CN208789515U - A kind of starting of helicopter and energization inspection system - Google Patents
A kind of starting of helicopter and energization inspection system Download PDFInfo
- Publication number
- CN208789515U CN208789515U CN201821598002.5U CN201821598002U CN208789515U CN 208789515 U CN208789515 U CN 208789515U CN 201821598002 U CN201821598002 U CN 201821598002U CN 208789515 U CN208789515 U CN 208789515U
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- China
- Prior art keywords
- module
- display screen
- energy
- temperature sensor
- storage module
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The utility model discloses a kind of starting of helicopter and energization inspection systems; including PMS controller, indicator light, display screen, charge relay, charging adapter, overcurrent, short circuit protection module, discharge prevention module, temperature sensor, NTC thermistor and energy-storage module; the output end of PMS controller is connect with the input terminal of indicator light, display screen, charge relay, charging adapter, overcurrent, short circuit protection module, discharge prevention module respectively, and PMS controller is bi-directionally connected with temperature sensor.The setting that the utility model passes through discharge prevention module; reach in use process; if there is total voltage is too low or low battery; PMS controller can notify client by display screen and indicator light; it reminds client to charge, by the setting of temperature sensor and NTC people's resistance, has reached temperature sensor and passed through NTC thermistor; it is connected with the resistance of known value, the size of temperature is judged by the voltage difference between two resistance of detection.
Description
Technical field
The utility model relates to helicopter starting and energization Examined effect field, specially a kind of helicopter starting and energization
Inspection system.
Background technique
Helicopter needs to check the capacitance type energy storing battery of interior of aircraft, capacitance type energy storing battery temperature monitoring before take-off
Electronic product be to temperature it is extremely sensitive, excessively high temperature and too low temperature will affect the stability of product, cause to charge
It can not be carried out with electric discharge, such as be unable to double check before take-off, it will huge security risk is brought to user, for this purpose,
We have proposed a kind of starting of helicopter and energization inspection systems.
Utility model content
The purpose of this utility model is to provide a kind of starting of helicopter and energization inspection systems, have inspection carefully, and
The good advantage of Checking on effect, solves and is unable to double check before take-off, it will brings huge security risk to user
The problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of helicopter starting and the inspection system that is powered
System, including PMS controller, indicator light, display screen, charge relay, charging adapter, overcurrent, short circuit protection module, electric discharge guarantor
Protect module, temperature sensor, NTC thermistor and energy-storage module, the output end of the PMS controller respectively with indicator light, aobvious
The input terminal connection of display screen, charge relay, charging adapter, overcurrent, short circuit protection module, discharge prevention module, the PMS
Controller is bi-directionally connected with temperature sensor, and the output end of the charge relay and the input terminal of energy-storage module connect, described
The output end of charging adapter and the input terminal of energy-storage module connect, the overcurrent, the output end of short circuit protection module and energy storage
The input terminal of module connects, and the output end of the discharge prevention module and the input terminal of energy-storage module connect, the temperature sensing
Device is bi-directionally connected with NTC thermistor, and the NTC thermistor is bi-directionally connected with energy-storage module.
Preferably, the charging adapter includes the charging of mould group and monomer equalizaing charge both of which.
Preferably, the indicator light is tri-colour LED, respectively red, yellow and green.
Preferably, the display screen is using wide warm OLED display screen.
Compared with prior art, the beneficial effects of the utility model are as follows:
1, the utility model is by the setting of charge relay, when having reached energy-storage module and being charged, if there is total
Voltage, monomer voltage, temperature, current anomaly and when needing to be serviced, PMS controller can active control charge relay close
It closes, after trouble shooting, charge relay can be attracted work again, by overcurrent, the setting of short circuit protection module, reach root
Factually border test case, if occurring output overcurrent, short-circuit conditions in use process, PMS controller will by display screen and
Indicator light notifies user, reminds user's load, by the setting of discharge prevention module, has reached in use process, if
Appearance total voltage is too low or low battery, PMS controller can notify client by display screen and indicator light, and client is reminded to fill
Electricity has reached temperature sensor by NTC thermistor by the setting of temperature sensor and NTC people's resistance, by its with it is known
The resistance of resistance value is connected, and the size of temperature is judged by the voltage difference between two resistance of detection.
2, the utility model is reached by the setting of charging adapter internal model group charging and monomer equalizaing charge both of which
The relay that PMS controller is connected in condenser type energy-storage module charge circuit and each module monomer charge circuit by control
Charging is controlled, when not enough power supply, two kinds of charge modes are involved in work, are the setting of three colors by indicator light, reach
It can show dangerous warning information and charge information, the fast blink of LED light red prompts user when energy-storage module capacity is low, fills
LED light red flashes at a slow speed when electric, and LED light green is always on when normal, if there is energy-storage module damage, overdischarge, overcharge,
The phenomenons such as monomer superpressure, monomer are under-voltage or global voltage is low, system detect indicator light by circuit and are exported, indicator light yellow
Fast blink, by display screen using the setting of wide warm OLED display screen, having reached display screen can satisfy low temperature to subzero four
It is used under ten degrees Celsius of environment, while there is good optical characteristics, guarantee can normally to show under strong illumination condition
Effect.
Detailed description of the invention
Fig. 1 is Tthe utility model system operation principle schematic diagram；
Fig. 2 is the utility model active equalization schematic illustration；
Fig. 3 is the utility model power supply external communication interface working principle diagram.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-3, a kind of helicopter starting and energization inspection system, including PMS controller, indicator light, display screen,
Charge relay, charging adapter, overcurrent, short circuit protection module, discharge prevention module, temperature sensor, NTC thermistor and
Energy-storage module, the output end of PMS controller respectively with indicator light, display screen, charge relay, charging adapter, overcurrent, short circuit
The input terminal connection of protective module, discharge prevention module, charging adapter include the charging of mould group and two kinds of moulds of monomer equalizaing charge
Formula has reached PMS controller and has passed through control by the setting of charging adapter internal model group charging and monomer equalizaing charge both of which
It makes the relay being connected in condenser type energy-storage module charge circuit and each module monomer charge circuit to control charging, electricity
When amount is insufficient, two kinds of charge modes are involved in work, and indicator light is tri-colour LED, and respectively red, yellow and green pass through
Indicator light is the setting of three colors, and dangerous warning information and charge information can be shown by having reached, LED light when energy-storage module capacity is low
Red fast blink prompts user, and LED light red flashes at a slow speed when charging, and LED light green is always on when normal, if there is energy storage
Module damage, overdischarge, overcharge, monomer superpressure, the phenomenons such as monomer is under-voltage or global voltage is low, system are referred to by circuit detection
Show that lamp is exported, indicator light yellow fast blink, display screen is using wide warm OLED display screen, by display screen using wide temperature
The setting of OLED display screen, has reached display screen and can satisfy and used under low temperature to subzero 40 degrees Celsius of environment, has simultaneously
Good optical characteristics, guarantees the effect that can normally show under strong illumination condition, and PMS controller and temperature sensor are double
To connection, the output end of charge relay and the input terminal of energy-storage module are connected, the output end and energy-storage module of charging adapter
Input terminal connection, overcurrent, the output end of short circuit protection module and energy-storage module input terminal connection, discharge prevention module it is defeated
The connection of the input terminal of outlet and energy-storage module, temperature sensor are bi-directionally connected with NTC thermistor, NTC thermistor and energy storage
Module is bi-directionally connected, by the setting of charge relay, when having reached energy-storage module and being charged, if there is total voltage, list
Bulk voltage, temperature, current anomaly and when needing to be serviced, PMS controller can active control charge relay close, work as failure
After releasing, charge relay can be attracted work again, by overcurrent, the setting of short circuit protection module, reach according to practical survey
Situation is tried, if occurring output overcurrent, short-circuit conditions in use process, PMS controller will be led to by display screen and indicator light
Know user, reminds user's load, by the setting of discharge prevention module, reached in use process, if there is total electricity
Low or low battery is pressed through, PMS controller can notify client by display screen and indicator light, remind client to charge, pass through
The setting of temperature sensor and NTC people's resistance has reached temperature sensor by NTC thermistor, by itself and known value
Resistance series connection, pass through the voltage difference between two resistance of detection to judge the size of temperature.
In use, by the setting of charge relay, when having reached energy-storage module and having been charged, if there is total voltage,
Monomer voltage, temperature, current anomaly and when needing to be serviced, PMS controller can active control charge relay close, when therefore
After barrier releases, charge relay can be attracted work again, by overcurrent, the setting of short circuit protection module, reach according to reality
Test case, if occurring output overcurrent, short-circuit conditions in use process, PMS controller will pass through display screen and indicator light
It notifies user, reminds user's load, by the setting of discharge prevention module, reached in use process, if there is total
Brownout or low battery, PMS controller can notify client by display screen and indicator light, and client is reminded to charge, and lead to
The setting of excess temperature sensor and NTC people's resistance has reached temperature sensor by NTC thermistor, by itself and known resistance
The resistance of value is connected, and the size of temperature is judged by the voltage difference between two resistance of detection.
In summary: helicopter starting and energization inspection system pass through PMS controller, indicator light, display screen, charging
Relay, charging adapter, overcurrent, short circuit protection module, discharge prevention module, temperature sensor, NTC thermistor and energy storage
Being used cooperatively for module, solves and is unable to double check before take-off, it will brings huge security risk to user
Problem.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of starting of helicopter and energization inspection system, including PMS controller, indicator light, display screen, charge relay, fill
Electric adapter, overcurrent, short circuit protection module, discharge prevention module, temperature sensor, NTC thermistor and energy-storage module, it is special
Sign is: the output end of the PMS controller respectively with indicator light, display screen, charge relay, charging adapter, overcurrent, short
The input terminal connection of road protective module, discharge prevention module, the PMS controller is bi-directionally connected with temperature sensor, described to fill
The output end of electrical relay and the input terminal of energy-storage module connect, the input of the output end and energy-storage module of the charging adapter
End connection, the input terminal connection of the overcurrent, the output end of short circuit protection module and energy-storage module, the discharge prevention module
The connection of the input terminal of output end and energy-storage module, the temperature sensor are bi-directionally connected with NTC thermistor, the NTC temperature-sensitive
Resistance is bi-directionally connected with energy-storage module.
2. a kind of helicopter starting according to claim 1 and energization inspection system, it is characterised in that: the adaptive charging
Device includes the charging of mould group and monomer equalizaing charge both of which.
3. a kind of helicopter starting according to claim 1 and energization inspection system, it is characterised in that: the indicator light is
Tri-colour LED, respectively red, yellow and green.
4. a kind of helicopter starting according to claim 1 and energization inspection system, it is characterised in that: the display screen is adopted
With wide warm OLED display screen.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821598002.5U CN208789515U (en) | 2018-09-29 | 2018-09-29 | A kind of starting of helicopter and energization inspection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821598002.5U CN208789515U (en) | 2018-09-29 | 2018-09-29 | A kind of starting of helicopter and energization inspection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208789515U true CN208789515U (en) | 2019-04-26 |
Family
ID=66211323
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821598002.5U Active CN208789515U (en) | 2018-09-29 | 2018-09-29 | A kind of starting of helicopter and energization inspection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208789515U (en) |
-
2018
- 2018-09-29 CN CN201821598002.5U patent/CN208789515U/en active Active
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