shown in Fig. 2 the power supply of control circuit is connected to battery by switch of pulling pin, radio communication line and power line are all Linked on circuit board by CRM2 plug.Telecommand outside igniter wireless receiving, output current, excite priming system to complete Parachute-opening.
Remote control Booting sequence, ground remote control device can connect SM56 wireless data transmission module or with carrying serial ports to adjust by nonshared control unit The computer (palm PC etc.) of examination software connects SM56 wireless data transmission module composition;With nonshared control unit only need to press startup by Button then starting ignition device, connects SM56 wireless data transmission module with computer, and wireless data transmission module computer-chronograph of powering need to not stop Ground sends 0xaa order by serial ports to radio station, and igniter excites priming system to work after receiving order, throw umbrella hatchcover, open Umbrella.
It should be appreciated that for those of ordinary skills, can be improved according to the above description or be converted, And all these modifications and variations all should belong to the protection domain of this utility model claims.

Claims (3)

1. a kind of igniter working under high rotational speeds is it is characterised in that include power module, wireless data sending mould Block, microprocessor, relay and ignition module;Wherein this power module is connected with wireless data transmission module, microprocessor;This is wireless Digital transmission module receives the telecommand of ground remote control device by antenna and is sent to microprocessor;Microprocessor is with drive module even Connect, relay is connected with drive module, ignition module is connected with relay module.
2. the igniter working under high rotational speeds according to claim 1 is it is characterised in that this power module Including the battery being connected and power-switching circuit.
3. the igniter working under high rotational speeds according to claim 1 is it is characterised in that relay includes Electromagnetic induction coil, one diode of this electromagnetic induction coil reversal connection.
CN201620984351.5U 2016-08-29 2016-08-29 The igniter working under high rotational speeds Expired - Fee Related CN205998144U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620984351.5U CN205998144U (en) 2016-08-29 2016-08-29 The igniter working under high rotational speeds

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620984351.5U CN205998144U (en) 2016-08-29 2016-08-29 The igniter working under high rotational speeds

Publications (1)

Publication Number Publication Date
CN205998144U true CN205998144U (en) 2017-03-08

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620984351.5U Expired - Fee Related CN205998144U (en) 2016-08-29 2016-08-29 The igniter working under high rotational speeds

Country Status (1)

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CN (1) CN205998144U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110737258A (en) * 2019-10-08 2020-01-31 航宇救生装备有限公司 floating system controller ignition circuit on-line detection system and detection method
CN111946491A (en) * 2020-07-14 2020-11-17 上海机电工程研究所 Wireless induction type ignition and speed measuring device between aircraft cabins

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110737258A (en) * 2019-10-08 2020-01-31 航宇救生装备有限公司 floating system controller ignition circuit on-line detection system and detection method
CN110737258B (en) * 2019-10-08 2022-10-18 航宇救生装备有限公司 Online detection system and detection method for ignition circuit of floating system controller
CN111946491A (en) * 2020-07-14 2020-11-17 上海机电工程研究所 Wireless induction type ignition and speed measuring device between aircraft cabins
CN111946491B (en) * 2020-07-14 2023-02-28 上海机电工程研究所 Wireless induction type ignition and speed measuring device between aircraft cabins

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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: 20170308

Termination date: 20190829