CN109301924A - A kind of air-drop signal activation system and its working method based on monocell - Google Patents
A kind of air-drop signal activation system and its working method based on monocell Download PDFInfo
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- CN109301924A CN109301924A CN201811214542.3A CN201811214542A CN109301924A CN 109301924 A CN109301924 A CN 109301924A CN 201811214542 A CN201811214542 A CN 201811214542A CN 109301924 A CN109301924 A CN 109301924A
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- air
- drop
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- mode
- control unit
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
- H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
- H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
- H02J9/061—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems for DC powered loads
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- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Remote Monitoring And Control Of Power-Distribution Networks (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The present invention relates to a kind of air-drop signal activation system and its working method based on monocell, belong to power system design technical field.Invention introduces electrical circuit on the relay J1 of air-drop discharge cock K2 control, it can be achieved that signal and power supply and the automatic collection and connection under air-drop state;Mode selector switch K1 is introduced, with realizing double wire system the switching with one wire system ground, and provides type collection for control unit ECU;It devises the dual control based on mode switch K1 and air-drop discharge cock K2 and drops timing logic, avoid faulty operation of the control unit ECU after control discharge cock K2 pin is extracted, after landing of dropping from the air.The setting of relay J2 can effectively ensure that in the case where chassis powers on, air-drop signal activation system is not influenced by air-drop discharge cock K2;This programme is based on air-drop case internal cell and realizes, does not increase additional battery, and entire working time power consumption is less than 5Ah, there is apparent advantage in weight.
Description
Technical field
The invention belongs to power system design technical fields, and in particular to a kind of air-drop signal activation system based on monocell
System and its working method.
Background technique
In the disaster relief, the airdrop missions such as speedily carry out rescue work, the general method launched respectively using personnel and equipment, after personnel's landing,
Need to find equipment as early as possible, conventionally employed light, sound isotype are big by internal electric source and external environment influence, do not find for a long time
Aerial delivery provisions goods and materials will lead to the damage of power-supply system, influence the execution of task.
Summary of the invention
(1) technical problems to be solved
The technical problem to be solved by the present invention is how to solve the problems, such as that air-drop front and back personnel operate power-supply system.
(2) technical solution
The air-drop signal activation system based on monocell that in order to solve the above-mentioned technical problems, the present invention provides a kind of, packet
It includes:
Double-pole switch mode control switch K1, air-drop discharge cock K2, battery main switch K3, relay J1, relay J2
With control unit ECU;
The double-pole switch mode control switch K1, is double-pole two-position switch, is located on device panel, connects control unit
ECU is divided into daily and air-drop two states, for daily and air-drop pattern switching;It is in parallel in the output end of battery main switch K3
Positive supply may be implemented to relay J2 in the case where battery main switch K3 is closed all the way, shielding air-drop discharge cock K2 control
The influence of the relay J1 of system;The air-drop discharge cock K2 is located at outside vehicle, is activated automatically when dropping out cabin, is had normally closed and normal
Two contacts are opened, after air-drop, the pin of air-drop discharge cock K2 is extracted, and realizes that normally closed switch is opened, normally opened switch closes
It closes, thus the flag bit realizing the switching of power supply and being powered on as delay;The battery main switch K3 is located on the panel of vehicle, and
A route out connects the relay J2, connects the relay J1 and control unit ECU, opens for shielding air-drop after landing
Off status;The relay J1 connects K2, when the pin of K2 is extracted, normally opened switch is closed as air-drop power source active relay
It closes, is powered on for control unit ECU;Described control unit ECU is used to acquire the position of the switch of K1, and the timing for acquiring K2 starts letter
Number, and complete the distribution task to communication load.
Preferably, the system also includes air-drop mode indicating lamp K, for being in air-drop in the grid-connected switch K1 of accessory power supply
When mode, control system is lighted in the case where there is power supply.
Preferably, the flicker cycle of the air-drop mode indicating lamp K is 2Hz, closes air-drop mode in time with prompt person.
Preferably, the relay J1, relay J2 contact be also connected with a battery, the cathode connection of the battery
Switch K1.
Preferably, the load is gPS class like positioning device, according to local situation, the positioning of replacing different-waveband
Signal generator.
The present invention also provides a kind of working methods of system, comprising the following steps:
When the daily mode of the grid-connected switch K1 of accessory power supply is true, power supply system is one wire system, and battery main switch K3 is closed
J2 is connected after conjunction, after shielding influence of the air-drop discharge cock K2 to system is at this point, control unit ECU powers on, acquires accessory power supply
The daily mode signal of grid-connected switch K1 is very, to default distribution to positioning device, be not delayed;
When the air-drop mode of the grid-connected switch K1 of accessory power supply is true, power supply system is double wire system, and battery main switch K3 is disconnected
The case where opening, the pin insertion of K2, the ground of J1 control loop disconnect, and air-drop signal system power-off is in ready mode, at this time without
Power consuming load is connected, and air-drop is waited, and when the pin of K2 is freed, the ground of J1 control loop is connected, and control unit ECU is powered on, and is controlled
Unit ECU detect the air-drop mode of K1 be very after, into air-drop power up mode, control unit ECU start monitor K2 it is normally closed
Switching signal, pin K2 free, and control unit ECU starts timing in 200 seconds, and after the completion of timing, it is negative to connect two-way for waiting landing
It carries;Countdown logic is connected in control unit ECU activation at this time, and two-way load is closed after 1 hour.
Preferably, when K1 is in air-drop mode, air-drop mode indicating lamp K light, flicker cycle 2Hz, prompt person and
When close air-drop mode, be to be controlled by battery main switch K3 by two-way load transfer.
(3) beneficial effect
Invention introduces electrical circuits on the relay J1 of air-drop discharge cock K2 control, it can be achieved that signal and power supply and sky
Automatic collection and connection under throwing state;Mode selector switch K1 is introduced, with realizing double wire system the switching with one wire system ground, and is
Control unit ECU provides type collection;The dual control air-drop timing based on mode switch K1 and air-drop discharge cock K2 is devised to patrol
Volume, avoid false judgment of the control unit ECU after control discharge cock K2 pin is extracted, after landing of dropping from the air.Relay J2
Setting can effectively ensure in the case where chassis powers on, air-drop signal activation system not by air-drop discharge cock K2 shadow
It rings;This programme is based on starting battery realization in aerial delivery provisions, does not increase additional battery, entire working time power consumption is less than
5Ah has apparent advantage in weight.
Detailed description of the invention
Fig. 1 is monocell air-drop signal activation circuit system schematic diagram of the invention.
Specific embodiment
To keep the purpose of the present invention, content and advantage clearer, with reference to the accompanying drawings and examples, to of the invention
Specific embodiment is described in further detail.
As shown in Figure 1, the invention mainly comprises double-pole switch mode control switch K1, air-drop discharge cock K2, power supply are total
Switch K3, relay J1, relay J2, control unit ECU and air-drop mode indicating lamp K;
Double-pole switch mode control switch K1 (in panel, for daily and air-drop pattern switching), drops discharge cock K2
(outside equipment, being activated automatically when for dropping out cabin), battery main switch K3 (original equipment panel, and a route out, relay
J2 facilitates personnel to operate for shielding air-drop switch state after landing);Relay J1 drops power source active relay, K2's
When pin is extracted, normally opened is closed the switch, and can be powered on for control unit ECU;Control unit ECU provides the switch position of acquisition K1
It sets, the timing commencing signal of K2, the distribution task of timing in 200 seconds and load (positioning device).It is described in detail as follows:
Increase an air-drop discharge cock K2 in outside vehicle, there is normally closed and normally open two contacts, after air-drop, the guarantor
The pin that nearly switchs is extracted, and normally closed switch may be implemented and open, and normally opened closes the switch, for realizing power supply switching and prolong
The flag bit of Shi Shang electricity.
In the grid-connected switch K1 of the accessory power supply of aerial delivery provisions instrument panel position arrangement, it is double-pole two-position switch, is divided into
Daily and air-drop two states, may be implemented air-drop and the switching of daily mode;In the output end of battery main switch K3, parallel connection one
Road positive supply may be implemented to relay J2 in the case where battery main switch K3 is closed, shielding air-drop discharge cock K2 control
Relay J1 influence.
The air-drop mode indicating lamp K is set, and when the grid-connected switch K1 of accessory power supply is in air-drop mode, control system exists
It is lighted in the case where having power supply.Flicker cycle 2Hz, prompt person close air-drop mode in time, avoid two-wire control equipment to electric power storage
The influence in pond.
The main operation modes of above-mentioned air-drop signal activation system include:
1) when the daily mode of the grid-connected switch K1 of accessory power supply is true, power supply system is one wire system, and battery main switch K3 is closed
J2 is connected after conjunction, and (switch, which is inserted into or is not inserted into, not to be influenced aerial delivery provisions and make for influence of the shielding air-drop discharge cock K2 to system
With being mainly used for the debugging that equipment such as is packaged at the stages), at this point, after control unit ECU is powered on, acquire the grid-connected switch of accessory power supply
The daily mode signal of K1 is very, to default distribution to positioning device, be not delayed.
In the case where signal activation system is dropped as one wire system, after battery main switch K3 is disconnected, system cut-off makes to be conventional
Use state.
2) the air-drop mode of the grid-connected switch K1 of accessory power supply is true, and power supply system is double wire system.Battery main switch K3 is disconnected
The case where, the pin insertion of K2, the ground of J1 control loop disconnects, and air-drop signal system power-off is in ready mode, lossless at this time
Electric loading is connected, it is ensured that the prolonged inventory of equipment waits air-drop.When the pin of K2 is freed, the ground of J1 control loop is connect
Logical, control unit ECU is powered on.Control unit ECU detect the air-drop mode of K1 be very after, into air-drop power up mode, control
Unit ECU starts to monitor the normally closed switch signal of K2, and pin K2 frees, and control unit ECU starts timing in 200 seconds, waiting air-drop
Equipment landing.After the completion of timing, positioning device is connected;Countdown logic is connected in control unit ECU activation at this time, is closed after 1 hour
The load of positioning device two-way is closed, aerial delivery provisions power supply is protected, avoids over-discharge.
3) to avoid after air-drop equipment from being chronically at the operating condition of double wire system and power on again and in the case that pin is not inserted into
It can false triggering air-drop signal activation system logic.Setting air-drop mode indicating lamp K mono-, when K1 is in air-drop mode, control
System is lighted in the case where having power supply, and flicker cycle 2Hz, prompt person closes air-drop mode in time, is by two-way load transfer
It is controlled by battery main switch K3.
As can be seen that invention introduces electrical circuits on the relay J1 of air-drop discharge cock K2 control, it can be achieved that signal
With the automatic collection and connection under power supply and air-drop state;Mode selector switch K1 is introduced, with realizing double wire system with one wire system
Switching, and provide type collection for control unit ECU;Devise the dual control based on mode switch K1 and air-drop discharge cock K2
Timing logic is dropped, avoids control unit ECU after control discharge cock K2 pin is extracted, the mistake after airborne landing is sentenced
It is disconnected.The setting of relay J2 can effectively ensure that in the case where aerial delivery provisions power on, air-drop signal activation system is not dropped
The influence of discharge cock K2;This programme is based on aerial delivery provisions and starts battery realization, does not increase additional battery, entirely when work
Between power consumption be less than 5Ah, have apparent advantage in weight.Therefore, before air-drop signal activation system of the invention solves air-drop
The life problems and charge and discharge problem of the problem of personnel operate power-supply system afterwards and air-drop power-supply system.
The above is only a preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, without departing from the technical principles of the invention, several improvement and deformations can also be made, these improvement and deformations
Also it should be regarded as protection scope of the present invention.
Claims (7)
1. a kind of air-drop signal activation system based on monocell characterized by comprising
Double-pole switch mode control switch K1, air-drop discharge cock K2, battery main switch K3, relay J1, relay J2 and control
Unit ECU processed;
The double-pole switch mode control switch K1, is double-pole two-position switch, is located on the panel of vehicle, connects control unit ECU,
It is divided into daily and air-drop two states, for daily and air-drop pattern switching;In the output end of battery main switch K3, parallel connection is all the way
Positive supply may be implemented to relay J2 in the case where battery main switch K3 is closed, shielding air-drop discharge cock K2 control
The influence of relay J1;The air-drop discharge cock K2 is located at outside vehicle, is activated automatically when dropping out cabin, has normally closed and normally open two
A contact, after air-drop, the pin of air-drop discharge cock K2 is extracted, and realizes that normally closed switch is opened, and normally opened closes the switch, from
And the flag bit realizing the switching of power supply and being powered on as delay;The battery main switch K3 is located on the panel of vehicle, and out one
Route connects the relay J2, connects the relay J1 and control unit ECU, for shielding air-drop switch shape after landing
State;The relay J1 connects K2 as air-drop power source active relay, and when the pin of K2 is extracted, normally opened is closed the switch,
It is powered on for control unit ECU;Described control unit ECU is used to acquire the position of the switch of K1, acquires the timing commencing signal of K2, with
And complete the distribution task loaded to two-way.
2. the system as claimed in claim 1, which is characterized in that the system also includes air-drop mode indicating lamp K, for auxiliary
When power grid switch K1 being helped to be in air-drop mode, control system is lighted in the case where there is power supply.
3. system as claimed in claim 2, which is characterized in that the flicker cycle of the air-drop mode indicating lamp K is 2Hz, with
User is prompted to close air-drop mode.
4. the system as claimed in claim 1, which is characterized in that the relay J1, relay J2 contact be also connected with a storage
Battery, the cathode connection switch K1 of the battery.
5. the system as claimed in claim 1, which is characterized in that the load is variety classes positioning device.
6. a kind of working method of the system as described in any one of claims 1 to 5, which comprises the following steps:
When the daily mode of the grid-connected switch K1 of accessory power supply is true, power supply system is one wire system, after battery main switch K3 is closed
J2 is connected, and after shielding influence of the air-drop discharge cock K2 to system is at this point, control unit ECU powers on, acquisition accessory power supply is grid-connected
The daily mode signal of switch K1 is very, to default distribution to positioning device, be not delayed;
When the air-drop mode of the grid-connected switch K1 of accessory power supply is true, power supply system is double wire system, what battery main switch K3 was disconnected
Situation, the pin insertion of K2, the ground of J1 control loop disconnect, and air-drop signal system power-off is in ready mode, at this time without power consumption
Load is connected, and air-drop is waited, and when the pin of K2 is freed, the ground of J1 control loop is connected, and control unit ECU is powered on, control unit
ECU detect the air-drop mode of K1 be very after, into air-drop power up mode, control unit ECU start monitor K2 normally closed switch
Signal, pin K2 free, and control unit ECU starts timing in 200 seconds, and waiting landing after the completion of timing, connects two-way load;This
When control unit ECU activation connect countdown logic, after 1 hour shutdown signal load.
7. method as claimed in claim 6, which is characterized in that when K1 is in air-drop mode, drop mode indicating lamp K point
Bright, flicker cycle 2Hz, prompt person closes air-drop mode in time, is to be controlled by battery main switch K3 by two-way load transfer.
Priority Applications (1)
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CN201811214542.3A CN109301924B (en) | 2018-10-18 | 2018-10-18 | Air-drop signal activation system based on single battery and working method thereof |
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CN201811214542.3A CN109301924B (en) | 2018-10-18 | 2018-10-18 | Air-drop signal activation system based on single battery and working method thereof |
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CN109301924A true CN109301924A (en) | 2019-02-01 |
CN109301924B CN109301924B (en) | 2021-07-02 |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201528221U (en) * | 2009-09-10 | 2010-07-14 | 安徽方兴科技股份有限公司 | Three-path power automatic-switching circuit for improving service life of EPS system |
JP2012062768A (en) * | 2010-09-14 | 2012-03-29 | Denso Corp | Engine stop/start control device |
CN106843281A (en) * | 2017-03-09 | 2017-06-13 | 北京航天控制仪器研究所 | A kind of intelligence accurately drop from the air aerial delivery system |
CN206432730U (en) * | 2016-12-02 | 2017-08-22 | 武汉航空仪表有限责任公司 | A kind of power switch circuit of cyclelog |
-
2018
- 2018-10-18 CN CN201811214542.3A patent/CN109301924B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201528221U (en) * | 2009-09-10 | 2010-07-14 | 安徽方兴科技股份有限公司 | Three-path power automatic-switching circuit for improving service life of EPS system |
JP2012062768A (en) * | 2010-09-14 | 2012-03-29 | Denso Corp | Engine stop/start control device |
CN206432730U (en) * | 2016-12-02 | 2017-08-22 | 武汉航空仪表有限责任公司 | A kind of power switch circuit of cyclelog |
CN106843281A (en) * | 2017-03-09 | 2017-06-13 | 北京航天控制仪器研究所 | A kind of intelligence accurately drop from the air aerial delivery system |
Non-Patent Citations (1)
Title |
---|
李党索等: "运输机机载空投系统延迟环节和初步延迟时间分析", 《航空科学技术》 * |
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